Design Guide
1545 design rules for small and tabletop cyclotrons, extracted from the
amateur-relevant accelerator literature — Livingston & Blewett to
undergraduate machine theses. Each rule carries its formula where the source
gives one, a verbatim quote, a page-level citation, and a stable identifier
(dg-001…dg-1545) that can be cited and linked
directly. Most readers want one of the per-subsystem pages in the directory
below; for a first reading, start at
level 1 — the 40 rules that govern any machine’s
feasibility. The editorial notes are calibrated to one concrete machine, whose
parameters come first.
Verify before use. These rules were machine-extracted from the literature, and every one is a source extract: faithful to its cited source, not an independently validated engineering requirement. The quote on each card is the source verbatim; the rule and the editorial note beneath it are this site’s, the note an extrapolation to tabletop scale the source never addressed. Any rule that drives a real design decision — and every safety-critical number — deserves a re-read at the cited page before you commit metal, money, or high voltage. Pair the rules with the safety fundamentals and your jurisdiction’s registration requirements; the full editorial contract, including how the extraction and its audits work, is on the methodology page.
The reference machine
Every row is the builds-census entry mullins-2017, which cites the machine's public build log; no figure here comes from anywhere else. It is one peer among the machines in the builds census, cited there like any other source, and it appears here because a note that says “~0.8 mm of turn separation” is only checkable against a machine whose numbers are on the page.
- Magnet
- Home-built H-frame, 1018 cold-rolled steel, 757 lb — two coils, 538 turns of 1/4-inch copper tubing, Sorensen DCS 55-55 supply
- Poles
- 8 in diameter, 1.42 in gap — 203 mm poles on a 36 mm gap
- Field
- 0.58–0.59 T in operation operating — 0.582 T at the best run; 0.850 T is the maximum measured, at 55 A, and the machine has never run beam there
- RF
- 8.9–9 MHz operating — 8.87 MHz at the best run; a 5 W amplifier drives a single 4-inch dee
- Dee voltage
- ~1.3 kV uncalibrated — the figure the build log quotes, read from a pickup coil and never absolutely calibrated; treat any turn count derived from it as indicative
- Vacuum
- ≈6 × 10⁻⁶ torr while operating operating
- Beam
- protons, 1–2 nA typical, 3.2 nA best operating — internal only — a Faraday cup on a 4-inch linear translator; the machine has no extraction
- Energy
- ≈150 keV typical, ≈164 keV best demonstrated computed — computed from field and radius rather than measured, and the guide's own rules say why that distinction matters
- Usable field radius
- ~3.2 in of the 4-in pole radius — where the field is still flat. The beam is collected further out than this, in the fringe, which is why a naive B²R² estimate over the flat region lands below the machine's demonstrated energy
- Planned upgrade
- 100–500 W RF amplifier, dee toward 5–13 kV planned — the "next machine" of the notes is a higher-field, tighter-gap successor, not this upgrade
The tier labels are the guide’s own discipline applied to itself: a design point, a bench measurement and the configuration a machine actually runs in are three different quantities, and a source will quote whichever it likes without saying which. Where a note says “a next machine”, it means a prospective higher-field, tighter-gap successor to this build. Full entry with citations: builds census.
How the rest of this page works: each rule’s level (1–5)
ranks how early and how universally it binds a design — breadth, never weight. A level
is not permission to skip a rule whose trigger your machine has, and safety rules are
never skippable on level alone; how the levels were assigned and audited is on the
methodology page. dg-NNNN
anchors resolve here and on the per-domain pages alike (e.g.
/design-guide/#dg-217). And this page is the evidence layer: the
Learn deep dives are the syntheses that read a subsystem in
order, citing these rules as they go — where the two differ, the source quote wins.
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Momentum-analyze the beam to select one ion species with a small energy spread using a bending field and defining slit: in the source, a 10 cm bend radius, poles about 4 cm wide with a 1 cm gap at up to 18 kG, and a 0.5 x 1 cm slit sort out a given kind of ion.
r = 10 cm, gap 1 cm, B up to 18 kG; slit 0.5 cm x 1 cmSource quote & editorial note
The mean radius of curvature of the path is 10 cm., and the pole pieces are about 4 cm. wide and are separated by a 1-cm. gap. The electromagnet used will produce a field of 18,000 gauss between these pole-pieces. A slit Y, 0.5 cm by 1 cm, serves to define the deflected beam and sort out a given kind of ion with a small range of energies.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 262
Editorial note, tabletop extrapolation: In a cyclotron the machine itself is the analyzer, but an external species check on a next machine's beamline follows the same method: compute the magnetic rigidity of each species at the beam energy, choose bend radius and field to separate them, and let a defining slit pass one - the source's geometry is a worked example at its stated beam, not proportions to copy.
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Compute achievable proton energy as T(MeV) = 3.12e-4 x B^2(kilogauss) x R^2(inches), where R is the radius of usable UNIFORM field, not the physical pole radius.
T(MeV) = 3.12e-4 * B^2(kG) * R^2(in) for protons; 1.56e-4 for deuteronsSource quote & editorial note
Protons: T (Mev) = 3.12 x 10-4 B2R2 ... the radius R applies to the extent of the uniform magnetic field; the physical radius of pole faces must be larger by about one-half the gap length.
Livingston & Blewett, Particle Accelerators (1962) — p. 158
Editorial note, tabletop extrapolation: For 8-in poles at 5.9 kG with the reference machine's 1.42-in gap, the flat field ends near R = 3.2 in, predicting ~110 keV - below what the machine demonstrates, because its cup collects further out, in the fringe. Read the formula as the energy the UNIFORM field alone buys; a wider pole or smaller gap moves that number as B^2R^2.
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Keep the field index n = -(r/B)(dB/dr) between 0 and 1 everywhere ions circulate; both axial and radial oscillations are stable only in this band.
B = B0*(r0/r)^n (constant-n form); stability requires 0 < n < 1; f_axial = sqrt(n)*f0, f_radial = sqrt(1-n)*f0Source quote & editorial note
for particle oscillations about an equilibrium orbit to be stable for both axial and radial coordinates, the value of n must be in the range 0 < n < 1.
Livingston & Blewett, Particle Accelerators (1962) — p. 161
Editorial note, tabletop extrapolation: Map n(r) on the 8-in poles; any region where the field rises with radius (n < 0) is axially defocusing, and the longer the beam spends there the less of it survives - shim such regions out rather than reasoning about how much defocusing is tolerable.
Cited in: Beam Dynamics: An Interactive Laboratory
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Shape the field to fall smoothly with radius by a total of 3 to 4 percent (small machines with relatively high dee voltage and few turns) or ~2 percent (medium 15-20 MeV machines) from center to the exit radius - the quoted historical totals.
total radial field decrease: 3-4% (small cyclotrons), ~2% (15-20 MeV), ~1% (very large)Source quote & editorial note
the total decrease below the value of the central field out to the exit slit is about 2 per cent. The radial decrease can be larger (3 to 4 per cent) in small machines in which D voltage is relatively high.
Livingston & Blewett, Particle Accelerators (1962) — p. 161
Editorial note, tabletop extrapolation: The reference machine is the small, few-turn case the quote names, and the census machines converged on the same few-percent smooth droop (dg-702). Aim for a smooth 3-4%-class fall-off shaped against the machine's own n(r) requirement (dg-003), with the number as the historical anchor rather than the spec.
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MIT's measured weak-focusing profile: n(r) rises roughly linearly from 0 at center to ~0.02 where fringing begins, then rapidly to ~0.4 at the exit-slit radius and 1.0 just beyond; they placed the septum just inside the maximum-energy radius.
MIT: n = 0 -> 0.02 at r = 0.8*R_pole, 0.40 at exit slit (18.75 in), 1.0 at 19.25 inSource quote & editorial note
The n value rises almost linearly from zero at the center to 0.02 at 15 in. (where fringing effects start), then increases rapidly to 0.40 at 18.75 in. (exit-slit location) and to 1.0 at 19.25 in.
Livingston & Blewett, Particle Accelerators (1962) — p. 161-183
Editorial note, tabletop extrapolation: One documented profile, useful as a shape target rather than a scaling law: fringe onset and width depend on gap-to-pole ratio, edge shape and shims, so map n(r) on the actual 8-in poles (FEMM, then measurement) and place extraction where the MEASURED n has climbed toward ~0.4 - before the n = 1 radial-stability edge.
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Machine pole faces parallel to about 1 part in 50,000 of the pole diameter; a rigid stack of a few heavy machined blocks needs very few bolts, with dowel pins or keys for alignment.
parallelism tolerance ~ D_pole / 50,000Source quote & editorial note
Precise machining of the surfaces in contact is necessary to make pole faces accurately parallel. The required machine tolerance is about 1/50,000 of the pole diameter and calls for the best machine practice. The structure of a few heavy blocks with machined faces in contact is quite rigid and requires very few bolts; alignment can be maintained by dowel pins or keys.
Livingston & Blewett, Particle Accelerators (1962) — p. 193
Editorial note, tabletop extrapolation: For 8-in poles that is ~0.00016 in (~4 um) parallelism - a surface-grinder job; non-parallel poles show up as the sinusoidal azimuthal error in field maps.
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Taper the poles so flux density stays roughly constant along their length; a designed 18 kG gap field needs a pole base about 24 percent larger in diameter to stay under ~20 kG in the iron.
42-in pole face at 18 kG -> ~52-in base; keep B_iron < ~20 kG (saturation)Source quote & editorial note
For a designed flux density of 18 kilogauss in the gap of a 42-in. cyclotron ... the pole base would have to be about 52 in. in diameter to keep flux density in the base of the pole below the practical limit.
Livingston & Blewett, Particle Accelerators (1962) — p. 193
Editorial note, tabletop extrapolation: At 5.9 kG straight cylindrical poles are fine on the reference machine; taper starts paying when the LOCAL flux in the pole approaches the steel's knee - a FEMM check, not a gap-field threshold. The source's worked case is the calibration: an 18 kG gap wanted a base about 24% larger in diameter.
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Size the magnet gap around 1/8 of pole diameter when energy matters (5-6 in gaps on 42-in poles, 8-9 in on 60-in); excitation power grows roughly as gap length squared and a wider gap loses usable radius to fringing.
g/D_pole ~ 0.12-0.14; magnet power ~ g^2Source quote & editorial note
the longer the magnet gap the larger is the power required for excitation, varying approximately with the square of gap length ... use of 5- to 6-in. gaps for 42-in. poles and 8- to 9-in. gaps for 60-in. poles.
Livingston & Blewett, Particle Accelerators (1962) — p. 194
Editorial note, tabletop extrapolation: On 8-in poles the historical ratio suggests a ~1-inch-class gap as a starting point - at tabletop scale the RF structure, chamber walls and fringe-vs-radius scaling often force it larger, so treat the ratio as the iron-economy pull in a trade the other subsystems get votes in (dg-163). Every extra gap costs amp-turns (power ~ g^2) and usable radius.
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Regulate magnet current to better than 1 part in 1000 (sense a series standard resistor against a voltage reference and feed back); a drifting field detunes resonance before anything else does.
dI/I < 1e-3Source quote & editorial note
The magnet field must be accurately regulated to maintain a steady beam ... A constant-current regulator is needed, capable of reducing fluctuations to better than 1/1000.
Livingston & Blewett, Particle Accelerators (1962) — p. 194
Editorial note, tabletop extrapolation: A modern current-regulated supply can meet this - verify ripple AND thermal drift on the actual unit: 0.1% of 5.9 kG is 6 G, a shift of the same order as deliberate shim corrections, so supply drift competes with the shim budget (and with RF detuning) for the resonance.
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Create the radial field droop with a flat pyramidal stack of thin iron disk shims of graded diameter in the shimming gaps between chamber and poles (MIT: four 0.020-in soft-iron disks of 6, 14, 18, and 22 in diameter for 38-in usable field).
graded-diameter 0.020-in soft iron disks stacked concentrically in the shimming gaps (MIT: 6, 14, 18, 22 in)Source quote & editorial note
with a magnitude of decrease out to this point of about 2 per cent of the central field. Although this field shape can be achieved by machining of the surfaces of the pole faces, it is usually obtained by inserting a flat pyramidal stack of thin iron shims in shimming gaps outside the pole-face plates. ... obtained by the use of such stacks in the two shimming gaps, each consisting of four disks of 0.020-in. soft iron sheet of 6, 14, 18, and 22 in. diam.
Livingston & Blewett, Particle Accelerators (1962) — p. 195
Editorial note, tabletop extrapolation: MIT's stack is historical calibration, not a recipe - shim response does not scale geometrically with pole size or gap. For the reference machine, set the droop target from the focusing requirement, then determine disk diameters and count by field mapping or magnetostatic modeling, iterating; the graded flat-pyramid form is the transferable part.
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Fasten soft-iron ring shims to the extreme pole edge to hold off fringing droop, but size them cautiously: oversized rings (or correct rings run at lower field) produce a local field minimum that defocuses.
MIT optimum edge-ring section: 3/4 in x 1/4 in on 42-in polesSource quote & editorial note
At MIT the optimum ring section was 3/4 by 1/4 in. ... Shims which are too large produce a minimum in the radial field plot which would cause defocusing. Also, a set of shims which are correct at high fields will be too strong and produce a defocusing minimum in the plot at lower fields.
Livingston & Blewett, Particle Accelerators (1962) — p. 196
Editorial note, tabletop extrapolation: An edge ring can extend the reference machine's usable radius, but size it empirically: start conservative, map the radial field at every operating current (the lower-field defocusing minimum is the trap), and trim iteratively - MIT's 3/4 x 1/4 in section is their optimum on 42-in poles, not a scaling template.
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Operators of large classical cyclotrons agreed that unintended azimuthal field variation under 0.1 to 0.2 percent of B - measured as the maximum variation around a circle of constant radius, most critically near the exit-slit radius - is desirable; correct with sector- and wedge-shaped shims after mapping.
max azimuthal variation < 0.1-0.2% of B; MIT reduced 2% as-built errors to <0.1%Source quote & editorial note
The figure of merit used to describe azimuthal uniformity is the maximum per cent variation around a circle of constant radius, and the most critical region is near the exit-slit location. ... Most operators agree that a variation of less than 0.1 to 0.2 per cent is desirable in large cyclotrons. ... After careful correction by use of sector-shaped and wedge-shaped shims, the errors were reduced to less than 0.1 per cent for all radii out to the exit slit.
Livingston & Blewett, Particle Accelerators (1962) — p. 196-197
Editorial note, tabletop extrapolation: At 5.9 kG this means holding azimuthal wobble to ~6-12 G; an azimuthal bump acts like a field error that pumps radial oscillation amplitude.
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Find the magnetic median plane (it can sit well off the geometric midplane - 1/2 in at MIT) with a pair of opposed identical search coils equally spaced about the center, axis normal to the pole faces; recenter it by trimming the relative excitation of the upper and lower windings in the direction the measurement indicates (MIT reduced the upper).
two identical coils in series opposition straddling midplane; balance point = magnetic median planeSource quote & editorial note
A special search coil can be used to observe the median plane in the radially decreasing field, using two opposed identical coils equally spaced about the center and with the axis precisely aligned normal to the pole surfaces. At MIT the uncorrected field showed a median plane displaced 1/2 in. below the central plane ... adequately corrected by reducing excitation in the upper magnet windings relative to the lower ones.
Livingston & Blewett, Particle Accelerators (1962) — p. 197
Editorial note, tabletop extrapolation: The beam follows the magnetic plane, not the machined one; with separate top/bottom coil circuits (or a properly rated shunt across one layer, as MIT used for a dished plane) the builder can steer it back to mid-gap - size any shunt for its current and dissipation first.
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When empirical shimming stalls, stop and run a full measurement campaign (radial plots, azimuthal circles at many radii, median-plane survey, spot checks for local flaws like blowholes); MIT's measured-then-corrected field beat years of cut-and-try on the first try.
Source quote & editorial note
The experience at MIT is typical. After several years of empirical shimming, with continual difficulties in maintaining high-intensity operation, a careful program of measurement and correction was carried out as indicated in the illustrations above. When this program was completed, the cyclotron was reassembled and on the first operation gave the highest beam intensities ever obtained, with no further empirical shimming.
Livingston & Blewett, Particle Accelerators (1962) — p. 197
Editorial note, tabletop extrapolation: The single strongest process lesson for a next machine: map first, shim from data - a systematic field map costs far less time than open-ended beam-chasing, and measurement-based correction is what ended MIT's years of cut-and-try.
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Local field defects have local fixes: a 0.5 percent weak spot (e.g., casting blowhole) is corrected with a small spot shim; a dominant fundamental (once-around) azimuthal sinusoid suggests checking pole parallelism and measurement-pivot centering first.
Source quote & editorial note
A local weak spot in the field (0.5 per cent low) was observed in the MIT magnet which was presumed to be due to a blowhole in the pole casting; it was corrected by a local spot shim.
Livingston & Blewett, Particle Accelerators (1962) — p. 197-284
Editorial note, tabletop extrapolation: Read azimuthal maps by their harmonic content, as a first diagnosis rather than a chart: a dominant first harmonic says check tilt and centering first (it can also be a genuine dipole asymmetry of iron, coil or yoke, or nearby hardware); higher harmonics point at localised defects, sector features, extraction hardware or the measurement itself. Confirm a suspected cause by re-mapping after the mechanical correction, then trial shims taped on before permanent installation. [Note revised 2026-08-23: earlier note presented the harmonic reading as one-to-one.]
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The gap field follows B = mu0*Ni/g while the iron is well below saturation; at higher excitation the observed field falls short of the ideal - Livingston & Blewett's example delivered 0.73 of the prediction at 18 kilogauss - as iron reluctance and leakage grow.
B = K*mu0*Ni/g; K -> 1 at low excitation, measured 0.73 at 18 kG on their magnet; 10 kG across a 10 cm gap: 7.95e4 A-turns idealSource quote & editorial note
To produce a field B of 1 weber/m2 (10 kilogauss) in a gap of 10 cm length, the number of ampere-turns required is 7.95 x 10^4 ... At 18 kilogauss ... the observed value of B is 0.73 of that predicted.
Livingston & Blewett, Particle Accelerators (1962) — p. 258-260
Editorial note, tabletop extrapolation: At the reference machine's 5.9 kG the ideal formula is a good first estimate (~1.7e4 ampere-turns across its 3.6 cm gap) before iron reluctance and leakage add their share - FEMM closes that gap. Field headroom is cheap while the iron stays unsaturated and expensive after; where the knee sits is a property of the specific circuit, not a universal 10 kG line.
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Expect the usable field to end about half a gap-length inside the pole edge - the quoted offsets: 0.6g without shims, 0.45g with the chosen ring-shaped shims (what threshold defines 'usable', and the high-field behavior, are the book's context: scan re-read queued).
R_useful ~= R_pole - (0.45 to 0.6)*g; boundary moves inward at high B due to pole-corner saturationSource quote & editorial note
the edge of the usable region is inside the pole boundaries by about one-half the gap length ... Without shims the useful region was inside the pole edge by 0.6g; with the chosen ring-shaped shims it was inside by 0.45g.
Livingston & Blewett, Particle Accelerators (1962) — p. 260
Editorial note, tabletop extrapolation: With its 1.42-in gap on 8-in poles the builder loses ~0.85 in of radius to fringing; shrinking the gap or adding ring shims recovers usable radius.
Cited in: Cyclotron Magnet Design
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Map the field with a small search coil on a pivoted radial arm feeding an integrating fluxmeter; a full-circle sweep must return to zero deflection, which doubles as the amplifier drift check.
typical exploring coil: ~1000 turns fine wire, ~1/2 in ID x 1 in OD; Q = (Na/R)*dBSource quote & editorial note
A typical 'exploring' coil for a cyclotron magnet would have about 1000 turns of fine wire ... Total deflection should be zero after a full circle; this provides a check on the stability of the amplifier.
Livingston & Blewett, Particle Accelerators (1962) — p. 283-285
Editorial note, tabletop extrapolation: A pivoted-arm coil (or a modern Hall probe on the same fixture) sweeping circles at fixed radii is exactly the mapping jig an 8-in machine needs before shimming.
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Use the running cyclotron itself as a magnetometer: at resonance the RF frequency and e/m give the average field to high precision, but only the average - assigning it to a specific radius risks ~0.5 percent error.
B_avg = 2*pi*f*m/e at observed resonanceSource quote & editorial note
the magnetic field can be determined with high precision ... this resonance frequency represents an average value of the magnetic field from the center out to the exit radius ... an error of the order of 0.5 per cent is possible.
Livingston & Blewett, Particle Accelerators (1962) — p. 287-288
Editorial note, tabletop extrapolation: The reference machine's observed resonance peak vs magnet current is a magnetization-curve measurement of their own magnet - log it at every retune.
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A 'dished' (saucer-shaped) median plane indicates asymmetric magnet or foundation iron, asymmetrically located coils, or a shorted turn; MIT flattened one case by paralleling an external resistor across one coil layer to trim its current.
Source quote & editorial note
a common phenomenon ... is to find the median plane dished into a shallow saucer shape caused by asymmetries in the magnet iron or of the reinforcing iron in the foundations. A similar shape will result if the coils are not located symmetrically or if there is a shorted turn. ... At MIT such a 'dished' median plane was corrected by connecting an external resistor in parallel with one of the coil layers, which reduced the current in this layer and in this case had the effect of flattening the median plane.
Livingston & Blewett, Particle Accelerators (1962) — p. 288
Editorial note, tabletop extrapolation: Rebar in the floor or a nearby steel bench can dish an H-frame tabletop field; remove or symmetrize nearby steel first where practical, then trim electrically (a rated shunt across one accessible layer, as MIT did) rather than re-machining.
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Shrinking the pole gap raises the field at fixed excitation: the source expected reducing the gap from 3.8 cm to 1.3 cm to lift the same magnet from ~0.49 T to ~0.75 T - well short of the ideal inverse-gap prediction (~1.4 T), because leakage, iron reluctance, and (here) the permanent magnets' operating point all move with the gap; energy gain is quadratic in B, so gap reductions still pay twice.
ideal B ~ 1/g at fixed MMF is an upper bound (the source's own numbers deliver ~55% of it); T_final ~ B^2Source quote & editorial note
we will reduce the air gap between the poles of the magnet to 1.3 cm thereby increasing the magnetic field to roughly 0.75 T.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 22
Editorial note, tabletop extrapolation: The cheapest field upgrade for a next machine is gap reduction - thinner chamber lids, pole pieces reaching into the chamber - before any coil or steel changes. Model the actual gain in FEMM rather than assuming 1/g.
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Expect the 1%-uniform region of a flat-pole magnet to end well inside the pole radius - the measured case: 0.493 T uniform to 1% out to 6.19 cm on 7.6 cm radius poles, about 80% - and note the quoted geometry: their RF electrode at 7.14 cm CONTAINED the full uniform region, keeping acceleration inside it.
r_uniform(1%) ~ 0.8 * r_poleSource quote & editorial note
The magnetic field is uniform at 0.493 T, to within one percent, out to a radius of 6.19 cm... The RF electrode radius is 7.14 cm containing the full uniform region.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 22-23
Editorial note, tabletop extrapolation: Suggests planning the reference machine's usable beam radius around ~80% of the 8-in pole (~3.2 in) unless shims extend the flat region - with the machine's own field map as the arbiter (dg-098, dg-638).
Cited in: Cyclotron Magnet Design
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Characterize a repurposed electromagnet from its field-versus-gap curve before designing around it: the Varian V-3900 NMR magnet gives 2.7 T at a 1.25-inch gap, which at a 7.5 cm usable extraction radius yields E = q^2*B^2*r^2/(2m) ~ 1.96 MeV protons (the thesis's figure - usable radius, not the full 8 cm pole radius, goes in the formula).
KE = q^2*B^2*r^2/(2m); 2.7 T, r=0.075 m -> 1.96 MeVSource quote & editorial note
the magnet generates 2.7 T of magnetic field with a 1.25 inch pole separation... capable of accelerating protons to a maximum kinetic energy of 1.96 MeV
Editorial note, tabletop extrapolation: The surplus-NMR-magnet route to MeV energies: small radius is fully compensated by high B (energy ~ B^2*r^2), so a 6-inch 2.7 T machine beats a 12-inch 1 T machine.
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Concentrate flux by tapering the pole from a wider stem to a narrower face: Iowa State tapered 12-inch pole stems down to 10-inch pole faces with a 0.7-inch-thick shoulder at the face, and credits the tapered pole shape plus peripherally placed steel shims for field uniformity.
12 in stem -> 10 in face (1.2:1 taper), 0.7 in shoulder at pole face, plus peripheral steel shimsSource quote & editorial note
The magnet has tapered poles, the poles being tapered from 12-inch pole stems to 10-inch pole faces. There is a 0.7 inch thick shoulder at the pole face ... The tapered pole shape and peripherally placed steel shims contribute to the uniformity of the field.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 6-7
Editorial note, tabletop extrapolation: A concrete, machinable geometry pattern for concentrating flux into an 8-10 inch pole face - but transfer the method, not the numbers: taper, shoulder and shim dimensions depend on gap, saturation and yoke geometry, so model (FEMM) or map the field and set them iteratively.
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Plan roughly 20 kW of DC coil power - water-cooled hollow copper tubing on a 2-ton mild-steel core, 33-inch-diameter coils - as the Iowa State 1.5 MeV undergraduate cyclotron's magnet budget.
20 kW dc into water-cooled hollow-copper coils; 33 in coil diameter; 2-ton mild-steel core (Iowa State 1.5 MeV machine)Source quote & editorial note
The magnet consists of coils of hollow copper tubing wound on a two-ton core of mild steel ... These deliver to the magnet 20 kilowatts of electric power, which is dissipated by water circulating through the coils.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 6-7
Editorial note, tabletop extrapolation: Sets the scale of the jump from the reference machine's 0.59 T solid-tubing magnet toward a 1.5-1.7 T machine: at multi-kilowatt dissipation, hollow conductor with water flow is the usual regime (dg-092). The exact power for a next machine depends on its actual gap, field and copper budget - the magnet-power calculator sizes it, this precedent scales it.
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A workable student-cyclotron design point for ~1.5 MeV protons: 10-inch pole faces, 17,000 gauss, 25.68 MHz RF, 10-14 kV dee-to-dee at 2 kW RF, giving 2 uA of beam (about 1.3e13 protons/s).
10 in poles, 1.7 T, 25.68 MHz, Vdee 10-14 kV, 2 kW RF, 2 uA, 1.5 MeVSource quote & editorial note
Size: 10-inch pole diameter ... Dee voltage: 10,000 to 14,000 volts dee-to-dee; R.F. power: 2,000 watts; R.F. frequency: 25.68 megacycles ... Magnetic field strength: 17,000 gauss
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 9
Editorial note, tabletop extrapolation: The closest historical analogue to a next machine's target: same pole diameter as the reference machine, and the ~3x field buys the ~10x energy (E ~ B^2*r^2 at fixed radius). The ~10x dee voltage buys turn count, phase margin and beam survival at that field - not the energy ceiling itself.
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Regulate magnet current, not field, with a precision shunt feeding a difference amplifier against a voltage reference: this system held 17,000 gauss to +/-4 gauss (2.4e-4) - the stability that machine ran at.
+/-4 G on 17,000 G = 2.4e-4 stabilitySource quote & editorial note
This regulation system is capable of holding the 17,000 gauss field to within +/-4 gauss of its nominal value.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 9
Editorial note, tabletop extrapolation: A concrete precedent for a home magnet supply: a few parts in 1e4 is achievable with a shunt, op-amp and pass bank. What a given machine NEEDS follows from its turn count and phase budget (dg-273); this figure is the documented professional practice, not the requirement.
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Use an NMR magnetometer for the absolute field reference - the cited machine's instrument read easily to one gauss on its 17 kG field - and a Hall probe for mapping.
NMR field meter resolution ~1 gauss on 17 kGSource quote & editorial note
an instrument operating on the principle of nuclear magnetic resonance is used ... The instrument may be read easily to one gauss accuracy.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 9-10
Editorial note, tabletop extrapolation: The division of labor transfers: an NMR reading in a homogeneous region calibrates the mapping probe; a good calibrated Hall probe can carry the absolute job too if its spec covers the need. Either way the last word is the beam - resonance depends on the orbit-averaged field, harmonic and phase history, so set f from the map and trim on beam rather than expecting any point reading to set it exactly. (A DIY NMR gaussmeter is a classic amateur build; qualify its actual accuracy before trusting it.)
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Gap-height error is field error: hold pole-gap variation tightly - the source machine held gap variation at any given radius below 0.005 in on its 22-inch gap.
achieved: gap variation < 0.005 in at any radius (22-in gap, ~0.02% of gap)Source quote & editorial note
The pole gap is twenty-two inches, and, for any given radius, the gap variation is less than 0.005 inch.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 10
Editorial note, tabletop extrapolation: Derive the reference machine's own tolerance rather than copying the number: with dB/B ~ -dg/g for a gap-dominated circuit, the field error the orbit budget allows sets the gap tolerance - the source's fraction (0.005/22 ~ 0.02%) applied to a 2-in gap would mean ~0.0005 in, so pick the acceptable field error first and verify by mapping.
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Correct edge-region field falloff with 'Rose ring' shims - raised iron rings fastened near the pole periphery (ANL: 1/4 in thick x 2 in wide, radially 26 to 30 inches on the 30-inch-radius machine, fastened to the chamber lids) - plus an external pyramid of stacked discs (ANL: twelve 1/16-inch discs of decreasing radius, largest against the lid) for the bulk profile.
Rose rings 1/4 in x 2 in at r = 26-30 in (r/R ~ 0.87-1.0); external pyramid of twelve 1/16 in discs of decreasing radius (20, 16, 10, 6, 4, 3 in, in pairs)Source quote & editorial note
Magnetic shimming consists of internal Rose rings and external stepped shims. The internal rings are fastened to both the top and bottom lids and are radially located at 26 inches and extend outward to 30 inches. The rings are 1/4 inch thick and 2 inches wide. External top and bottom shimming consists of a pyramid of twelve discs, each 1/16 inch thick and of the following radii: 2 of 20 inches; 2 of 16 inches; 2 of 10 inches; 2 of 6 inches; 2 of 4 inches; and 2 of 3 inches. The largest disc is located in contact with the lid.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 10-11
Editorial note, tabletop extrapolation: The classic two-knob shim architecture for extending the reference machine's flat-field region: perimeter ring for the edge, thin stacked discs for the interior gradient.
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Use low-carbon soft iron for all flux-path parts: the ANL forgings ran C 0.12%, Si 0.17%, P 0.014%, S 0.024%, Mn 0.39% - the low-carbon end of the steel range is the standard magnet choice, with carbon the most-watched impurity.
C ~ 0.12% (low-carbon steel, 1010-1020 class or better)Source quote & editorial note
The magnet yoke, poles and tips, acceleration chamber lids, and shims are of soft iron forgings with the impurity analysis as follows: Carbon 0.12%...
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 11
Editorial note, tabletop extrapolation: A concrete spec to hand a supplier: 1010/1018-class low-carbon steel serves for a next machine's yoke stock; for pole tips avoid high-carbon or unknown scrap - and remember silicon and processing also move the curve, which is what measuring your own stock settles (dg-1330).
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Size the yoke return-path (arm) cross-section larger than the pole so the arms run below pole flux density and never saturate first: the source increased arm area by 25% and quotes the arm flux density as 1.2 T against the 1.6 T maximum (nominally 1.6/1.25 = 1.28 T - their 1.2 T is rounded or carries extra margin).
A_arm > A_pole; source: +25% area, quoted arm density 1.2 T vs 1.6 T pole (exact ratio 1/1.25 = 0.80)Source quote & editorial note
the arms of the yoke carry a 25% smaller flux density than the maximum: only 1.2 T. This is achieved by increasing their cross-sectional area by 25%.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 29
Editorial note, tabletop extrapolation: A ready sizing pattern for a next machine's H-frame: make every return-path section 25-33% larger in area than the pole face (33% if the goal is a genuine 25% density reduction), and check the narrowest section - that is the one that saturates first (dg-037).
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Machine a slight convex taper from pole center to edge to create the radially decreasing field needed for weak (betatron) focusing; the source specifies 0.02 inch on its poles.
cited machine: pole taper 0.02 in (0.5 mm) center-to-edge, 12-in poles at 1.6 TSource quote & editorial note
implement a .02'' convex taper from the center of the pole to the edge, to create sufficient bending of the magnetic field lines.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 31
Editorial note, tabletop extrapolation: The taper's size does not transfer: the gradient it produces depends on gap, pole radius, saturation and yoke geometry. Choose a target field index n = -(r/B)dB/dr for the reference machine, get the contour from magnetostatic modeling (FEMM), and finalize by field mapping and shimming - the source's 0.02 in is one machine's value, not a starting spec.
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Put a 45-degree chamfer on the pole edges to prevent local magnetic saturation at the corners and to soften the fringing field.
45 deg edge taperSource quote & editorial note
the edges of the pole have a 45 degree taper. This is to prevent magnetic saturation at the edges of the pole. The field due to the taper also fringes less sharply.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 31
Editorial note, tabletop extrapolation: Trivial machining step for a next machine's pole tips that buys margin against edge saturation at higher fields.
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Expect and accept roughly 4-5% total field droop from center to full dee radius (1.64 T -> 1.57 T at 6 in) in a weak-focusing design; verify with a magnetostatic code like Poisson Superfish.
dB ~ 0.08 T droop over 6 in radius at 1.6 T (~5%)Source quote & editorial note
at a dee radius of 6'' the field is 1.57 T, a .08 T drop off from 1.64 T directly at the center.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 31
Editorial note, tabletop extrapolation: One machine's by-design droop as a sanity anchor: a few percent total is the common class (dg-702's census clustering). What YOUR field may droop is set by the phase-slip budget and the n(r) requirement - verify with Poisson/FEMM against those, not against 5%.
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Size the coil from NI = B*g/mu0 as the first cut: 1.6 T across their 2.13-in gap computes to ~69 kA-turns, and they built 720 turns at 110 A (~79 kA-turns) - roughly 15% above the ideal figure, margin that real iron reluctance and leakage consume.
NI = B*g/mu0 (ideal gap-only first cut); their example: 68.9 kA-turns ideal, 79.2 kA-turns builtSource quote & editorial note
we used the basic equation for an electromagnet... we decided a 2.13'' gap a reasonable size... we then concluded that we needed 720 turns to reach 1.6T.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 32
Editorial note, tabletop extrapolation: The same sizing equation the reference machine's magnet obeys (its 538 turns are that build's own number, not this source's). The gap-only formula is the floor; the source's ~15% surplus is a realistic allowance for what it omits, and FEMM confirms the actual requirement (dg-016).
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Keep the magnetic circuit out of saturation: the source's 1060 steel saturates around 1.7 T, above which they treat further excitation as wasted, so their design keeps peak fields in the iron under about 1.6 T.
B_local(iron) < B_sat; B_sat(1060 steel) ~ 1.7 T (alloy- and treatment-dependent)Source quote & editorial note
Our magnet is constructed out of 1060 steel, which saturates at around 1.7 T; above this magnetic flux density the yoke is unaffected by further excitation.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 6, 29
Editorial note, tabletop extrapolation: The binding quantity is local flux density in the iron (narrowest yoke section, pole roots), not the gap field: at 0.59 T in the gap the reference machine is far from saturation everywhere, but a next machine pushing the gap past ~1.5 T must check each cross-section of the return path against its own steel's saturation curve - saturation onset is gradual and alloy-dependent, not a hard wall at 1.7 T.
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Use the permeance (magnetic Ohm's law) method for permanent-magnet circuits: judiciously divide external space into standard flux paths and sum permeances - total flux estimates come out within ~2% of computation, though local flux density may only be good to ~30%.
Phi = F * P_total; total-flux accuracy ~2%, local B ~30%Source quote & editorial note
agreement to within less than two percent. In contrast, calculations of the flux density at Point G yield 0.39 T for the analogue method and 0.30 T for the computer
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 10-11
Editorial note, tabletop extrapolation: If a next machine uses NdFeB anywhere (source magnets, the PM cyclotron study), the permeance method sizes gap flux without FEA - trusted for totals and not point fields, per the source's own one-circuit comparison (2% total-flux vs 30% local). Check the final design in FEA regardless.
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Clad the leakage surfaces of a permanent-magnet circuit with oppositely-polarized magnet material: in Leupold's horseshoe example cladding raised the gap field from 0.8 T to 2 T, and a 7 kg clad assembly outperformed a 55 kg unclad one (1.6 T) - but cladding pays only when leakage permeance dominates.
clad: 0.8 T -> 2.0 T, 7 kg vs 55 kg; gain small (0.5->0.8 T) when gap dominates permeanceSource quote & editorial note
The latter has a gap field of 2 T, as compared with only 0.8 T for the unclad structure... 7 kg mass of such an assembly compared to the 55 kg required to produce only 1.6 T ... When the horseshoe-like structure has no tapered pole pieces as in Fig. 7, most of the external permeance is in the gap, and cladding raises the gap field from 0.5 T to only 0.8 T.
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 15-16
Editorial note, tabletop extrapolation: Mostly a curiosity at cyclotron-gap geometry - the source's own no-taper horseshoe shows the gain collapsing (0.5 to 0.8 T) when the gap dominates the permeance - but valuable for compact PM ion-source or steering assemblies. The field and mass comparisons are between the source's specific example assemblies, not like-for-like scaling laws.
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A Halbach 'magic cylinder' delivers a transverse bore field Bw = Br*ln(R2/R1) with, in the ideal infinitely-long continuous model, zero exterior field; fields up to about twice the remanence (~2.0-2.5 T with NdFeB) are practicable, e.g. Br=1.2 T with 2.5 cm bore in a 15 cm OD gives 2.1 T with no power supply. Real finite, segmented assemblies leak: fringe and stray fields must be mapped, not assumed absent.
Bw = Br*ln(R2/R1) (ideal long continuous cylinder); practical max ~2*BrSource quote & editorial note
fields of twice the material remanence should be practicable, namely 2.0 to 2.5 T... Bw = 1.2 ln(15/2.5) = 2.1 T
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 24-25
Editorial note, tabletop extrapolation: Shows what PM technology can do at small bore: not a cyclotron gap replacement, but a zero-power option for beamline analysis/steering dipoles on a next machine's extracted beam.
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Open (non-enclosed) permanent-magnet field sources can be made when the required gap field is less than about half the material remanence - the source's feasibility condition for axially finite cavities. Above that, flux confinement (cladding, a closed yoke) or an optimized geometry (Halbach-class arrays) is what buys more.
B_gap (simple open source) <~ Br/2 - a sufficient-condition screen, not a hard ceilingSource quote & editorial note
If the required fields are less than about half the remanence, open compact sources for fields in axially finite cavities can be made
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 33
Editorial note, tabletop extrapolation: Quick feasibility screen: with Br ~ 1.3 T NdFeB, a simple open PM assembly reaches 0.6 T-class gap fields - marginal at the reference machine's field. Beyond it the answer is confinement or Halbach-class geometry, not impossibility.
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The infinite-permeability iron approximation used in permeance calculations fails when passive iron runs close to or above saturation - permeance bookkeeping is only valid for unsaturated pole pieces and yokes.
Source quote & editorial note
When passive materials such as iron are operated close to or above saturation the approximation mu_p = infinity does not hold and the method of permeance estimation is not readily practicable.
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 6
Editorial note, tabletop extrapolation: Same lesson as Tanabe from the PM side: every quick hand method assumes unsaturated iron. Rather than trusting a universal flux ceiling, check the chosen steel's B-H curve and verify peak local flux density (pole roots, corners) with a nonlinear FEA pass - an average yoke figure can hide saturated corners.
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Prefer rare-earth magnets (NdFeB, Br/B0c ~ 1.05, near-linear demagnetization) over alnico: an REPM has one circuit-independent mmf, while an alnico's operating point walks down minor loops whenever the gap is widened or the magnet removed, permanently losing strength.
Source quote & editorial note
no unique mmf can be assigned to a conventional permanent magnet... the magnet mmf will always be that corresponding to the lowest point on the demagnetization curve reached
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 8-10
Editorial note, tabletop extrapolation: Practical warning with the mechanism stated right: an alnico circuit loses strength when opening the gap drives it to a NEW lowest point on its demagnetization curve - the first excursion does the damage; repeating the same excursion mostly retraces the established minor loop - but every deeper excursion (magnet fully removed, steel tools across the gap) ratchets it further down. NdFeB's near-linear curve tolerates gap changes reversibly.
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For a permanent-magnet cyclotron the required PM material volume depends only on particle energy, gap height and PM working point - not on pole radius or average field - via the energy-product relation (required volume scales as (Bg*R)^2 at fixed gap), with the PM working hardest at its maximum-energy-product point.
Bg^2 ~ mu0*Bm*|Hm|*Vm/Vg (ideal); optimum working point: Bm = Br/2 and mu0*|Hm| = Br/2 on a linear demagnetization lineSource quote & editorial note
required volume of PM material depends only on particle energy, magnet gap and PM working point and doesn't depend on pole radius or average magnetic field value.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 1
Editorial note, tabletop extrapolation: Scaling law that makes a permanent-magnet follow-on build thinkable: at ~1 MeV and a 2 cm gap the required NdFeB volume is a few percent of the 1 ton needed for 10 MeV.
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Take average field as high as iron saturation allows to minimize magnet size, then split it into strong hills and weak valleys for focusing: 1.4 T average from 2.3 T hills and 0.5 T valleys in a classical 4-sector, 45-degree geometry.
<B> 1.4 T = 2.3 T hill / 0.5 T valley, 4 sectors of 45 deg, PM magnetization 1.23 T, pole dia 750 mm for 10 MeVSource quote & editorial note
To minimize weight and size of magnet system the average magnetic field value has to be high, limited by iron saturation ... average magnetic field value was chosen as 1.4 T provided of 2.3 T and 0.5 T of hill and valley region fields
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 1
Editorial note, tabletop extrapolation: A worked AVF datapoint, not a scaling law: hill/valley ratio, sector count and sector angle set flutter and tunes in a geometry-dependent way, so an 8-12 inch pole set re-derives them (FEMM plus a tune calculation) rather than copying 4.6:1 and 45 degrees. What does transfer is the design order: average field as high as iron saturation allows, then focusing from the hill/valley split - iron, not coil power, is the ceiling on a PM machine.
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Choose the hill gap from beam intensity requirements and let the valley gap follow at about 5x that: 20 mm hill gap with a 100 mm valley gap for a 10 MeV PET cyclotron.
hill gap 20 mm, valley gap 100 mm (5:1)Source quote & editorial note
As hill gap providing enough beam intensity was chosen as 20 mm and then corresponding valley gap is 100 mm.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 1
Editorial note, tabletop extrapolation: One worked ratio for a first AVF pole-tip sketch: hill gap from beam-aperture needs, valley several times deeper - re-derived for the actual field contrast and the RF/pumping geometry rather than copied. A deep valley is indeed where an amateur's Dee and pumping naturally live.
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Expect analytic/3-D calculations of average field to run a few per cent optimistic: measurement came out 5% below calculation, and the fix was reducing the valley gap from 100 mm to 70 mm while still fitting the RF cavity.
calculated <B> 5% above measured; valley gap 100 mm -> 70 mm to recover design fieldSource quote & editorial note
disagreement with calculation was found as the calculation average field value is 5 % higher than measured one ... the valley gap height was reduced from 100 mm to 70 mm
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 2
Editorial note, tabletop extrapolation: Design in adjustability - a gap or shim you can still reduce after measuring - because model-to-measurement discrepancies at the percent scale happen in either direction (this source's ran 5% optimistic). Adjustability is cheap before assembly and expensive after.
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Reach an isochronous field by iterating measurement with both pole cutting and shimming - five measure-and-machine steps were needed to converge on the design profile.
5 measure/machine steps from flat gap to isochronous <B>(r) (Fig. 4; its radial axis spans 0-36 cm)Source quote & editorial note
Average magnetic field distribution adjustment process is shown in figure 4 (last measurement is 5th step). Both cutting pole and shimming was applied to reach isochronous field. The resulting magnetic field strength is close to designed value and its shape is nearly isochronous
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 2
Editorial note, tabletop extrapolation: Budget several map-machine-remap cycles for a next machine's pole profile; the source machine took five.
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For permanent-magnet designs, allow for a gap-field temperature coefficient of about -0.07%/degC - measured on the source machine and judged acceptable there for normal cyclotron work.
dB/B ~ -0.07%/degC (measured, PM machine)Source quote & editorial note
The temperature coefficient of gap magnetic field was measured as about -0.07%/0C. Such coefficient is acceptable for normal work of cyclotron.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 2
Editorial note, tabletop extrapolation: A PM cyclotron in an unheated garage will drift off resonance with the seasons: from the quoted coefficient, a 10 degC swing is a 0.7% field change - orders of magnitude larger than the stability regulated professional machines hold (the dg-027 machine held +/-2.4 parts in 10^4).
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Eliminate the first harmonic of the field: an ion-source hole on one side only produced a first harmonic that grew radial oscillations to ~3 cm (risking the Qr-2Qz resonance), while the same field with the first harmonic removed gave <3 mm radial and <2 mm axial motion - the fix is a matching dummy hole on the opposite side.
radial oscillation 30 mm with 1st harmonic vs 3 mm without; axial 2 mm; remedy: symmetric second hole opposite the ion sourceSource quote & editorial note
Note that radial oscillations for this conditions and measured field is large enough as about 3 cm, that may lead to increasing axial oscillations through the nonlinear resonance Qr-2⋅Qz. The reason for increased radial oscillations is big first harmonic of magnetic field, which caused by non-symmetric structure of central part of cyclotron magnet ... radial oscillations now does not exceed 3 mm and axial ones does not exceed 2 mm ... to make symmetric central magnet part by setup second hole on opposite side with respect to ion source hole.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 2-3
Editorial note, tabletop extrapolation: A ten-fold reduction in orbit wander at the source machine for the cost of a symmetry-restoring second hole. For the reference machine, treat any asymmetric central feature as a first-harmonic suspect - but measure the harmonic (field mapping or orbit calculation) and choose the compensating geometry from the data; a mirror feature is not guaranteed to cancel a given perturbation.
Cited in: Beam Dynamics: An Interactive Laboratory · Beam Quality: What It Is and What Degrades It
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Dipole excitation per gap is NI = B*g/mu0, valid when iron path reluctance lambda/mu is negligible versus the gap; the exact form B_air = mu0*NI/(g + lambda/mu) shows when iron nearing saturation starts stealing amp-turns.
B_air = mu0*NI/(g + lambda/mu) ~ mu0*NI/gSource quote & editorial note
Bair = mu0 NI / (g + lambda/mu); ... Approximation ignoring iron reluctance (lambda/mu << g): NI = B g /mu0
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 25
Editorial note, tabletop extrapolation: The correction term is one contributor that bends the excitation curve at high current: comparing measured B-vs-I against the lumped formula flags when the iron starts stealing amp-turns - attributing the bend among saturation, leakage and fringing then belongs to FEMM, which the lumped model cannot do.
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Choose yoke topology by trade-off, per the lecture's comparison: C-core gives easy access but needs pole shims and is less rigid; H-core is symmetric and rigid but still shimmed; window-frame - the quoted row - has high field quality, no pole shim, symmetry and rigidity, at the price of major access problems (the C/H rows are the same slide set: scan re-read queued).
Source quote & editorial note
'Window Frame' Advantages: High quality field; No pole shim; Symmetric & rigid; Disadvantages: Major access problems.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 29, 31
Editorial note, tabletop extrapolation: Confirms the reference machine's H-frame as the right middle choice for a cyclotron (needs chamber access on both sides), with shimming accepted as part of the deal.
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Add small ferromagnetic shims at the two pole edges to compensate the finite pole width; their area and shape are tuned specifically to cancel the 6-, 10-, 14-pole error harmonics that pole symmetry allows.
shims cancel allowed harmonics n = 6, 10, 14, ... (dipole symmetry)Source quote & editorial note
The 'shim' is a small, additional piece of ferro-magnetic material added on each side of the two poles... optimised to reduce the 6, 10, 14... pole error harmonics.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 29, 37
Editorial note, tabletop extrapolation: Edge shims are how a next machine can widen its flat-field fraction without bigger poles (see dg-022 for how far short a bare flat pole falls); expect the gain to be geometry- and saturation-dependent, and verify by field mapping.
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Judge dipole field quality with the plot (By(x)-By(0))/By(0): the cited storage-ring dipole holds ~+/-1e-4 over its +/-12 mm good-field region, and its field computation is presented as whole-gap contours at +/-0.01%.
cited machine: dB/B ~ +/-1:10^4 within -12mm <= x <= +12mmSource quote & editorial note
typically +/- 1:104 within the 'good field region' of -12mm <= x <= +12 mm.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 41, 43
Editorial note, tabletop extrapolation: Sets the metric - not the number - by which the builder should present their own field maps: normalized deviation from the required field profile over the region the beam actually occupies. Derive the reference machine's tolerance from allowable RF phase slip and harmonic orbit displacement rather than adopting a generic figure; even a sub-MeV machine can be intolerant of a 1% error.
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Terminate high-field pole edges/ends with the Rogowski roll-off profile y = g/2 + (g/pi)*exp(pi*x/g - 1): it is the fastest gap increase that keeps surface flux density monotonically decreasing, i.e. no local saturation anywhere on the edge.
y = g/2 + (g/pi)*exp((pi*x/g) - 1); y = 0 is the gap centre line, and the surface asymptotes to the flat pole (y -> g/2) toward the magnet interior - the -1 inside the exponential is an x-origin shift (exp((pi*x/g)-1) = exp(pi*(x - g/pi)/g)), not an errorSource quote & editorial note
The 'Rogowski' roll-off: Equation: y = g/2 +(g/π) exp ((πx/g)-1); g/2 is dipole half gap; y = 0 is centre line of gap. This profile provides the maximum rate of increase in gap with a monotonic decrease in flux density at the surface ie no saturation
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 48-49
Editorial note, tabletop extrapolation: The mathematically graded version of the Cyclotron Kids' 45-degree chamfer; worth machining on a next machine's pole edges when field analysis predicts pole-edge flux density approaching the steel's saturation. (The 1.4 T in the source is the Diamond dipole's field, not a switch-on threshold.)
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Magnetic pressure is B^2/(2*mu0) - attractive along field lines, repulsive normal to them - and at 0.5 T it is already ~99.5 kPa = 14.4 psi, about one atmosphere pulling the poles together.
P = B^2/(2*mu0); 0.5 T -> 99,472 N/m^2 ~ 1 atmSource quote & editorial note
pressure @ 0.5T 99,472 Newton/m2... ~ 1 atmosphere
Editorial note, tabletop extrapolation: At the reference machine's 0.59 T the poles attract with ~1.4 atm over the 8-inch pole face — about 4,500 N (~1,000 lbf); clamps and any pole-retraction scheme must carry that load (chamber lids carry the separate atmospheric load — see the lid-deflection calculator). [Corrected 2026-08-20: previously printed as "~4500 lbf", the newton value mislabeled.]
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Estimate magnet stored energy as U = B^2/(2*mu0) * (gap volume) and coil inductance as L_coil = 2U/I^2; the ramping voltage needed is V ~ B0*N*a*L/dt with L the magnet length (the source's own symbol), so turn count N is the only free knob for matching a power supply once field, gap, and ramp time are fixed.
U = B^2/(2*mu0)*V_gap; L_coil = 2U/I^2; V = B0*N*a*L/dt + I*R (a = pole width, L = magnet length)Source quote & editorial note
Given the field = B0, pole width = a, Magnet Length = L and ramp time dt, the only design option available for changing the voltage is the number of turns, N.
Editorial note, tabletop extrapolation: Quick check on a next machine's supply matching: stored energy in a 10-inch, 1 T, 5 cm gap magnet is about 1 kJ from the gap alone (B^2/(2*mu0) x volume; fringe fields add more), and turn count trades current for voltage against whatever surplus supply the builder finds.
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Where return-yoke saturation contributes to leakage, make the yoke and return legs thick: the leaked field scales with (B_iron/mu) of the return path, so an unsaturated fat yoke leaks less. The source states this for a septum magnet's return path; pole-gap fringe and coil-end fields are separate contributions this does not address.
B_fringe ~ (B_iron/mu) * (L_iron/L_fringe)Source quote & editorial note
This reduction is accomplished by reducing the saturation by making the yoke and back leg of the septum magnet as thick as possible.
Editorial note, tabletop extrapolation: Supports generous H-frame cross-section on the next machine, but the return path is only one leakage source - model or map the stray field before siting ion gauges, turbo pumps and CRT-era instruments near the magnet.
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The 3-D fringe field of an unchamfered dipole is longest at the pole center and shorter at the edges (roughly quadratic across the pole), so its integrated error looks like a sextupole; SPEAR3 reduced it with a chamfer whose depth profile was determined empirically and was approximately parabolic, prototyped on a removable machined insert.
fringe length ~ h at pole end, varying ~quadratically across widthSource quote & editorial note
the fringe field is longer at the center of the magnet and drops off near the edges. This distribution is approximately quadratic and the integrated multipole field looks like a sextupole field. ... a removable insert with a machined chamfer installed on the SPEAR3 prototype gradient magnet. ... The shape of the chamfer depth was determined empirically and was approximately parabolic. It was designed to reduce the integrated sextupole field.
Editorial note, tabletop extrapolation: Mostly relevant if the builder adds edge shaping for extraction: expect the field falloff at the pole rim to vary azimuthally with any non-axisymmetric pole feature, and fix it empirically with removable machined inserts.
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Generate the geometry point list in a spreadsheet (CONCATENATE the x,y columns into '$po x=..., y=...$' lines) rather than typing the deck by hand - the source shows the exact cell formula - and be aware POISSON's mesher is weak for detailed geometry.
Source quote & editorial note
the meshing package for POISSON is rather weak and often does not have the flexibility nor is robust enough to generate difficult detailed meshes easily. ... I find it easier to develop the geometry lattice using the Excel. ... =CONCATENATE(C$1,A5,C$2,B5,C$3)
Tanabe, Iron Dominated Electromagnets, Lecture 4: POISSON — A Two-Dimensional Magnetostatic Solver (2005) — p. 10, 19
Editorial note, tabletop extrapolation: Saves hours on shim-profile studies where dozens of geometry variants are compared; also justifies using FEMM instead for fiddly shim shapes.
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Use the free, LANL-maintained POISSON/PANDIRA/AUTOMESH/WFSPLOT chain for 2-D magnet cross-sections - the lecture's tour: AUTOMESH builds the mesh from a text file, POISSON relaxes the vector potential (PANDIRA for permanent-magnet and anisotropic problems), WFSPLOT draws geometry and equipotentials (component details per the lecture: scan re-read queued).
workflow: .am text file -> AUTOMESH -> Tape35 -> POISSON or PANDIRA -> WFSPLOT / OUTPOISource quote & editorial note
It is a public access code (it's free), maintained under contract with DOE by Los Alamos National Accelerator Laboratory (LANL) personnel.
Editorial note, tabletop extrapolation: Free tooling that runs on a PC, in the same code family the Houghton-line theses used (dg-142) - the standard amateur path to pole-profile design alongside FEMM.
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Request a harmonic (Fourier) edit on a circle inside the good field region rather than eyeballing contours: e.g. ktype=121, nptc=31 points, rint=20 mm interpolation radius, rnorm=25 mm normalization, nterm=14 multipole terms.
ktype=121, nptc=31, rint=20 mm, rnorm=25 mm, angle=90, nterm=14Source quote & editorial note
nptc=31 means number of points on the circle, rint=20 means interpolation on 20 mm radius arc, rnorm=25 means multipole normalization at 25 mm ... nterm=14 means the maximum number of multipole terms.
Editorial note, tabletop extrapolation: Turns a simulation into the same harmonic numbers you get from a measured field map, so simulation and Hall-probe map can be compared directly.
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Exploit symmetry with the boundary condition flags nbsup/nbslo/nbsrt/nbslf, where 0 = Dirichlet (flux parallel) and 1 = Neumann (flux perpendicular); putting a Neumann condition on the median plane lets you model only half (or a quarter) of the magnet.
nbsup, nbslo, nbsrt, nbslf: 0 = Dirichlet (flux parallel), 1 = Neumann (flux perpendicular)Source quote & editorial note
nbsup, nbslo, nbsrt and nbslf means the boundary condition at the upper, lower, right hand, and left hand boundaries. = 0 means Dirichlet (flux parallel) and =1 means Neumann (flux perpendicular) boundaries.
Editorial note, tabletop extrapolation: For the symmetric H-frame cross-section, a median-plane symmetry boundary halves the modeled domain and mesh - runtime usually falls accordingly, though not by an exact factor; a quarter model needs a second valid symmetry plane (geometry AND excitation symmetric about both).
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In a POISSON input deck, mat=1 is air/vacuum and mat=2 uses the built-in BH curve of a generic iron approximating 1010 steel - suitable for preliminary mild-steel yoke studies when the actual steel's BH data are unavailable.
mat=1 air; mat=2 iron (generic BH ~ 1010 steel); mode=0 selects finite permeability from a tableSource quote & editorial note
The iron yoke area uses mat=2, which uses the BH curve for a 'generic' iron whose magnetic properties approximate the behavior of 1010 steel.
Editorial note, tabletop extrapolation: Home-built yokes are typically A36/1018 mild steel; the default curve is a reasonable first pass, but A36 properties vary - run sensitivity checks with plausible BH curves (or supplier/measured data) before trusting predictions near saturation.
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Define coil regions by a closed polygon with cur = total ampere-turns (sign sets flux direction: negative current in the right-hand coil gives positive flux on the horizontal centerline); every region polygon must close, first point equal to last.
$reg mat=1 cur=-20000$ for a 20,000 A-turn coil block; all $po ... $ region polygons must closeSource quote & editorial note
Note that all regions must close, that is the first and last coordinates are equal ... Negative currents in the right hand coil gives positive flux on the horizontal centerline.
Editorial note, tabletop extrapolation: The two mistakes that make a first POISSON run fail; also shows amp-turns (not turns and amps separately) are what the model needs.
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Compute dipole excitation as NI = B*h/mu0 divided by an efficiency of about 0.98 - a well-designed iron yoke eats only ~2% of the MMF.
NI = B0*h/(mu0*eta), eta ~ 0.98Source quote & editorial note
efficiency ~ 0.98 For magnets with well designed yokes.
Tanabe, Iron Dominated Electromagnets, Lecture 6: Excitation, Coil Design, System Design and Water Flow (2005) — p. 4-6, 12
Editorial note, tabletop extrapolation: Lets the builder size a next machine's amp-turns by hand before any FEA - with the ~2% read correctly: it is the yoke's MMF consumption in a well-designed magnet, not the accuracy of the estimate. Saturation, the real B-H curve, leakage and geometry can move the answer by far more than 2%, which is what the FEMM pass is for.
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If a core is glued or laminated, electrically bond all laminations with a small weld bead and ground the core at a single point to avoid floating/looping ground paths.
Source quote & editorial note
It is necessary to add a small weld bead, electrically connecting all the laminations. The core can then be grounded to a single ground point.
Editorial note, tabletop extrapolation: Single-point grounding of the yoke also matters on a solid-core machine carrying RF and HV nearby - one deliberate ground, no accidental loops.
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Never route the magnet's electrical bus so the supply conductors form a loop around the beam path - the loop makes a stray solenoidal field that rotates the beam; run feed and return conductors close together.
Source quote & editorial note
The electrical bussing connection creates a loop around the beam line, resulting in a small solenoidal field... the in and out conductors should be placed close to each other.
Editorial note, tabletop extrapolation: Cheap to get right on a next machine: dress the coil leads as a twisted/adjacent pair and keep supply cables from encircling the chamber.
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Accelerator magnet alignment norms (Tanabe): hold transverse and vertical position to about +/-250 um and longitudinal to +/-500 um - and plan alignment provisions from the start, because the cost of retrofit is high.
+/-250 um transverse/vertical; +/-500 um longitudinal (the rotational tolerance figure was uncited - removed pending re-read)Source quote & editorial note
Magnet alignment specifications... typically call for < +250 um precision transversely and vertically and < +500 um longitudinally... The cost of retrofit is high.
Editorial note, tabletop extrapolation: For a single-magnet cyclotron the numbers relax, but the lesson holds: machine reference flats and leveling features into the next machine's yoke before assembly.
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Support a magnet kinematically with exactly six linearly independent constraints (six-strut or three-block scheme): three vertical (y, pitch, roll), two longitudinal (z, yaw), one transverse (x) - more supports overconstrain, fewer underconstrain.
6 supports = 3 vertical + 2 longitudinal + 1 transverseSource quote & editorial note
A true kinematic support system must have at least and at most six linearly independent supports.
Editorial note, tabletop extrapolation: A next machine's stand with three adjustable feet plus lateral stops gives repeatable leveling of the median plane without fighting a warped frame.
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For a DC magnet with a simple flat pole contour, a solid machined core is appropriate; choose laminations only for time-varying fields or when magnet-to-magnet reproducibility across a family matters (lamination economics: ~$50k die set, ~$1/lamination, 2-4 man-days stacking per core).
die set ~50 k$; ~$1/lamination; 2-4 man-days/core assemblySource quote & editorial note
Solid iron yokes are often used in simple, flat pole contour magnets.
Editorial note, tabletop extrapolation: Settles the default for a next machine: a one-off DC cyclotron magnet is normally solid steel - the source's 'often used' practice - because lamination tooling only pays across a production family. Laminations re-enter if the design ramps or regulates fast enough for eddy currents to matter (dg-089).
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Iron B-H properties vary with chemistry from heat to heat, carbon dominating - the quote; the lecture's practical corollaries (variation with position in the pour and rolling direction; ordering non-oriented steel; same-heat purchasing) accompany it in its discussion (scan re-read queued).
Source quote & editorial note
The BH characteristics of iron are variable and depend on the chemistry of the iron (dominated by the Carbon content, which is highly variable from heat to heat).
Editorial note, tabletop extrapolation: Practical purchasing rule: buy a next machine's pole and yoke stock as one lot from one heat where possible - and treat mixed-source top/bottom iron as a candidate cause if the median plane comes out asymmetric (a dg-138-class symptom).
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Cover or tape coils against personnel contact whenever I*V > 150 VA, or I > 30 A, or V > 130 V, or stored magnetic energy > 5 J; ground every core, and attach removable cover sections with at least four screws.
thresholds: 150 VA, 30 A, 130 V, 5 J stored energySource quote & editorial note
IV > 150 V-Amperes or I > 30 Amps or V > 130 Volts or when the magnet stored energy is > 5 joules.
Editorial note, tabletop extrapolation: The reference machine's magnet exceeds several of these thresholds, so the source's guarding rule applies: a sheet-metal or polycarbonate coil cover including the hot cooling fittings. Guarding is one layer only - protective earthing, overcurrent protection, and stored-energy discharge are separate requirements this rule does not cover.
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Set the isochronous field correction from the measured orbital-frequency error using dB(r)/B(r) = gamma(r)^2 * df_p(r)/f_p(r); converting the required dB/B into actual shim geometry then needs a magnetic model or a calibrated shim-response measurement.
dB(r)/B(r) = gamma(r)^2 * df_p(r)/f_p(r)Source quote & editorial note
Shimming of pole edges or shims based on equation: dB(r)/B(r) = gamma(r)^2 * df_p(r)/f_p(r)
Zaremba, Magnets for Cyclotrons (2005) — p. 10
Editorial note, tabletop extrapolation: For protons from ~150 keV to 1 MeV, gamma is about 1.00016-1.00107. Relate the reference machine's measured phase slip to a local orbital-frequency error first, then use the formula for the required field correction, and get shim thickness from simulation or measured shim sensitivity - relativistic effects are small at these energies but not automatically subdominant to mechanical field errors.
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Start every cyclotron magnet from the rigidity relation B*rho = sqrt(T^2 + 2*T*E0)/(300*Z) (B in tesla, rho in m, T and rest energy E0 in MeV) to fix the field-radius product before any geometry is drawn.
B*rho = sqrt(T^2 + 2*T*E0)/(300*Z)Source quote & editorial note
The maximum kinetic energy T determines magnetic rigidity: B*rho = sqrt(T^2+2T*E0)/(300*Z)
Zaremba, Magnets for Cyclotrons (2005) — p. 19
Editorial note, tabletop extrapolation: For 1 MeV protons B*rho = 0.145 T*m: at 1 T that is a 14.5 cm final orbit radius, which immediately sizes the next machine's pole diameter (with overhang and fringe allowances added).
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Choose the pole gap as a compromise: a small gap cuts the ampere-turns and lets orbits run close to the pole edge, while a large gap buys space for ion source, probes, and easier vacuum pumping at the price of field and power.
Source quote & editorial note
small gap: reduced number of At of coils, pole radius reduced, orbits close to outer edge; large gap: large space: injection, extraction, probes, easier vacuum pumping
Zaremba, Magnets for Cyclotrons (2005) — p. 22
Editorial note, tabletop extrapolation: Frames the central tradeoff for a next machine: shrinking the gap raises B at fixed ampere-turns while the iron stays unsaturated (dg-021's measured case shows the ideal 1/g is an upper bound) - and everything (dee aperture, ion source, probes) must still fit and pump through the smaller gap.
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Before freezing magnet geometry, check the design against every subsystem it must host: RF system, vacuum pumping, ion source/injection, extraction or internal target, and diagnostic probes.
Source quote & editorial note
Cyclotron magnet design should always consider interaction with subsystems: RF system, vacuum pumping, ion source or injection system, extraction system or internal target, diagnostic probes.
Zaremba, Magnets for Cyclotrons (2005) — p. 3, 45
Editorial note, tabletop extrapolation: A magnet that works but leaves no port for the probe or the pump is a classic amateur trap - exactly what this five-item checklist exists to prevent; run it on every layout iteration for a next machine.
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Do first-pass cyclotron magnet numbers analytically with the lecture's formula set: average field <B> = alpha*B_hill + (1-alpha)*B_valley (alpha = pole azimuthal fraction), flutter F = alpha(1-alpha)(B_hill-B_valley)^2/<B>^2, total flux Phi = B_hill*S_poles (a hard-edge estimate that neglects the valley contribution), NI from Ampere's law, and coil cooling dT(C) = 60*P(kW)/(4.19*N(l/min)).
dT(C) = 60*P(kW)/(4.19*N(l/min)); F = alpha(1-alpha)(Bh-Bv)^2/<B>^2Source quote & editorial note
coil cooling estimation: dT(C) = 60*P(kW)/(4.19*N(l/min))
Zaremba, Magnets for Cyclotrons (2005) — p. 30-32
Editorial note, tabletop extrapolation: The cooling formula is immediately usable: a next machine's 5 kW coil at 4 L/min runs ~18 C water rise; the flutter formulas matter only if the builder adds sector (AVF) pole faces.
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If using sectored (AVF) poles, a hill fraction k = 0.5 gives best RF efficiency (most valley room for dees); increase toward k ~ 0.67 (60-degree hills) only to shrink machine diameter, and design to a vertical tune around nu_z ~ 0.2.
k = hill angle/period; k=0.5 best for RF, IBA chose k=0.67, nu_z ~ 0.2Source quote & editorial note
For best RF efficiency, k=0.5 BUT to decrease machine dimensions k >0.5 (more hill, thus more field) CHOICE : k=0.67 (60 deg hills)... CHOICE : nu_z = 0.2
Zaremba, Magnets for Cyclotrons (2005) — p. 32-33
Editorial note, tabletop extrapolation: If a next machine goes AVF to escape the weak-focusing energy ceiling, IBA's documented choices are a starting point, not proven tabletop values: k between 0.5 (best RF room) and 0.67 (compactness), and a modest vertical-tune target like their nu_z = 0.2 - each re-derived for the actual geometry, since a 60-degree hill only gives k = 0.67 in their sector periodicity, and sector count and valley usage carry their own trades.
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Follow the iterative magnet design loop: rough model, hand calculations, 2-D field code, then 3-D field code - and a good 3-D model agreed with measurement to better than 3% in the source's experience.
3-D calculation vs measurement < 3%Source quote & editorial note
calculation results and measurements differ less than 3 percent
Zaremba, Magnets for Cyclotrons (2005) — p. 4, 35
Editorial note, tabletop extrapolation: The reference machine's Poisson/FEMM workflow is the professional one. Treat ~3% as the achievable-agreement benchmark rather than a diagnostic razor: a larger mismatch means something is wrong - model geometry or BH data, but equally possibly Hall-probe calibration, positioning, excitation error, or remanence - so check the measurement chain alongside the model before rebuilding either.
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Target field homogeneity of dB/B <= 0.01% over a dipole's good-field region - 'reasonable but nevertheless challenging' in the source's assessment.
dipole: (By(x,y)-By(0,0))/By(0,0) <= 0.01% (the quadrupole-gradient figure was uncited - removed pending re-read)Source quote & editorial note
Achieving the following homogeneity values is reasonable but nevertheless challenging. Dipole: dB/B0 <= 0.01%
Editorial note, tabletop extrapolation: A useful upper bar from beamline practice. A weak-focusing cyclotron deliberately wants a controlled radial gradient, and its azimuthal tolerance is a different quantity: specify it as Fourier-harmonic limits (especially the first harmonic) derived from orbit-error analysis, using 0.01% only as a sense of what precision magnets achieve.
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Build the aperture budget as: good field region + vacuum chamber wall (0.3-2 mm) + installation/alignment margin (0-5 mm), with the paper allowing a further 5-10 mm within the good field region for closed-orbit distortion.
aperture = GFR + chamber wall (0.3-2 mm) + margin (0-5 mm); GFR includes 5-10 mm closed-orbit allowanceSource quote & editorial note
The total required aperture size is the sum of the good field region, the vacuum chamber thickness (0.3-2 mm) and a margin for installation and alignment (0-5 mm).
Editorial note, tabletop extrapolation: Explains why the pole gap exceeds the chamber's internal height by several millimetres once walls and margins stack - sum the budget's terms in a consistent full-gap or half-gap convention rather than quoting a round figure, since mixing conventions double-counts the allowances.
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Compute the required excitation directly from the gap: NI per pole = B*h/(2*eta*mu0), with efficiency eta typically 99% for a well-designed iron circuit - pole area does not enter the ideal term - and the source's own warning kept: the equation is approximate, neglecting fringe fields and iron saturation.
NI_per_pole = B*h/(2*eta*mu0); eta ~ 0.99; mu0 = 4*pi*1e-7Source quote & editorial note
where h is the magnet gap height in [m] ... eta is the efficiency (typically 99%), mu_0 is the permeability of free space ... Note that Eq. (5) is only approximate and neglects fringe fields and iron saturation.
Editorial note, tabletop extrapolation: First-cut sizing for a next machine: at a 2 cm gap and 1.0 T, ~8000 A-turns per pole sets conductor and current-density scale before any FEMM run - the floor that FEMM then corrects for fringe and saturation.
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Size the iron so flux density in the yoke stays below 1.5 T and yoke reluctance stays a small fraction (about 1%) of gap reluctance - with areas in the comparison, R_iron/R_gap = [lambda/(mu_r*A_iron)] / [h/A_gap] - and circuit efficiency exceeds 99% in the source's practice.
B_iron < 1.5 T; lambda/(mu_r*A_iron) << h/A_gap (the source's length-only form assumes comparable areas); eta > 99% when both holdSource quote & editorial note
It is good practice to keep the iron yoke reluctance smaller than a few per cent of air reluctance ... such that the magnetic flux in the iron remains smaller than 1.5 T ... the efficiency is better than 99%.
Editorial note, tabletop extrapolation: The single most useful yoke-sizing rule for an H-frame homebuilt magnet: pick return-leg area with margin beyond flux/1.5 T - equality puts the iron AT the 1.5 T line, not under it - and verify the narrowest return section in FEMM, because that section sets the circuit's behavior.
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Approximate the magnetic (effective) length as l_mag = l_iron + 2*h*k with k between 0.3 and 0.6 - and, per the quote, a precise k comes only from measurement or numerical calculation; the lecture's qualitative guidance on when k shrinks (narrow poles, saturation, close coil heads) accompanies the formula (scan re-read queued).
l_mag = l_iron + 2 h k, k = 0.3-0.6Source quote & editorial note
l_mag = l_iron + 2hk ... Typical values of k are between 0.3 and 0.6. A precise determination of k is only possible with measurements or numerical calculations.
Editorial note, tabletop extrapolation: Quantifies the fringe-field bulge at the pole edge - the region where a tabletop cyclotron's outermost orbits actually live.
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Estimate the total flux the return yoke must carry as Phi = B_gap * (w + 2h) * l_mag, where w is pole width and h the gap - i.e. add one gap-height of stray flux on each side of the pole.
Phi ~= B_gap (w + 2h) l_magSource quote & editorial note
Total flux in the return yoke is Phi = integral B da ~= B_gap (w + 2h) l_mag ... where h is the gap height and w the pole width.
Editorial note, tabletop extrapolation: For an 8-inch pole with a 1-inch gap this says design the yoke for ~25% more flux than the naive pole-area estimate.
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Estimate stored energy (hence inductance L = 2U/I^2 and supply voltage) for a simple gap magnet as U = B^2/(2mu0) * (V_gap + 2*V_coil/6 + V_yoke/mu_r).
U_magnet = B^2/(2 mu0)*(V_gap + 2*V_coil/6 + V_yoke/mu_r); energy-equivalent L = 2U/I^2 (valid for a near-linear circuit - near saturation the ramp voltage follows d(flux linkage)/dt, not this L); V_tot = R*I + L*dI/dtSource quote & editorial note
U_magnet = U_gap + 2 U_coil + U_yoke = B^2/(2 mu_0) (V_gap + 2 V_coil/6 + (1/mu_r) V_yoke)
Editorial note, tabletop extrapolation: Tells you the inductance scale and therefore how fast a bench supply can ramp the magnet and how big the flyback/dump protection must be (dg-218) - computing the protection against the worst-case inductance across the operating range, not the single linear figure.
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Choose magnet topology by field quality, per the lecture: the window-frame design provides a very homogeneous field even without shims (the quote), while a dipole C-magnet TYPICALLY produces a ~0.1% gradient across the pole with even harmonics; the lecture's H/C weight and shim comparisons sit alongside (scan re-read queued).
C-magnet: ~0.1% gradient across pole vs central field, harmonics n = 2,4,6Source quote & editorial note
Typically, the dipole produces a gradient across the pole of 0.1% with respect to the central field ... the window-frame design provides a very homogenous field quality even without shims.
Editorial note, tabletop extrapolation: Validates the reference machine's H-frame choice for a cyclotron (two-fold symmetry, lighter than a C) and warns that shimming will still be needed.
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For yoke steel use cold-rolled non-grain-oriented electro-steel (EN 10106) with sheet 0.3-1.5 mm, coercivity Hc < 65 A/m (spread < +/-10 A/m); solid yokes are unsuited to fast cycling - eddy currents lag and heat them, though slow ramps are fine - and, if used, all parts should come from the same melt for reproducibility.
sheet 0.3-1.5 mm; density 7.60-7.85 kg/dm3; Hc < 65 A/m; dHc < +/-10 A/m; resistivity 0.16-0.61 uOhm*mSource quote & editorial note
Sheet thickness 0.3 <= t <= 1.5 mm ... Coercivity Hc < 65 A/m ... Coercivity spread dHc < +/- 10 A/m
Editorial note, tabletop extrapolation: For a DC cyclotron magnet solid mild steel is fine, but this gives the numeric target for 'good' steel and explains why scrap-plate yokes vary.
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Cycle the magnet through the same excitation loop to its standard maximum value - chosen within the coil and supply's electrical and thermal ratings - before settling at the operating field, whatever field you need, so hysteresis and remanence effects are reproducible; approach the operating point along the same branch every time.
Source quote & editorial note
In normal operation, the magnet is always cycled to its maximum value, irrespective of the required field, to ensure that hysteresis effects are reproducible.
Editorial note, tabletop extrapolation: Free operational fix for run-to-run field shifts in a home cyclotron: resonance is set by B, so reproducibility matters directly - how much field error the beam tolerates depends on RF voltage, turn count and acceptance, so measure it rather than assume. If true zero field is needed, degauss with diminishing alternating cycles instead of trusting zero current.
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Estimate the mean turn length as l_avg = pole perimeter + 8 x (clearance between pole and coil) + 4 x coil width - the quoted formula; the lecture's sanity band 2.5*l_iron < l_avg < 3*l_iron (l_iron the iron core length) is its companion check for racetrack geometry (scan re-read queued).
l_avg = pole perimeter + 8*clearance + 4*coil width; 2.5 l_iron < l_avg < 3 l_ironSource quote & editorial note
l_avg = pole perimeter + 8 x clearance between pole and coil + 4 x coil width
Editorial note, tabletop extrapolation: Gives copper length, hence resistance and power, straight off a sketch - exactly what a garage builder needs before ordering tubing.
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Pick current density from the cooling method and coil geometry: at most 1 A/mm^2 for voluminous coils almost entirely enclosed in the yoke, up to ~2 A/mm^2 only for small thin well-exposed air-cooled coils, and up to ~10 A/mm^2 as the typical upper end for direct water-cooled hollow conductor - higher is possible but at the cost of reliability.
air (bulky, enclosed): j <= 1 A/mm^2; air (small, thin): j < 2 A/mm^2; water-cooled: j up to ~10 A/mm^2 (typical upper end)Source quote & editorial note
the maximum current density for voluminous coils which are almost entirely enclosed in the magnet yoke should not exceed 1 A/mm2 ... The current density in direct water-cooled coils can be typically as high as 10 A/mm2.
Zickler, Basic Design and Engineering of Normal-Conducting, Iron-Dominated Electromagnets — arXiv:1103.1119 (2010) — p. 28-29, 31
Editorial note, tabletop extrapolation: The reference machine's 538-turn solid copper tubing coils sit in the air-cooled regime; unless they qualify as small and thin enough to shed heat (the source's 2 A/mm^2 case), the quoted limit for enclosed coils is 1 A/mm^2 - going higher means hollow conductor with water flow.
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Design water cooling to keep coolant velocity turbulent but below 5 m/s (Re > 4000), coil surface below 60 C, and water temperature rise <= 30 C from a 30 C inlet, with 0.1-1.0 MPa (1-10 bar) available pressure drop.
u_avg <= 5 m/s; Re > 4000; dT <= 30 C; T_surface < 60 C; dp = 0.1-1.0 MPaSource quote & editorial note
The velocity of the cooling medium ... should be sufficiently high to guarantee a turbulent flow but low enough (u_avg <= 5 m/s) to avoid erosion and vibration. A maximum permitted temperature of less than 60 C on the coil surfaces was found to be good practice.
Editorial note, tabletop extrapolation: Hard numbers for a home chilled-water loop as DESIGN limits, not damage cliffs: hold velocity under ~5 m/s (erosion and vibration risk grow beyond it), coil surfaces under 60 C (insulation aging accelerates with temperature), and note the arithmetic - a 30 C inlet plus 30 C rise means up to 60 C outlet water, consistent with the surface limit but tight in a hot garage: derate for your ambient.
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Use the closed-form water-cooling recipe in the source's units throughout: flow Q[l/s] = 2.388e-4 * P/dT, temperature rise dT = 3.04e-7 * P/(u_avg d^2), and required bore d = 5.59e-3 * (P/(dT*Kw))^0.368 * (l/dp)^0.21, with Kw as defined in the source.
Q = 2.388e-4 P/dT; dT = 3.04e-7 P/(u d^2); d = 5.59e-3 (P/(dT Kw))^0.368 (l/dp)^0.21; u_avg = 0.3926 d^0.714 (dp/l)^0.57 - coefficient-based, unit-specific: convert every input to the source's units before useSource quote & editorial note
Q_water = 2.388 x 10^-4 P/dT ... d = 5.59 x 10^-3 (P/(dT Kw))^0.368 (l/dp)^0.21
Editorial note, tabletop extrapolation: Lets the builder compute the hollow-conductor bore and pump requirement for a next machine's 5-20 kW magnet with a spreadsheet, no CFD - provided every input is converted to the source's units first: a bar-for-pascal slip in the pressure drop moves the bore answer far more than the recipe's real margin.
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Compute dipole excitation as NI = B*h/(eta*mu0) with magnet efficiency eta ~= 98% for a well-designed unsaturated yoke (the iron path costs only ~1-2% extra ampere-turns when mu_iron >= 1000 and L_iron <= 10h).
NI_dipole = B*h/(eta*mu0), eta ~ 0.98Source quote & editorial note
NI_dipole = Bh/(eta*mu0), where the magnet efficiency, eta... The magnet efficiency for a well designed yoke is eta >= 98%.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 116-117, 129
Editorial note, tabletop extrapolation: One-line check of the reference machine's 538 turns: at 0.59 T and its gap the formula predicts the required current within a couple percent if the H-frame iron is unsaturated. A measured efficiency well below the formula's ~98% says the model is missing something - saturation, leakage, a parasitic joint gap, or a wrong effective-gap value - and FEMM sorts out which.
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Choose low-carbon magnet steel (the 1010 class, carbon near or below 0.10%); its BH curve becomes highly nonlinear above B ~ 1.5 T and shows fully saturated behavior by B ~ 2.0 T - incremental permeability falling toward mu0 while B still creeps up with H - so keep working iron flux density below ~1.5 T for linear, reproducible excitation.
1010-class steel: nonlinear B >= 1.5 T; fully saturated behavior B >= 2.0 T (incremental mu -> mu0; B does not stop rising)Source quote & editorial note
The BH relationship becomes highly nonlinear at B >= 1.5 Tesla and the material exhibits fully saturated behavior at B >= 2.0 Tesla.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 249-251
Editorial note, tabletop extrapolation: Sets the iron budget for the next machine: yoke and pole cross-sections should be sized so flux density stays under ~1.5 T anywhere on the return path, and pole-tip fields much above 1.8 T are not worth chasing with iron.
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Good 2-D dipole practice: taper the pole so it is wider at the root, use a wide coil slot rather than a narrow one, and put a radius on the pole corner - the source credits these with keeping the field uniform and the excitation linear over a wider range.
Source quote & editorial note
At high fields, the top of the pole can saturate. The right hand figure illustrates a tapered pole which is wider at the top... The right hand figure illustrates a wider coil with approximately the same area and a higher reluctance path and a lower transverse field due to both the wider coil slot and the tapered pole edge. ... a radius at the pole corner, reducing this magnetic flux stress concentration. ... The results of the listed improvements in the two dimensional design are magnets whose field remains uniform and whose excitation remains linear over a wider range of excitation.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 251-252
Editorial note, tabletop extrapolation: Cheap insurance for the next machine's pole design: a root taper and corner radius cost one lathe operation and help keep the field shape constant over a wider excitation range.
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Assume the fringe field extends about one half-gap h beyond the steel pole edge of a dipole (h/2 for a quadrupole of pole radius h); the pole steel therefore ends about one half-gap inside where the field effectively ends.
L_fringe ~ h (dipole), ~h/2 (quad), ~h/3 (sextupole)Source quote & editorial note
A general rule of thumb is that the length of the fringe field beyond the edge of the steel pole tip is = h, = h/2, or = h/3, for the dipole, quadrupole or sextupole
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 252-253
Editorial note, tabletop extrapolation: Tells the builder where usable field really stops on an 8-inch pole: the fringe extends about one half-gap BEYOND the steel edge before dying away, while the flat, usable region ends somewhat inside the pole radius as the falloff begins. Map B(r) (FEMM, then Hall probe) to place the maximum stable orbit; the h rule sizes how much radial real estate the fringe transition consumes.
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When end-chamfering poles to fix the integrated field, machine the depth distribution computed from the measured field integral; the cut angle itself is unimportant - 45 degrees is convenient because it splits the corner into two equal half-angles and minimizes local saturation. SPEAR3 did this on bolted-on steel end pieces, remachining after measurement, and reached the final shape in two iterations.
chamfer depth Delta-z(x) from measured Leff(x); cut angle 45 degSource quote & editorial note
The angle of the cut is unimportant. However, a 45 degree angle cut is convenient and distributes the same angle at two points and minimizes saturation effects due to the sharp corners. ... solid steel pieces, machined with the two dimensional pole contour, were bolted onto the pole ends. These pieces were removed, machined with the required distribution of the chamfer depth determined by the described iterative process and replaced. After replacement, the distribution of the field integral was measured. The final chamfer shape was achieved after two iterations.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 253-254
Editorial note, tabletop extrapolation: If the next machine's pole edge is chamfered or radiused to soften the field falloff for extraction - a different geometry and objective than a dipole end chamfer, so model or map it for the cyclotron case - use bolt-on machinable end pieces so the shape can be iterated the way SPEAR3 did.
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Improve dipole field flatness by adding smooth bumps (shims) near the pole edges; the bumps squeeze flux through a locally narrower gap, make the flow lines go horizontal earlier - increasing the fraction of the aperture with uniform field - and reduce flux crowding and saturation at the pole corner.
Source quote & editorial note
the field quality can be improved by adding smooth bumps near the edge of the pole, causing the flow lines to squeeze through a narrower gap and causing them to transition earlier to horizontal lines. This increases the fraction of the aperture with uniform field distribution. The smooth bumps also reduce the crowding of the flow and flux lines near the pole corner, reducing the saturation of the iron in this region.
Editorial note, tabletop extrapolation: The classic Rose-shim trick: a machined or stacked-shim ring at the edge of the 8 inch poles buys field uniformity (and hence more usable radius) far more cheaply than a bigger magnet.
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Size dipole pole width by adding pole overhang beyond the good-field region: for an optimized (edge-bumped) pole, overhang a = h*(-0.14*ln(dB/B) - 0.25); for a flat unoptimized pole, a = h*(-0.36*ln(dB/B) - 0.90), where h is the half gap.
x=a/h; optimized: dB/B=(1/100)exp[-7.17(x-0.39)]; unoptimized: dB/B=(1/100)exp[-2.77(x-0.75)]Source quote & editorial note
The canonical expressions... are used to estimate the amount of pole overhang required to achieve a desired field quality... for both unoptimized and optimized pole contours.
Editorial note, tabletop extrapolation: Directly sizes how much of the reference machine's 8-12 inch pole diameter is usable good field; e.g. for dB/B=1e-3 an unoptimized pole needs ~1.6 half-gaps of extra pole beyond the outermost useful orbit.
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Plain radial-sector pole tips fared worst in the Rutgers 12-inch mapping campaign: the steepest average-field falloff with radius - unusable in their assessment - while spiral sectors compromised between usable average field and roughly triple the weak-focusing axial tune.
weak focusing: flattest <B>(r); radial sector: largest falloff (unusable); spiral sector: intermediate, ~3x weak-focus nu_z at small radiiSource quote & editorial note
the radial sector poletips have the greatest average falloff - so great that it amounts to be an unusable field. The spiral sector AVF field is a compromise between the two.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 10
Editorial note, tabletop extrapolation: Direct guidance for a next machine's pole-tip upgrade at the 8-12 inch scale, as a measured comparison among these candidates rather than a ban: radial-sector AVF machines exist, but making one work takes sector-angle and profile design these candidates did not carry. Also warns that narrow spiral vanes saturate at large radius - the measured field fell below simulation there.
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Screen candidate pole-tip designs with two numbers from the 2-D map - average field vs radius (isochronism) and axial tune from nu_z^2 = n + F^2*N^2/(N^2-1), the straight-sector smooth approximation - and reserve full phase-space tracking for the final one or two contenders.
nu_z^2 ~= n + F^2*N^2/(N^2-1) (smooth approximation, straight sectors; spiral sectors add a (1+2tan^2 xi) factor; check the flutter definition in use before substituting)Source quote & editorial note
this analysis approach can be used to quickly assess a field during design, relegating the laborious task of phase space mapping and determining the limits of stability to the few the final contenders.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 10-11
Editorial note, tabletop extrapolation: A cheap, quantitative design filter that works from measured maps of a home-built magnet, no orbit code required.
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Build the mapping stage around a fine leadscrew drive - the source's stage works out to 800 steps per inch - run the steppers gently (the source used 25% of rated current, with velocity ramp-up/ramp-down to prevent skipping), and take readings only while moving in the forward direction to minimize backlash effects.
800 steps/inch aggregate (200 steps/rev motors, 5/16-8 two-start leadscrew); stage run at 25% rated motor currentSource quote & editorial note
T304 stainless steel 5/16-8 double lead (2 start) thread with 0.25-inch pitch ... Astrosyn Type 23KM-K213-P7V stepper motors that advance 1.8 degrees per step. A ramp-up and ramp down of velocity prevents skipping. Since the load on the x-y stage is low, the stepper motors are only required to run at 25% their rated operating maximum current. The aggregate of lead screw pitch and motor resolution correlates to 800 steps per inch. To further minimize the potential for backlash, field measurements are only made while stages are moving in the 'forward' direction.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 2
Editorial note, tabletop extrapolation: A stage resolving 1/800 inch (0.03 mm) is more than enough for an 8-12 inch pole and is buildable from surplus stepper/leadscrew parts; verify actual positioning repeatability (the source checked theirs with a dial indicator) and pick the map grid from the field structure, not from the step size.
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Set the Hall-probe dwell time after each stage move empirically: step through dwell times in 0.5 s increments along the steepest field gradient and use the first value where successive profiles differ by less than the stationary noise (Rutgers found no difference above 2.0-2.5 s and used 3 s).
dwell = 3 s (0-0.5 s dwell gave >1% profile error; 2.0 s and 2.5 s indistinguishable)Source quote & editorial note
There are field profile differences in excess of 1% between zero of half-second dwell times. However, there is no measureable difference between dwell times of 2.5 and 2.0 seconds.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 3
Editorial note, tabletop extrapolation: Directly applicable method: any DIY gaussmeter-plus-stepper mapper should measure its OWN settling behavior - step the dwell in 0.5 s increments along the steepest gradient and adopt the first value where successive profiles agree within the stationary noise. Rutgers' 2-3 s is their apparatus's answer; an uncalibrated mapper risks a systematic error of unknown size, which is the reason to run the calibration, not a guaranteed 1%.
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Fiducialize the field map with five small excited iron needles precisely located around the pole tips: four to calibrate x and y scale, and a fifth placed off-symmetry to resolve the orientation ambiguity; with the main magnet de-energized, scan and locate each bump center by fitting a 2-D Gaussian.
5 needle bumps (<100 gauss), calibrated with main magnet de-energized; bump-pair spacing recovered as 2.500 in vs 2.500 in mechanicalSource quote & editorial note
To calibrate the Hall probe's position against the magnet's mechanical center we have employed five field bumps that are formed by iron needles excited by small copper coils which are precisely located around the cyclotron magnet pole tips. ... it was necessary for our field-bump calibration to be performed with the primary cyclotron magnet de-energized. After a full 2-D scan was completed; peaks, corresponding to the needles' centers are found by fitting a Gaussian, figure 6, to the measured field bump. Four needles were used to scale both dimensions; the fifth needle was used to break the symmetry, removing orientation ambiguities. Use of the lower field (<100 Gauss) bumps necessitates two scans ... A post-measurement analysis of the two returned a distance of 2.500 inches while mechanical measurement found the distance to be 2.500.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 3-4
Editorial note, tabletop extrapolation: Trivially cheap (iron nails plus a few turns of magnet wire) and it ties the field map to the magnet's mechanical center - extend that to chamber-center registration only by surveying the needle positions against the chamber geometry.
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Before trusting a two-scan (magnet-off then magnet-on) mapping procedure, qualify the stage's endpoint repeatability: Rutgers ran 100 cycles of 15 one-inch forward increments plus a 15-inch return (1600 moves, 2.4 million steps) and the carriage returned to the distal point within the digital dial indicator's 0.0001-inch resolution.
1600 travel manipulations / 2.4e6 motor steps -> return error < 0.0001 inSource quote & editorial note
After 1600 travel manipulations were executed by 2.4 million motor steps, the probe carriage reproducibly returned back to the distal point within the digital dial indicator's resolution of 0.0000 inches
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 4
Editorial note, tabletop extrapolation: Cheap insurance: an afternoon of cycling the homemade stage qualifies its endpoint repeatability under those conditions - also spot-check intermediate positions, the other axis, and repeatability across the session before trusting the maps; the indicator's resolution bounds what the test can see, not the stage's true error.
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Find the magnetic center of a weak-focusing (azimuthally symmetric) map by plotting Bz around trial reference circles, sweeping the circle center in x then y, and taking the minimum of a parabola fit to the standard deviation; iterate until successive center estimates differ by less than the positional uncertainty implied by the field noise and fit covariance.
minimize sigma(Bz) around circle vs center position; Rutgers centers from different radii agreed 'to 10-4' (the source states the figure without a unit - read it as a normalized agreement, not an absolute distance)Source quote & editorial note
the sequence of standard deviations was fit to a parabola from which the minimum standard deviation, i.e. the center locations, could be inferred ... the centers of each measurement circle were found to be coincident to 10-4.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 5-6
Editorial note, tabletop extrapolation: Exactly the analysis the builder needs for a symmetric-pole next machine: it also tells you how far the magnetic center sits from the mechanical center of the chamber.
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For the cited fourfold AVF field: pick a reference circle of half the maximum ion radius, FFT Bz around it, and move the circle center to maximize the 4th harmonic while minimizing the 2nd, 3rd and 5th. For other sector counts, derive the analogous harmonic objective for that symmetry - do not substitute N mechanically.
reference circle radius = 0.5 x r_max (2.5 in for a 5 in max ion radius); fourfold case: maximize 4th harmonic, minimize 2nd/3rd/5thSource quote & editorial note
we choose a reference circle to have a radius half that of the maximum ion radius ... the reference circle is swept to maximize the 4th harmonic, while minimizing the second, third, and fifth.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 6-7
Editorial note, tabletop extrapolation: Applies if a next machine moves to sectored pole tips; on a 12-inch machine the whole analysis is a spreadsheet/Octave job on the map you already took.
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Ferromagnetic materials lose their advantage above their saturation field (typically ~2 T): incremental permeability falls toward 1, so added excitation buys little more than it would in an air-core coil - the reason iron-dominated designs stay below saturation.
mu_r -> 1 as B approaches saturation (typically ~2 T)Source quote & editorial note
ferromagnetic materials lose their advantages above their saturation field (typically 2 T).
Humphries, Principles of Charged Particle Acceleration (1986) — p. 104, 108
Editorial note, tabletop extrapolation: Sets the practical scale of the iron-magnet approach for a next machine: above the saturation region, further field comes almost entirely from added ampere-turns at air-core rates - which is why higher-field machines move to superconducting coils. Below about 1.5 T the iron does most of the work.
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First-order coil sizing: producing 1 T across a 2 cm gap requires ~16 kA-turns (e.g. 160 turns at 100 A); for a given supply and winding, gap field is inversely proportional to pole spacing.
NI = B*g/mu0; 1 T x 0.02 m -> 1.6e4 A-turnsSource quote & editorial note
production of a field of 1 T in a gap with a 0.02 m spacing requires 16-kA turns (160 turns of wire if a 100-A supply is available).
Humphries, Principles of Charged Particle Acceleration (1986) — p. 111
Editorial note, tabletop extrapolation: Numerically the builder's own worked example: 538 turns at ~30 A across the reference machine's 1.42-in (3.6 cm) gap predicts ~0.56 T from the ideal gap formula - an upper bound, because real iron reluctance and leakage only subtract from it. The measured shortfall from ideal maps those losses; FEMM attributes them.
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Magnetic fringe fields extend beyond a gap a distance comparable to the gap width (the quote's scale length); the same Laplace-equation scaling governs electrode pairs, which is why deflector designs terminate their field with a septum rather than letting it leak into the last orbits.
fringe extent ~ gap width gSource quote & editorial note
The vertical field magnitude decreases away from the magnet over a scale length comparable to the gap width.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 140, 526
Editorial note, tabletop extrapolation: Rule of thumb for a next machine's layout: expect roughly one gap-height of field transition at the pole edge - how much of it is actually unusable depends on the field tolerance, so map it (dg-098) - and shield any deflector with a grounded septum as designed practice.
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A dipole edge inclined at (signed) angle beta acts as a thin lens in the non-bend plane with 1/f = tan(beta)/r_g (r_g = gyroradius): a properly oriented exit edge focuses the extracted beam vertically, but the sign convention decides focus vs defocus, and fringe fields modify the effective strength.
f_vertical = r_g/tan(beta)Source quote & editorial note
fx = (gamma mo vz/qBo)/tan beta = rgo/tan beta.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 141
Editorial note, tabletop extrapolation: If a next machine ever extracts a beam, angling the magnet exit edge can focus the diverging beam without any extra magnet - check the sign convention for the actual bend geometry and verify the full extracted-beamline optics rather than trusting the thin-lens number.
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Shape the magnet for field index 0 < n < 1 through the beam region - the weak-focusing band the source's bending magnets were shaped to: n > 0 gives vertical focusing, n < 1 keeps radial focusing.
0 < n(r) < 1; nu_r = sqrt(1-n), nu_z = sqrt(n) (azimuthally symmetric weak-focusing model)Source quote & editorial note
The bending magnets were shaped to produce a field with index in the range 0 < n < 1.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 159, 521
Editorial note, tabletop extrapolation: The outer bound that pairs with Koeth's n<0.2 refinement: the reference machine's field must fall (n>0), but slowly, all the way to full radius.
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Non-relativistic cyclotron energy is Tmax[MeV] = 48*(Z*R[m]*B[T])^2/A - energy scales as the square of both field and radius.
Tmax[MeV] = 48*(Z*R*B)^2/ASource quote & editorial note
Tmax = 48 (Z RB)2/A, where Tmax is given in MeV, R in meters, and B in tesla.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 524
Editorial note, tabletop extrapolation: The master sizing formula: the reference machine's 0.582 T at r ~ 0.10 m gives ~163 keV, which is its best demonstrated run; 1 MeV needs (R*B) ~ 0.144 T-m, e.g. 1.2 T at 12 cm.
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For axial stability the field must decrease with radius (n > 0, i.e. dB/dr < 0) - achievable with a flat-pole H-magnet's natural falloff - and oscillation solutions are real only for 0 < n < 1, with tunes nu_r = sqrt(1-n), nu_z = sqrt(n).
nu_r = sqrt(1-n), nu_z = sqrt(n); require 0 < n < 1Source quote & editorial note
Have real sinusoidal solutions for 0<n<1; this condition is true in a classical cyclotron
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 36-37
Editorial note, tabletop extrapolation: The reference machine's flat-pole H-frame gets its weak focusing from natural radial falloff - but a flat pole is nearly uniform over much of its radius and falls mainly near the edge, so map n(r) rather than assuming it: the design task is confirming where n is usefully positive, then controlling how fast it rises.
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The lecture's scaling argument: final energy goes as T ~ K*Q^2/A with K = (e*B*rho)^2/(2*m0), so at fixed energy the extraction radius falls as 1/B - and, under geometric similarity, iron volume as 1/B^3 (their example: r_extraction 2.28 m at 1 T vs 0.76 m at 3 T, a 1/27 volume ratio).
K_B = (e*B*rho)^2/(2*m0); radius ~ 1/B at fixed energy; volume ~ 1/B^3 under geometric similaritySource quote & editorial note
Almost (but not quite) spherical: Efficient cyclotron magnetic circuits include more iron laterally than axially
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 48-50
Editorial note, tabletop extrapolation: The B^2 energy leverage argues for raising a next machine's field before enlarging poles: doubling B quadruples energy at fixed radius. The 1/B^3 mass saving holds only while the whole magnet scales geometrically - gap included - and the iron's own saturation (dg-096) caps how far the argument runs.
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Choose the ISM frequency 13.56 MHz (B = 0.889 T for protons) to drive the dee from commercial RF generators - the source machine's reason for its tuning - typically 50-ohm hardware through a matching network.
f = qB/(2*pi*m): 13.56 MHz protons -> B = 0.889 T; 50-ohm source -> matching network -> high-Z deeSource quote & editorial note
The cyclotron circuit was originally tuned to a frequency of 13.56 MHz due to the requirements of the commercial RF generator in use ... a magnetic field of 0.889 Tesla is required.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 10-11
Editorial note, tabletop extrapolation: Directly actionable option for a next machine: targeting ~0.89 T instead of 0.59 T puts the machine on the 13.56 MHz ISM band, where used generators, amplifiers and matchboxes are plentiful. Legality rides on emissions containment rather than the band label (dg-1373's verification), and the match must still be designed for the dee's actual impedance (dg-287).
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Shape pole faces (spherical slice or edge 'lump') to produce a few-percent radial field decrease - a flat 'magnetic capacitor' gap gives n = 0 and no vertical restoring force, so some deliberate contouring is required; the source works the example of a ~3% edge fall-off on a 6-in-radius pole via a best-fit sphere of rho ~ 21.8 in (about a 32-degree slice).
for 3% edge fall-off on 6-in-radius pole: best-fit sphere rho ~ 21.8 in (slice ~32 deg); B_z = B_0*(r0/r)^n, restoring force needs 0 < n < 1Source quote & editorial note
A radially decreasing field can be described as Bz = B0(r0/r)^n for n >= 0, where n = 0 implies a uniform field and n > 0 implies a restoring force.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 7-9
Editorial note, tabletop extrapolation: Exactly the reference machine's problem class and size: machine a gentle crown or stepped 'lump' into the 8-inch poles (or shim equivalently), aiming for the few-percent center-to-edge fall-off of the source's worked case - and verify the result against the mapped n(r) (dg-003, dg-561) rather than the geometric recipe, since the actual profile depends on gap and permeability.
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Respect mechanical constraints when contouring poles: the practical shape is 'a pole piece with a flat surface at the edge with a thickness sufficient for the screws and a kind of lump in the middle with a flat top' - a flat screw-land rim blended with a raised central region. [Corrected 2026-08-23: a worked 'lump model' (R = 6 in, 0.3 in boss, crown radius ~19.6 in, 3% fall-off) was removed - the sagitta arithmetic did not check (0.3 in over a 5-6 in half-width implies a crown radius of ~40-60 in), and the fall-off depends on gap reluctance, saturation and fringing, not pole radius alone.]
Source quote & editorial note
a pole piece with a flat surface at the edge with a thickness sufficient for the screws and a kind of lump in the middle with a flat top
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 8
Editorial note, tabletop extrapolation: Directly applicable fabrication pattern for contoured pole caps that still bolt on - and a geometric design check to run: verify the theoretical contour leaves enough thickness at the mounting screws before committing, since a steep profile can thin the screw land below usability.
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Pick pole size by mission: 6-9 inch poles are the economical educational range; go to 12-15 inches if you want enough energy for neutron-yielding light-element reactions.
educational: 6-9 in poles; light-element/neutron reactions: 12-15 inSource quote & editorial note
For educational applications a six to nine-inch pole piece is an economical range; for inducing light element reactions ... a somewhat larger machine, say, 12 to 15 inches
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 11-12
Editorial note, tabletop extrapolation: Frames the next machine's decision the way the source does: 8-inch-class poles sit in the educational range, and light-element reaction goals argue for the 12-15 inch class. Pole diameter is a proxy - field and species matter as much - and small does not mean neutron-incapable: deuteron operation makes neutrons at any energy via D(d,n)3He, which is a hazard question before it is a capability one (see the safety rules).
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Compute magnet excitation from NI = 2.02 x B(gauss) x gap(inches) - the ideal air-gap MMF in historical units (NI = B*g/mu0).
NI (ampere-turns) = 2.02 x gauss x inches of gapSource quote & editorial note
Ampere-Turns = 2.02 x gauss x inches gap
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Editorial note, tabletop extrapolation: Directly applicable: 5900 G across a 2-inch gap needs ~24,000 ampere-turns as the ideal floor, with iron reluctance and leakage added on top (dg-016, dg-036). Leakage multiplies the FLUX the iron must carry - that sizes the yoke - not the gap MMF this formula computes.
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Design pole and coil fastenings for the magnetic forces: pole-face attraction is (kilogauss)^2 x (area in in^2)/1.735 pounds, and conductor force is kG x amps x inches/1750 pounds.
F_pole(lb) = kG^2 x in^2 / 1.735; F_cond(lb) = kG x A x in / 1750Source quote & editorial note
Lbs. force on conductor = 1/1750 x kilogauss x amperes x inches length; Lbs. force between pole faces = 1/1.735 (kilogauss)^2 x (inches^2 area)
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Editorial note, tabletop extrapolation: Directly applicable: at 5.9 kG on 50 in^2 poles that is ~1000 lb of attraction a next machine's bolts and spacers must carry.
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Wouters' recommendation: run the magnet iron near saturation for most economical performance, with most soft irons beginning to saturate near 16 kilogauss and some usable to 21 kG.
B_sat(soft iron) ~ 16 kG; upper limit ~21 kGSource quote & editorial note
most soft irons begin saturating in the vicinity of 16 kilogauss, though some may be operated as high as 21 kilogauss
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 2
Editorial note, tabletop extrapolation: Directly applicable - with the right variable: the binding number is the LOCAL flux density in the narrowest iron section, which leakage, joints and corners push above the gap figure (dg-037). The reference machine's 5.9 kG gap field leaves apparent margin; how much field a next machine can add before the iron dominates is a FEMM answer, not a factor read from the gap value.
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Size the yoke/coil for leakage flux by multiplying the gap flux by a factor set by the gap-height/gap-diameter ratio: 1/2 gives 2.0, 1/4 gives 1.5, 1/10 gives 1.2 (small cyclotrons live in the 1.5-1.2 region).
leakage multiplier: h/D=1/2 -> 2.0; 1/4 -> 1.5; 1/10 -> 1.2Source quote & editorial note
Ratio Gap Height/Gap Diameter ... Multiplying Factor: 1/2 -> 2; 1/4 -> 1.5; 1/10 -> 1.2, region of small cyclotrons
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 2
Editorial note, tabletop extrapolation: Directly applicable sizing rule: for an 8-inch pole with ~1.5-2 inch gap (h/D ~ 1/4), design coils and yoke for ~1.5x the gap flux.
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Make the pole-core length and the pole-core-to-return-yoke distance at least twice, preferably three times, the gap height.
L_core >= 2-3 x h_gap; core-to-yoke spacing >= 2-3 x h_gapSource quote & editorial note
the length of the pole cores and the distance from pole cores to return yokes is at least twice and preferably three times the gap height
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable to a next machine's H-frame: coil space often pushes the frame toward compliance anyway - check it explicitly whenever the frame is shortened, rather than assuming the coils did the enforcing.
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Bias saturation away from the return path by giving the yoke at least 25 per cent more total cross-sectional area than the cores - the source's margin.
A_yoke >= 1.25 x A_coreSource quote & editorial note
the return yoke must accordingly be designed so that its total cross sectional area is a good deal greater than that of the cores, say, at least 25 percent greater
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable: for 8-inch (50 in^2) cores, provide at least ~63 in^2 of total yoke steel around the flux return - and still check the narrowest local section, corner and joint (dg-037, dg-132): the area margin lowers AVERAGE density, while local constrictions can saturate first regardless.
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Machine yoke-to-yoke and yoke-to-core contact surfaces flush to eliminate parasitic air gaps in the magnetic circuit.
Source quote & editorial note
It is important that the contact surfaces between yoke pieces and between yoke and pole cores be flush to eliminate additional air gaps
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable: any unintended air gap adds straight onto the magnetic circuit's gap budget - 0.003 in against a 1.5-in main gap is 0.2%, small but real; the same error across tight pole-cap joints is proportionally worse. Machine flush because it is cheap at build time and unfixable after assembly.
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Make vacuum-chamber top and bottom thin, circular steel plates - the quoted design, chosen to decrease the magnetic gap as much as possible - and make the side wall non-magnetic (brass, per the source) so field is not bypassed around the gap.
Source quote & editorial note
top and bottom of the vacuum chamber should be thin, circular steel plates ... to decrease the magnetic gap as much as possible. To prevent field bypassing, the tank wall must be non-magnetic, preferably brass
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 5
Editorial note, tabletop extrapolation: Directly applicable chamber architecture for a small machine; every millimeter of chamber wall inside the gap costs ampere-turns.
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The gap drives the field: for a gap-dominated, unsaturated magnet B ~ mu0*NI/g, so keep the pole gap as small as the vacuum chamber, dee clearance and beam aperture allow, even at the cost of a harder chamber design - the source calls its tight spacing 'essential' despite the chamber difficulty it caused. [Corrected 2026-08-23: earlier text also asserted the magnet is 'the single most expensive subsystem', which the quote does not say.]
B ~ mu0*NI/g for a gap-dominated, unsaturated circuit; real magnets add fringe, yoke reluctance and saturationSource quote & editorial note
it is advantageous to keep the gap between the magnet poles small. This tight spacing made the design of the vacuum chamber more difficult, but it was essential.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 1-2
Editorial note, tabletop extrapolation: The central trade for a next machine: each millimetre of gap saved is field (at fixed ampere-turns), and energy scales as B^2 (at fixed radius and species) - but only within the unsaturated, gap-dominated regime, and only after dee-voltage clearance, pumping and field quality have had their say. Verify the saturation and fringe terms in FEMM before banking the gain. [Note revised 2026-08-23: an earlier text called the gain 'for free'; the chamber redesign it costs is the quote's own point.]
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The proton RF frequency is 15.2 MHz per tesla; use a table of f = 15.23*B MHz to co-design magnet field and RF tuning range (Cyclotron Kids' table: 1.0-1.7 T maps to 15.2-25.9 MHz, with matching capacitance 166 pF down to 57 pF for their fixed tank inductance).
f(MHz) = 15.23 * B(T) for protonsSource quote & editorial note
B (Tesla) 1 ... 1.6 ... f (MHz) 15.23 ... 24.36
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 12
Editorial note, tabletop extrapolation: The reference machine's 0.59 T resonates at ~9.0 MHz; a next machine's field choice fixes the synchronous frequency via this 15.23 MHz/T constant (fundamental-harmonic protons). The tank tuning range then follows from the chosen inductance - the source's capacitance column is specific to theirs.
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Size the return yoke cross-section larger than the pole so yoke flux density drops below pole-tip field (Cyclotron Kids: 1.6 T on 14-inch poles reduced to 1.2 T in the yoke), keeping the return path out of saturation with scrap steel.
A_yoke/A_pole >= B_pole/B_yoke_target (1.6 T -> 1.2 T)Source quote & editorial note
Increased cross section reduces flux through yoke to 1.2T
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 8
Editorial note, tabletop extrapolation: Area-ratio thinking for welding a next machine's frame from surplus plate: size the yoke so its flux density lands comfortably below the knee of the ACTUAL steel's BH curve - surplus plate is rarely certified, so measure or assume conservatively - and check per-limb: flux splits between return limbs, and the narrowest section, corner or weld is what saturates first, not the gross ratio.
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Machine a slight taper on the pole faces so the field decreases with radius, providing the weak-focusing (restoring) Lorentz force on the beam - design it in the field code before cutting steel.
Source quote & editorial note
Slight taper on pole applies a corrective Lorenz force to the beam. Made with freeware! Poisson Superfish
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 8
Editorial note, tabletop extrapolation: The documented amateur approach at the reference machine's scale - Cyclotron Kids here, with the pole-shaping rules (dg-119, dg-152) carrying the design math: put the field index into the pole profile deliberately, designed in the field code before cutting steel, rather than relying on accidental fringing.
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The article's account: a 300 keV-class proton cyclotron completed for under $1000, with base pressure 0.01 mTorr, 1.6 kVpp on the dees at ~400 W peak RF, a C-frame yoke of welded soft-steel bar and meehanite pole pieces face-milled to a field-index profile (the quoted engineering; completion and cost per the article's narrative - scan re-read queued).
300 keV: ~1e-5 torr, 1.6 kVpp dee, 400 W pk, machined field-index pole profileSource quote & editorial note
Polepieces of meehanite steel facemilled to a profile that gave appropriate field index... 1.6kVpp on Ds, 400Wpk. Base pressure 0.01mTorr
Niell, Effective Scientific Equipment Procurement Strategies: Building on a Budget (2010) — p. 11-17
Editorial note, tabletop extrapolation: An existence-proof account at exactly the reference machine's energy class: modest dee voltage (1-2 kVpp), 1e-5 torr, and a machined pole profile - not heroic RF or UHV - are what the article describes sufficing below ~300 keV.
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The Rutgers 9-inch prototype found its first beam (September 16, 1999) by slowly sweeping the magnetic field to locate the resonance condition - a useful first-beam method when the RF can be held fixed and the magnet swept reproducibly.
sweep B at fixed f until f = qB/(2*pi*m)Source quote & editorial note
1st successful operation was recorded by slowly sweeping B-field to locate resonance condition. September 16, 1999
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 8
Editorial note, tabletop extrapolation: A good commissioning move for a next machine when the RF stays matched at fixed frequency; whether B is the easy knob depends on the magnet - supply limits, inductance, hysteresis and settling time can make slow, repeatable B sweeps the hard part.
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Keep the n = 0.2 contour out of the region the beam occupies: n = 0.2 is the coupled Walkinshaw resonance (2*nu_z = nu_r), and a weak-focusing machine whose ions spend many turns near it transfers radial oscillation into vertical growth wherever a coupling perturbation - field asymmetry, misalignment - drives it; real machines usually have one.
n = -(r/B)(dB/dr) < 0.2 for r < r_max; unmodified Houghton magnet reached n = 0.2 at r = 5.9 cm vs 7.8 cm Dee radiusSource quote & editorial note
the field index value n=0.2 must not occur inside the maximum ion orbit radius to avoid coupled resonances
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 2, 39
Editorial note, tabletop extrapolation: One necessary check for weak-focusing pole shaping on a 100 keV-1 MeV tabletop machine, and computable from a measured B(r) curve - necessary, not sufficient: axial focusing margin (n > 0), radial stability (n < 1), phase slip, aperture and orbit clearance all still have to be verified against the actual B(r). Where the contour cannot be pushed out to the final radius (dg-152), the design question becomes how few turns the beam spends near it, not whether the machine can work at all.
Cited in: Beam Dynamics: An Interactive Laboratory
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Keep cyclotron shims thin - historical practice used iron sheets typically 0.25 inch or less - because an over-thick shim makes B change too abruptly at the shim edge and the ion fails to get past it; what counts as thin is geometry-dependent (Houghton's modelled 0.125-in shim was still far too thick for its small machine).
historical practice: sheets typically <= 0.25 in; Houghton modelled 0.3175 / 0.635 / 1.27 cm shims - all too thick for its geometrySource quote & editorial note
Shimming involves the insertion of thin iron sheets (typically 0.25 inches or less) between the pole faces and the vacuum chamber. ... the magnetic field changes too quickly near the edge of the shim. This is a result of making the shim too thick. ... In retrospect it appears that these shims were far too thick and created too dramatic of a change in magnetic field. While shims could still be used with the Houghton cyclotron, the thin shims these calculations suggest would be challenging to make
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 25, 44, 46
Editorial note, tabletop extrapolation: Warns the builder off the obvious first shimming attempt; the useful shims are thinner than are convenient to fabricate and hold in place - model, or test progressively thinner shims against, the actual gap geometry.
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Make Bz decrease with radius so that the field has a restoring radial component off the median plane: weak axial focusing comes from a negative dBz/dr, and Morrow's thesis describes achieving it with a linearly decreasing Bz. The criterion that matters is the field index n = -(r/B)(dB/dr) staying in its stable range (dg-145, dg-136), not linearity of B(r) as such - constant n means B proportional to r^-n, not a straight line. [Corrected 2026-08-23: earlier text told the builder to judge every shim by the linearity of B(r) and stated Br = C*z; the sign is Br ~ z*dBz/dr (negative for a falling field) and linearity is one field shape that focuses, not the acceptance test.]
Near the median plane (curl B = 0): Br ~ z * dBz/dr. Axial focusing needs dBz/dr < 0, i.e. n = -(r/B)(dB/dr) > 0; stability 0 < n < 1, with n = 0.2 the Walkinshaw resonanceSource quote & editorial note
weak magnetic focusing can be achieved by producing a magnetic field in which Bz linearly decreases.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 26-27
Editorial note, tabletop extrapolation: For a shimming attempt on the reference machine's 8-inch poles the plottable acceptance test is n(r) from the measured B(r), by finite differences, kept inside its stable range over the whole used radius - not a straight-line fit to B(r). A field profile that passes that test still has to be checked for isochronism and phase slip (dg-1328), the n = 0.2 contour (dg-136, dg-152) and radial stability; "no orbit code needed" was an overreach, though a simple n(r) plot does reject a bad shim before any tracking is run.
Cited in: Beam Dynamics: An Interactive Laboratory
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Watch for adding-type trim coil configurations like the reference thesis's modelled cases, where B rises with radius out to ~5 cm: that produces a NEGATIVE field index (down to -0.1 in those models) and axial defocusing.
B increasing to r ~ 5 cm -> n < 0 (down to -0.1 in the modelled cases)Source quote & editorial note
the magnetic field actually increases in magnitude out to around r = 5 cm at which point it begins decreasing again. This is problematic because it yields a negative field index
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 51-53
Editorial note, tabletop extrapolation: A concrete trap when adding iron or coils near the center of an 8-inch pole: check the sign of dB/dr over the whole usable orbit range, not just at the edge - the 5 cm crossover and the -0.1 index are that geometry's numbers, not general thresholds.
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Do not expect a bucking-coil fix to rescue weak focusing cheaply: in the reference thesis's modelled geometry, bucking coils moved the n = 0.2 radius outward by only ~0.2 cm while cutting peak field from 1.27 T to 1.07 T - a 15.7% drop the source rounds to '~20%' - and the modification was judged insufficient.
dr(n=0.2) = +0.2 cm for dB: 1.27 T -> 1.07 T (a 15.7% decrease; the source says ~20%); energy scales with (B r)^2 of the final orbit, so trading field for a marginal radius gain losesSource quote & editorial note
the difference in radius is minimal - about 0.2 cm - and comes at the steep cost of a ~20% reduction in maximum magnetic field from 1.27 T to 1.07 T. As such, this modification was considered insufficient.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 53-54
Editorial note, tabletop extrapolation: Saves a next machine's builder from spending months on one class of trim-coil fix inside a small gap (they also steal gap height) - but this is one modelled geometry: evaluate any other trim-coil design from its full B(r) map and orbit dynamics.
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A modeled upgrade with real leverage: replacing the Houghton chamber's aluminium lids with magnetic stainless-steel lids reaching 2.2 cm beyond the poles makes them act as wide pole faces drawing field outward - in the thesis's PSF model this pushed n = 0.2 from r = 5.9 cm out to r = 8.3 cm, cut the effective pole gap from 3.9 cm to 2.54 cm, and raised B from 1.27 T to 1.77 T (27.0 MHz, 0.91 MeV computed, vs 0.47 MeV for the unmodified design).
modeled: lid radius = pole radius + 2.2 cm; gap 3.9 -> 2.54 cm; B 1.27 -> 1.77 T; f = 27.0 MHz; Tmax 0.47 -> 0.91 MeVSource quote & editorial note
replace the current aluminum chamber lids with magnetic stainless steel lids with radius 2.2 cm larger than the Dee ... As the vacuum chamber radius is 2.2 cm larger than the radius of the magnet poles, these lids act as wide pole faces that draw the magnetic field lines out to larger radii. ... The maximum magnetic field of the unmodified design is B = 1.27 T and is B = 1.77 T for the lid design. This is because the pole gap of the unmodified design is 3.9 cm while the lid design has a pole gap of 2.54 cm. ... B = 1.77 T corresponds to a Dee frequency of 27.0 MHz and a maximum kinetic energy of 0.91 MeV for protons. ... n=0.2 occurred at r=5.9 cm for the unmodified and at r=8.3 cm for the lid.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 54-55
Editorial note, tabletop extrapolation: Cheap in materials and potentially the highest-leverage change of this class, but the numbers are one thesis's model of one geometry: model your own lid as part of the magnetic circuit, verify the full B(r) and n(r), confirm the chosen stainless grade is actually ferromagnetic and vacuum/structurally suitable, and recompute energy from the usable orbit radius.
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Use the Poisson Superfish (free, 2-D magnet cross-section) plus SIMION 8.1 (commercial ion tracking) workflow to evaluate magnet modifications before cutting steel; the thesis includes the geometry files and the PSF-to-SIMION conversion recipe.
PSF model: pole face 150 mm, pole gap 39 mm, coil current 70 A, half-plane sliceSource quote & editorial note
Pole face: 150mm, Pole gap: 39mm, Current: 70A ;NOTE: this is a slice down the middle of the magnet
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 60-68
Editorial note, tabletop extrapolation: Low-cost simulation path for a hobbyist - Superfish is free, SIMION is paid but widespread, and FEMM plus the playbook's Python tracker is the all-free equivalent; the appendix geometry file is a working starting template for an 8-15 cm pole magnet.
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Falling beam current with collector radius was observed on the reference thesis machine and attributed to beam loss before full radius; shaped ferromagnetic shims between chamber and pole faces were proposed (not demonstrated) to strengthen magnetic focusing and recover current.
Source quote & editorial note
much of the beam current is being lost by the time the beam reaches larger radii... This could be done by adding shims of ferromagnetic material between the chamber and pole faces.
Editorial note, tabletop extrapolation: Predicts the current-vs-radius profile the builder should measure. If a next machine loses beam before full radius, diagnose first - map B(r) and n(r) and identify the loss mechanism - then shim, and re-verify field and transmitted current; a shim can worsen the index if misshaped.
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Once iron poles saturate - about 2 T in the source's accounting - added excitation buys little further field and maximum energy grows mainly with radius; iron-pole designs therefore plan around fields below saturation.
pole saturation ~2 T (source's figure; onset is alloy- and geometry-dependent and gradual)Source quote & editorial note
once the iron magnet poles become saturated (at about 2 T) the maximum energy is determined by R
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 18
Editorial note, tabletop extrapolation: Frames the next machine's tradeoff space: pushing the reference machine's 0.59 T toward 1.2-1.5 T is cheap energy gain (E ~ B^2 at fixed radius), while near pole saturation the iron stops helping and pole diameter becomes the effective lever.
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Keep the classical-cyclotron field index n = -(r/B)(dB/dr) between 0 and 1 everywhere inside the acceleration region - n<0 loses axial focusing, n>1 loses radial stability - and empirically n should rise roughly linearly from 0 toward 1 with radius, shaped by shimming.
n = -(r/B)dB/dr; 0 < n < 1, rising ~linearly with r; f_z = sqrt(n)*f0, f_r = sqrt(1-n)*f0Source quote & editorial note
the value of n for the cyclotron must be between 0 and 1; it has been determined empirically the index should increase with r roughly linearly between 0 and 1
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 21-23
Editorial note, tabletop extrapolation: Source-specific weak-focusing guidance, and not a target to shim toward: 0 < n < 1 is the stability condition, but the empirical 0-to-1 ramp is Loucks' description of one machine's profile, not an instruction to drive n as high as possible. n = 0.2 is the Walkinshaw coupling resonance (dg-136, dg-152, dg-563, dg-694), and in a many-turn classical cyclotron it can constrain the usable orbit long before n approaches 1. Map B(r) with a Hall probe, compute n(r) by finite differences, and shape the profile with that contour in mind. [Note added 2026-08-22: the resonance cross-reference was missing; read in isolation the rule invited shimming toward n = 1.]
Cited in: Beam Dynamics: An Interactive Laboratory
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Budget cooling water across subsystems explicitly - the Houghton thesis's own bookkeeping: the 15 cm magnet wanted 6.1 L/min at 70 A, but the chiller could spare only 3.0 L/min after the diffusion pump's 0.8, capping operation at 50 A / 1.1 T. The chiller, not the power supply, set maximum field.
GMW 3473-70: 70 A needs 6.1 L/min; chiller 3.8 L/min total -> limited to 50 A, 1.1 T at 3.85 cm gapSource quote & editorial note
the maximum field is limited by available water cooling and the power supply... To achieve the maximum field, using 70 A, the magnet requires 6.1 L/min
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 35-36
Editorial note, tabletop extrapolation: Do the L/min bookkeeping for the whole next machine (magnet + diffusion/turbo + RF amp) before buying a chiller; the cooling loop is a first-class design constraint, not an afterthought.
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Measure n(r) by finite differences of Hall-probe readings on a rotating non-magnetic jig (aluminum disc in the median plane): n(r) ~ -(r/<Bz>)*(d<Bz>/dr) computed from azimuthally averaged readings, with the reference experiment using 1 cm radial steps - adequate in smooth field regions, too coarse near shim edges and pole fringes.
n ~ -(r/<Bz>)*(delta<Bz>/delta r), <Bz> azimuthally averaged; reference spacing dr = 1 cm, reduce near sharp gradients; prefer centered differencesSource quote & editorial note
the dBz/dr term was approximated by dBz/dr, where dr is the difference between two radii (1 cm)
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 36-38
Editorial note, tabletop extrapolation: A directly copyable measurement rig for a next machine's field map: rotating grooved aluminum disc plus angular scale gives B(r,theta) with hardware the builder already owns; average over theta before differencing, and tighten the spacing where the gradient changes fast.
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A 1.2 T tabletop cyclotron design point: 15 cm flat pole faces with the chamber in place giving a 3.81 cm pole-tip separation, 1.28 T at 70 A, water cooled at 18 C and 0.8 gallon/min at 50 A.
15 cm poles, gap 3.81 cm, 1.28 T at 70 A (1.16 T at 50 A); cooling 18 C water at 0.8 gpmSource quote & editorial note
With the chamber in place, the separation between the pole tips is 3.81 cm, giving a maximum magnetic field of 1.28 T at 70 A ... requiring 18 C water flowing at 0.8 gallons per minute (at 50A)
Editorial note, tabletop extrapolation: A purchasable-magnet benchmark almost exactly at the reference machine's scale. The 0.8 gpm is a flow figure, not a chiller spec: size the chiller from coil dissipation and allowable temperature rise (P = flow x heat capacity x dT - the magnet-power calculator's territory), with the flow number as the plumbing constraint it is.
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A proven parameter set at exactly the reference machine's scale: 12 in poles, 4 in gap with removable 1 in pole tips, 1.2 T max, single 5 in radius dee with 0.9 in aperture, 2-30 MHz RF at up to 1.5 kW giving ~10 kV dee, 1e-5 Torr operating pressure.
12 in poles / 4 in gap / 1.2 T / 5 in dee / 0.9 in aperture / 1.5 kW -> ~10 kV dee / 1e-5 TorrSource quote & editorial note
12 inch diameter poles pieces forming a 4-inch gap to which upper and lower pole tips up to 1-inch thick can be easily attached and removed. ... all capable of producing a maximum central axial field, Bz(r=0), of 1.2 Tesla ... a single 5-inch radius DEE with a 0.9 inch vertical aperture and a matching dummy DEE. The Radio Frequency (RF) supply is tunable from 2 to 30 MHz with adjustable power up to 1.5 kW ... capable of achieving a peak DEE voltages on the order of 10 kV ... the 2-inch tall, 13-inch diameter cyclotron vacuum chamber's operating pressure of 1E-5 Torr.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: A complete cross-check machine for a next machine's sizing; note the removable-pole-tip trick that lets one magnet host many field profiles.
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Make pole tips removable, swappable inserts - up to 1 inch thick per the quote, with the source machine keeping four sets - so field-shaping and AVF experiments proceed without rebuilding the magnet.
Source quote & editorial note
upper and lower pole tips up to 1-inch thick can be easily attached and removed - we currently have four sets of pole tips.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: Probably the single best architecture decision the builder can copy: swap-on tips let a next machine iterate field profiles cheaply - with the caveat that a sector-tip (AVF) conversion is still re-checked against return-path saturation and coil clearances (dg-045).
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Power the upper and lower coils from independent supplies so a deliberate top/bottom ampere-turn imbalance can shift the beam's vertical equilibrium (accelerating) plane onto the geometric midplane of the dee.
Source quote & editorial note
The magnet's upper and lower coils are independently energized enabling an intentional axial field imbalance so as to vertically shift the accelerating plane.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: Cheap beam-height trim for a next machine: two supplies, or a properly rated current-trim circuit on one coil, instead of re-machining anything - verify the result with a field or beam measurement, since unequal excitation perturbs the midplane symmetry it exploits.
Cited in: Beam Dynamics: An Interactive Laboratory
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Shape the weak-focusing pole taper so the field index reaches n = 0.2 only at the final ion radius: the n = 0.2 point is the nu_r = 2*nu_z coupling resonance, where dwelling ions grow axially as far as the driving perturbation and dwell time allow - the aperture is what catches them when they do.
n(r) = -(r/Bz)(dBz/dr); require n < 0.2 for all r < r_finalSource quote & editorial note
if n = 0.2 is to be avoided (vx=2vz), then the rate at which the vertical field decreases must be moderated such that n=0.2 occurs at the final ion radius.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 3
Editorial note, tabletop extrapolation: The quantitative pole-taper design rule for a next machine: map n(r) from the field profile and keep 0 < n < 0.2 out to full beam radius.
Cited in: Beam Dynamics: An Interactive Laboratory
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Proof by counterexample: poletips built to intentionally drive a destructive axial resonance put n = 0.2 near r = 3.5 in, well inside the 5-in dee radius; because n = 0.2 is a difference resonance whose axial amplitude is bounded by the initial radial offset, a ~3 mm displacement of chamber center from magnet center was needed to seed the axial blow-up.
'bad' poles: n = 0.2 at r = 3.5 in (70% of dee radius); ~3 mm center offset seeded the resonant axial blow-upSource quote & editorial note
We have built a set of poletips designed to intentionally drive a destructive axial resonance; we refer to these as the 'bad' weak focusing poles tips. The n=0.2 location occurs near r=3.5 inches, well within the 5 inch DEE radius, so as to allow the ion displacement to grow. Since the n=0.2 is a difference resonance the axial peak-to-peak amplitude is bounded by the initial radial offset. A displacement of the chamber's center of about 3mm with respect to the magnet center was necessary to seed the resonant axial blow up
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 5
Editorial note, tabletop extrapolation: Shows how little margin there is between good and bad tapers on an 8-12 inch machine; motivates measuring n(r), not guessing it.
Cited in: Beam Dynamics: An Interactive Laboratory
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For AVF/hybrid pole designs, use the tune formulas nu_z^2 = -k + F(1+tan^2 xi) and nu_r^2 = 1 + k (k = average field index, F = flutter, xi = spiral edge angle) and keep both tunes away from integer and rational-fraction resonances.
nu_z^2 = -k + F(1+tan^2(xi)); nu_r^2 = 1+kSource quote & editorial note
The axial tune... can be summarized by: vz2 = -k + F(1+tan2xi) and the radial tune is written as: vr2 = 1+k
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 6
Editorial note, tabletop extrapolation: If a next machine gets sector pole tips (allowing a rising average field), these two lines are the first-order SCREEN - in the source's conventions: check the sign convention for k and the flutter definition before substituting (dg-156's lesson) - with resonance avoidance and then tracking completing the design.
Cited in: Beam Dynamics: An Interactive Laboratory
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To find closed orbits experimentally, a current-carrying wire loop (the source used 30 AWG, 71 mm circumference, 2.5 A) placed in the magnet gap snaps to and traces stable equilibrium orbits, revealing off-center orbits that are hard to locate otherwise.
30 AWG loop, 71 mm circumference, 2.5 ASource quote & editorial note
A 30 AWG wire loop, with a circumference of 71 mm, was energized with a current of 2.5 amps and placed in the magnet gap. ... The energized wire loop simply needed to be tossed towards the gap and it would reproducibly snap to the nearest stable orbit.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 7
Editorial note, tabletop extrapolation: A cheap field-quality diagnostic, but run it as an engineered experiment, not a party trick: current-limit and isolate the supply, insulate and restrain the leads, set up de-energized, check the wire's temperature rise at the chosen current, and mind magnetic forces and pinch points around a 0.5-1 T gap.
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Compute both tunes from the same four quantities - field index n, flutter F, sector number N and spiral angle xi - using nu_z^2 = n + (N^2/(N^2-1))*F*(1+2tan^2 xi) with F = (<B^2>-<B>^2)/<B>^2 as the source defines it, and the matching radial expression.
nu_z^2 = n + (N^2/(N^2-1)) * F * (1 + 2 tan^2 xi); F = (<B^2> - <B>^2)/<B>^2 (the source's flutter - many texts call this quantity F^2; check the convention before substituting); n = -(r/B) dB/drSource quote & editorial note
F = ((<B^2> - <B>^2)/<B>^2) is called the flutter and represents the hill to valley field difference
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 25-26
Editorial note, tabletop extrapolation: The complete design equation set for an AVF follow-on build; every term is measurable from a 2-D Hall-probe map of the built magnet.
Cited in: Beam Dynamics: An Interactive Laboratory
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Spiral the poles rather than relying on edge focusing alone when flutter is small: edge focusing from a radial sector gives one focusing and one defocusing edge per hill, whereas a spiral angle multiplies the flutter term by (1+2tan^2 xi) at both edges.
focusing enhancement factor (1 + 2 tan^2 xi); at xi = 45 deg the flutter term triplesSource quote & editorial note
N large: high maximum energy, F small and quasi circular orbits -> spiral compulsory
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 26, 28
Editorial note, tabletop extrapolation: Explains when the extra machining pain of spiral tips pays: when flutter is small and orbits quasi-circular - the quoted regime, where 'spiral compulsory'. Whether an 8-12 inch N = 4 design wants spiral or more hill/valley contrast is a computed comparison (the (1+2tan^2 xi) factor against achievable flutter), not a default.
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Use N >= 3 sectors in any AVF design: the perturbative radial-tune expression breaks down at N = 2 (its resonant denominator vanishes - the pi stop-band boundary behind the quote's 'N must be larger than 2'), and each N carries an energy ceiling T = (N/2 - 1)*E0 - about 469 MeV for N = 3 and 938 MeV for N = 4 protons.
nu_r^2 = 1 - n + (N^2/(N^2-1))(3/(N^2-4)) F^2 (1+2tan^2 xi); T_max = (N/2 - 1) E0Source quote & editorial note
It implies that N must be larger than 2 (lower limit of the pi stop-band) and there is an energy limit for every N value T = (N/2 - 1)E0
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 27-28
Editorial note, tabletop extrapolation: Rules out 2-sector 'butterfly' pole tips that look easy to machine; N=3 or 4 is the practical amateur choice and neither limits sub-MeV protons.
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With constant gaps B(r) falls naturally with radius and the larger the gap the faster it falls, while coil-dominated field rises with radius but only matters once the iron saturates - use that pairing to get the profile you want.
Source quote & editorial note
Constant gaps : B(r) naturally decreasing. The larger the gap, the stronger the decrease ... Coil field : B(r) naturally increasing. Important only when iron becomes saturated
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 32
Editorial note, tabletop extrapolation: Explains the positive field index (n > 0 in the site's n = -(r/B)dB/dr convention) that a flat-pole tabletop magnet already has from its natural falloff - and why a bigger gap gives more weak focusing but less field.
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Reach for the iron before the copper when shaping a warm magnet's field: trim coils increase the gap and are 'very weak except in superconducting machines' - and even then, model before implementing (both quoted); iron shaping carries the flip side the lecture tabulates - effective and cheap but non-linear and fixed once cut (comparison rows: scan re-read queued).
Source quote & editorial note
Trim coils increase the gap ... Very weak except in superconducting machines ... Model it before implementing it to avoid unexpected effects
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 33, 47
Editorial note, tabletop extrapolation: Settles the shim-vs-trim-coil question for a small warm magnet the way the Houghton thesis found empirically: iron wins for the main profile. A weak trim coil can still earn a place for fine, reversible adjustment where the gap budget allows one.
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The iron field-shaping catalogue (unordered; pick by geometry): vary hill/valley spanned angle with radius (horns), chamfer the pole end or add valley inserts to stop the field falling at large radius, decrease the gap with radius (elliptical gap), mill the lateral pole edges, add iron inserts or movable flaps, or change local saturation with trim rods.
Source quote & editorial note
The iron shaping methods zoo: Change the ratio of hill/valley spanned angle with radius ... Prevent field decrease at large radii ... Decrease the gap along radius ... Lateral edges milling ... Iron inserts ... Change local saturation
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 34-46
Editorial note, tabletop extrapolation: A menu of things the builder can machine on 8-inch pole tips, drawn from practice on real cyclotrons; movable flaps in particular give post-build adjustability. Unordered and geometry-dependent - model (FEMM) and map before machining any of them.
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Choose yoke stock by construction method - the quoted row: laminations are limited to about 300 mm stack thickness (200 mm usual) with good, slightly anisotropic magnetic and mechanical properties; the lecture's casting and forging rows carry their own trades (scan re-read queued).
laminated stack thickness: 300 mm max, 200 mm usualSource quote & editorial note
Laminated: Limited thickness : 300 mm max, usual 200 mm. Good magnetic and mechanical properties. Slight anisotropy.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 57
Editorial note, tabletop extrapolation: For an amateur the practical read is: mild-steel plate stock is fine for a DC magnet; note the anisotropy if you stack plate for pole tips.
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Trade pole gap deliberately: a small gap needs fewer ampere-turns and allows a smaller pole radius - which pushes the orbits close to the outer edge, leaves no room for probes, injection and pumping, and is very sensitive to errors (vertical losses); a large gap eases vacuum, injection, extraction and diagnostics at the cost of field.
Source quote & editorial note
small gap: reduced number of At of coils, pole radius reduced, orbits close to outer edge, no space, very sensitive to errors : vertical losses. large gap: large space: injection, extraction, probes, easier vacuum pumping, lower field
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 65
Editorial note, tabletop extrapolation: Frames the central decision for a next machine (the reference machine's chamber must fit in the gap) with the actual list of consequences on both sides.
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Follow the lecture's design order - step 0: squeeze the requirements; step 1: starting numbers by hand calculation; step 2: 2-D global model; step 3: 3-D global model; step 4: 2-D cuts for detailed local objects - preferring 2-D calculations wherever they serve.
step0 requirements -> step1 hand calculation -> step2 2D global -> step3 3D global -> step4 2D radial cutsSource quote & editorial note
step0: Squeeze requirements and extract juice; step1: Get starting numbers from hand calculation; step2: 2d global model; step3: 3d global model; step4: 2d cuts for detailed local objects ... 2d calculations must be preferred.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 68
Editorial note, tabletop extrapolation: A workflow a solo builder can actually execute, and it puts pencil-and-paper (Zickler-style) sizing ahead of any software.
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In a hill/valley magnet the average field at large radius is <B> = k*B_hill + (1-k)*B_valley with stacking factor k = N*theta_hill/360 (the source's k = hill-angle/90 is its four-sector case); RF efficiency prefers k = 0.5, compactness pushes k up - C235 chose k = 0.67 (60-degree hills).
<B> = k*B_hill + (1-k)*B_valley; k = N*theta_hill/360 (source's /90 form = four sectors); C235: k = 0.67Source quote & editorial note
For best RF efficiency, k=0.5 BUT to decrease machine dimensions k >0.5 (more hill, thus more field) CHOICE : k=0.67 (60 deg hills)
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 69
Editorial note, tabletop extrapolation: The arithmetic to go from a required <B> to hill/valley fields and sector angle - first-order and reusable at any scale, with fringe and gradient effects refining it in the field code.
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The source's design sequence: choose a target axial tune (their CHOICE: nu_z = 0.2), which then fixes the spiral angle once n, N and F are known; keeping flutter and spiral modest leaves room for a stronger field gradient.
CHOICE nu_z = 0.2; spiral angle xi then determined by nu_z^2 = n + (N^2/(N^2-1))F^2(1+2tan^2 xi)Source quote & editorial note
CHOICE : nu_z = 0.2. Flutter and spiral not too large. Field gradient can be strong. Spiral angle of pole completely determined since n, N, F and nu_z are known
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 69
Editorial note, tabletop extrapolation: Gives a numeric focusing target to design toward instead of 'as much focusing as possible'. On a classical weak-focusing machine at the reference machine's energies, nu_z = 0.2 means n = 0.04 - modest and achievable from pole-face falloff. The caveat belongs to AVF designs: there the isochronous average field RISES with radius (vertically defocusing on its own), and the flutter/spiral term must supply the whole tune, which is exactly why the source treats nu_z as a choice that determines the spiral angle.
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Field in the gap of an iron-dominated magnet is B = mu0*n*I/h - proportional to total ampere-turns, inversely proportional to gap, and independent of pole area; so minimize the reluctance of the iron path so the ampere-turns are spent on the gap.
B = mu0 n I / h (h = gap height)Source quote & editorial note
the field B = mu0 nI/h is proportional to the total current in the solenoid, is inversely proportional to the magnetic gap and is independent on the pole surface, a rather counter-intuitive fact to most people.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 70-71
Editorial note, tabletop extrapolation: The core sizing identity for a home magnet, in its regime (unsaturated iron, h the total effective gap): field follows ampere-turns over gap, and bigger poles alone buy nothing. Shaving the gap buys field at the price of chamber, dee and beam clearance (dg-163's trade) - cheap, not free.
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Remember permeability is a strong function of induction: it starts low (initial mu_r 50-150 for these materials), peaks at intermediate induction (maximum mu_r ~1000 for 0.9%-carbon steel against ~5000 for 99.8% iron), and falls toward 1 as saturation sets in - use low-carbon steel or better for yokes.
steel 0.9% C: mu_init 50, mu_max 1000; iron 99.8%: mu_init 150, mu_max 5000; iron 99.95%: mu_max 200,000Source quote & editorial note
Steel (0.9% C) 50 / 1000; Iron (99.8%) 150 / 5000; Iron (99.95%) 10,000 / 200,000
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 72-73
Editorial note, tabletop extrapolation: Concrete reason to buy A36/1018 low-carbon plate rather than whatever scrap steel is on hand for an H-frame yoke.
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Model a 3-D sectored magnet's AVERAGE properties in 2-D axisymmetry using pseudo-materials whose BH curve is scaled by the stacking factor: B_pseudo(H) = mu0*H + k*(B_iron(H) - mu0*H), k = fraction of the circle occupied by real material - a homogenization valid for average-field, flux-return and saturation studies, not for flutter, harmonics or spiral-edge focusing.
B_pseudo = mu0 H + k (B - mu0 H), k = stacking factor (fraction of azimuth filled by iron)Source quote & editorial note
The 3D geometry is modelled with a 2D code in axisymmetry using pseudo-materials. The stacking factor is the proportion of the circle occupied by the real material. Each pseudo-material is defined by a modified B-H curve
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 74
Editorial note, tabletop extrapolation: Lets a hobbyist study an AVF pole set's average field and yoke sizing in free 2-D codes (POISSON/FEMM) before committing to a 3-D solver; the azimuthal flutter and edge focusing that make an AVF machine work need the 3-D model or measurement.
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Control the mesh yourself where you need field derivatives, since the code gives potentials but tunes need first and second derivatives; a limited number of quadratic elements beats many linear elements for accuracy.
Source quote & editorial note
YOU must be in control of the mesh, not the code. A limited amount of quadratic elements is much more effective to accuracy than many linear elements
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 83
Editorial note, tabletop extrapolation: Explains noisy field-index curves out of a home simulation: n and nu_z are derivatives, so mesh quality matters far more than for B itself.
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Test your far-field boundary instead of trusting the code default, use symmetry boundaries where possible, and trust field codes for differences between two models more than for absolute values.
Source quote & editorial note
Is the rest of the universe far enough ? TEST IT! ... Codes are very good in the computation of small changes between 2 models but less good at absolute values.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 85-86
Editorial note, tabletop extrapolation: Practical simulation hygiene: use FEMM/POISSON to compare shim options (differences), and use the Hall probe for the absolute field.
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Give the average field a gentle radial decrease for axial focusing - the 86-inch used about 1% per 13 inches of radius (0.08%/inch) out to 20 inches, roughly 1.5% integrated, with azimuthal variation shimmed below 0.2%.
dB/B ~ -1%/13 in over the main region (~1.5% integrated to 20 in); azimuthal ripple < 0.2%Source quote & editorial note
The radial decrease in field strength is at a rate of one percent in 13 inches out to a radius of 20 inches ... These shims reduce azimuthal variations to less than 0.2%.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 15, 35
Editorial note, tabletop extrapolation: The fractional pattern transfers, not the inches: a smooth, monotonic few-percent center-to-edge fall-off with azimuthal ripple shimmed to the few-per-mille level is what the 86-inch exemplifies. The right numbers for an 8-inch pole come from its own n(r) stability requirement (dg-003, dg-119), not from this machine's profile.
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Machine field-correcting contour shims from thick steel plate (ORNL: 2 1/4 in. plate on a vertical boring mill) and iterate against field maps - the report describes changing shims and re-taking a complete field map in a few hours, and grinding 0.020 in. off a pole with a portable grinder to kill a localized high-field region after installation.
Source quote & editorial note
The shims were machined from 2 1/4 in. steel plate on a vertical boring mill ... The magnetization curve taken at the center of the tank with the contour shims in place is also shown. ... It is possible then to make minor changes in the shims and to take a complete set of field measurements in a few hours. ... After the contour shims were installed, field measurements indicated that the flux in an area of 3 to 4 square feet was ... higher than in the rest of the tank at corresponding radii. Approximately 0.020 in. of material from each pole over the area opposite the high field region was removed in about two hours with a portable grinder.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 35, 116
Editorial note, tabletop extrapolation: Directly applicable method: leave gap allowance for machined shim rings/plates so a next machine's field shaping is a measurement-and-remachining loop, not a magnet rebuild - and note ORNL fixed a residual local error by grinding the pole, so plan for both add and remove operations.
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Wind a small auxiliary coil on each pole (86-inch: 65 turns, up to 75 A) to steer the beam onto the magnetic median plane with a controllable field asymmetry.
86-inch control coils: 65 turns of #6 wire per pole, dc supply to 75 ASource quote & editorial note
By means of auxiliary coils wound on the pole pieces it is possible to control the position of the beam with respect to the median plane of the tank. The coils consist of 65 turns of #6 wire wound on each pole piece. A dc power supply provides up to 75 amperes
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 35
Editorial note, tabletop extrapolation: Cheap and direct for a next machine: an auxiliary winding on the poles gives a vertical-centering knob instead of mechanical re-shimming - size its ampere-turns from the field asymmetry the orbit calculation asks for (the 86-inch used up to ~4900 A-turns; a small machine needs proportionately less, but compute it), with a reversible supply and thermal check.
Cited in: Beam Dynamics: An Interactive Laboratory
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Site the RF power stage where the stray magnetic field is low - the cited machine mapped its fringe field and located the oscillator below ~60 oersteds (its copper-lined cabinet is the report's companion detail - re-read queued).
B_stray at oscillator < ~60 GSource quote & editorial note
A position of suitably low field intensity, < 60 oersteds, was located by mapping the stray field about the magnet.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 59
Editorial note, tabletop extrapolation: Map the reference machine's H-frame fringe field with a Hall probe and site the LDMOS amplifier, its magnetics and instrumentation by each component's OWN field tolerance - 60 G is the historical machine's siting outcome, not an immunity standard. Copper lining screens RF and electric fields, not the DC fringe; DC-sensitive items need distance or a high-permeability shield.
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Choose accessibility-driven machine orientation early: the 86-inch's U-shaped magnet 'gives direct access to the top of the vacuum chamber and permits the use of an overhead crane for transferring the assembled dee system' - the quoted rationale.
Source quote & editorial note
The U-shape of the magnet gives direct access to the top of the vacuum chamber and permits the use of an overhead crane for transferring the assembled dee system.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 7, 9
Editorial note, tabletop extrapolation: The principle (design the yoke around how you will service the chamber, not vice versa) is directly applicable to a next machine's H-frame layout.
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Design the magnet structure for magnetic forces, which dwarf vacuum loads (ORIC: 1,055,000 lb magnetic vs 60,000 lb vacuum), and machine mating pole/yoke surfaces flat and parallel within 0.005 inch at ~125 microinch finish.
mating surfaces: plane and parallel within +/-0.005 in TIR; 125 uin finishSource quote & editorial note
a magnetic load of 1,055,000 lb and a vacuum load of 60,000 lb could be expected ... mating surfaces of pole bases and yoke pieces to be planes within 0.005 in. T.I.R.
Editorial note, tabletop extrapolation: Direct transfer of the tolerancing practice: face-grind a next machine's pole and yoke mating surfaces and check with a dial indicator. Do not transfer the load ratio: at ORIC's scale the magnetic load dwarfed the vacuum load, but magnetic pressure is B^2/(2*mu0) - at 0.5 T about one atmosphere - so on a tabletop machine the two loads are comparable and the structure must carry both.
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Use plain low-carbon steel for cyclotron iron - the ORIC forgings ran ~0.11% C with low Si/Ni from consistent stock, per the report's specification - and a conventional closed yoke; ORIC's pole-base to yoke cross-section ratio was 1:1.
steel ~0.11% C; A_pole_base : A_yoke ~ 1:1 (closed yoke)Source quote & editorial note
The magnet is of a conventional closed-yoke design with a 1/1 ratio of pole base cross section to yoke cross section.
Livingston & Howard (eds.), The Oak Ridge Relativistic Isochronous Cyclotron — ORNL-2648, OSTI 4275955 (1958) — p. 118-119
Editorial note, tabletop extrapolation: Directly applicable: 1010/1018-class steel is the right iron for a next machine. On yoke sizing, the documented corridor runs from ORIC's 1:1 (pole BASE to yoke) to the +25-33% (pole FACE to return path) of dg-032 - the compared sections differ between sources, so pick one convention, apply it consistently, and check the narrowest section (dg-037).
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Prove magnet field designs on a scale model before cutting full-size iron: ORIC used ~1/8-scale models with a rotating-coil fluxmeter on a 1/4-inch measurement grid, achieving ~0.6% RMS point accuracy.
1/8-scale model; grid 1/4 in; error budget: recorder 0.2%, position 0.4%, current regulation 0.3% -> 0.6% RMSSource quote & editorial note
Approximately 1/8-scale model magnets were energized ... A complete grid of points 1/4 in. apart is thus obtained over the entire model.
Editorial note, tabletop extrapolation: Inverted for the builder: their whole magnet is model-sized, so a dense XY Hall-probe map - grid pitch chosen from the field structure you need to resolve - is the equivalent discipline, with an error budget drawn up for YOUR instrument chain (Hall calibration, angular alignment, temperature drift, positioning, current regulation) the way ORIC drew up theirs.
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Budget field-mapping errors explicitly: probe-position error dominates where gradients are steep - convert position uncertainty through the local gradient - and the source's techniques fell short of their desired 0.1% accuracy (their component error figures are report-attributed - re-read queued).
delta-B/B per point: position 0.4%, regulation 0.3%, readout 0.2%; goal 0.1%Source quote & editorial note
The error due to probe position varies depending on the field gradient ... techniques available to us at this time fall short of the desired 0.1% accuracy.
Editorial note, tabletop extrapolation: Directly applicable to a next machine's shimming: regulate and MONITOR magnet current during a map (in a linear magnet, current error maps ~1:1 into field error, so the regulation must beat the field goal, not just approach it), index the probe mechanically, and write the error budget with its combination rule before trusting shim-sized differences.
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When choosing dee voltage, remember it trades against gap size: more volts require a larger breakdown clearance and thus magnet hill gap, so 'some compromise must be reached' - ORIC's compromise landed at 100 kV (their reasoning: scan re-read queued).
V_dee up -> turns down, but gap (breakdown clearance) up -> compromiseSource quote & editorial note
Increasing the dee voltage, however, requires increasing the required voltage breakdown gap and thus the magnet hill gap, so that some compromise must be reached.
Editorial note, tabletop extrapolation: The coupled optimization transfers: pick a next machine's dee voltage and magnet gap together, since dee clearance ultimately costs ampere-turns and field.
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Design beam extraction simultaneously with the magnet from the start, so the deflection scheme is built into the machine instead of being retrofitted against a finished field.
Source quote & editorial note
the design of the beam deflection system will be worked out simultaneously with the design of the magnet ... all the problems which arise from trying to obtain deflected beams after the machine is built would be avoided.
Editorial note, tabletop extrapolation: Directly applicable lesson for a next machine: if an extracted beam is ever wanted, reserve the azimuthal slot, field-edge profile, and feedthrough ports now, even if the deflector comes later.
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For coil power, dissipation is inversely proportional to conductor volume, so choose power first and volume follows; keep packing ratio above 0.5 and size cooling water as q(gpm) = 6.82 x U(kW) / dT(degF).
P = rho*(NI)^2*l_turn^2/V_Cu (V_Cu = copper volume; with gross coil volume multiply the denominator by packing factor f); packing ratio > 0.5; q(gpm) = 6.82*U(kW)/dT(degF)Source quote & editorial note
power varies inversely with volume of conductor, so to a first approximation it can be chosen at will ... a well-designed coil will have a 'packing ratio' greater than 0.5.
Livingston & Blewett, Particle Accelerators (1962) — p. 273-277
Editorial note, tabletop extrapolation: If a next machine's coils run hot, more copper is a fix on equal footing with more cooling: doubling conductor volume halves dissipation at the same ampere-turns - paid for in coil size, weight and winding-window space.
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Bond coils into solid resin (epoxy/polyester over glass or cotton tape) so conductors cannot move under magnetic forces; turn-to-turn resin-glass insulation is good for >100 V/mil, but use mica for the higher voltage-to-ground insulation.
resin-impregnated glass/cotton: >100 V/mil (10-30 mil layers); tensile 1000-3000 psiSource quote & editorial note
The voltage breakdown strength of a resin-impregnated layer of glass cloth or cotton mesh is usually over 100 volts/mil ... necessary to utilize mica-sheet or mica-flake insulation to obtain the higher voltage-to-ground insulation.
Livingston & Blewett, Particle Accelerators (1962) — p. 278
Editorial note, tabletop extrapolation: Potting the reference machine's coils stops the slow insulation abrasion that coil hum causes. The >100 V/mil figure is the source's historical material datum, not an allowable design stress: size insulation from maximum turn-to-turn and coil-to-ground voltage with margin for voids, transients, creepage and temperature - the quote itself reserves voltage-to-ground duty for mica - and prove the finished coil with a hipot test rather than resting on the coupon number.
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The ANL 60-inch maintained cooling water demineralized at conductivity 10 micromho or less with pH about 7, and held dee cooling-water temperature stable to 1 F or better for steady operation.
sigma <= 10 umho/cm, pH ~7, dee water dT stability <= 1 FSource quote & editorial note
The conductivity is maintained at 10 micromhos or less, with a pH of about seven. Dee system water temperature stability of 1 F or better is required for steady operation.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 6
Editorial note, tabletop extrapolation: Two portable METHODS, not specs: monitor conductivity and pH on any hollow-conductor DI loop, and stabilize dee-water temperature if a next machine water-cools the dee (the RF tune walks with dee temperature). Set the actual limits from conductor material, voltage to ground, and measured RF drift, not from ANL's numbers.
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Size the cooling plant with about 3x margin over normal load (ANL: 1000 kW capacity vs ~300 kW normal operating load).
plant capacity ~ 3x normal heat loadSource quote & editorial note
The circulating pumps and heat exchanger are sized to handle a 1000-kw heat load, with the normal operating load being about 300 kw.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 6
Editorial note, tabletop extrapolation: For a next machine dissipating 1-5 kW, real margin over normal load is what makes long runs boring - ANL carried about 3x; pick your own factor from duty cycle, ambient conditions and fouling allowance rather than copying the ratio.
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Cool the RF matching secondary coil with oil or deionized water: even minute thermal expansion of the copper changes its inductance, detuning the network - which, uncompensated at fixed drive frequency, typically drops the dee voltage.
Source quote & editorial note
It is necessary for the secondary coil to be cooled with oil or deionized water... because even minute thermal expansion of the copper can change the inductor's value.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 23
Editorial note, tabletop extrapolation: Explains RF drift during long runs at the reference machine's power levels; cooling the tank coil stabilizes tune.
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The source's water-cooled 1/4 in x 1/4 in hollow square copper conductor, properly cooled, safely carried about 120 A; they designed the magnet to run at 110 A for margin.
source rating: ~120 A when properly cooled; operated at 110 ASource quote & editorial note
When properly cooled, our 1/4''x1/4'' hollow copper conductor can safely carry up to 120A. Allowing a margin of safety, we designed our magnet to operate at 110A.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 32
Editorial note, tabletop extrapolation: A conductor rating like this is conditional on the cooling that produced it - wall thickness, bore, flow, inlet temperature - so treat it as one documented data point for hollow-conductor coils, not a transferable ampacity. Rate a next machine's conductor from its own cooling calculation; the coil-geometry and magnet-power calculators cover the resistive side.
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Wind coils as 'double pancakes' (two-layer sub-coils with both leads exiting the same side): the source states this winding gives a more uniform field than a simple spiral.
Source quote & editorial note
Using this type of winding allows for a more uniform field than a simple spiral winding.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 32-33
Editorial note, tabletop extrapolation: A rebuild of the reference machine's 538 turns as potted double-pancakes with a cooling manifold is an attractive concept - as a design study: pancake count, potting, parallel water paths and repairability are engineering choices needing their own magnetic, hydraulic and thermal analyses, not properties the source's uniformity comparison confers.
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One machine's thermal envelope as calibration: the source magnet reports a 173 F (78 C) maximum and normal operation at no more than 142 F (61 C).
source magnet: T_normal <= 142 F (61 C), T_max 173 F (78 C)Source quote & editorial note
Our magnet can achieve a maximum temperature of 173 oF and will normally operate at no more than 142 oF.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 33
Editorial note, tabletop extrapolation: Set a next machine's potted-coil design point from the resin system's rated thermal class and a modeled or measured hotspot with margin for cooling failure - not from another magnet's numbers. Note 61 C at ordinary ambient is already a 36-41 C rise, looser than Tanabe's ~30 C-rise guidance for long potted-coil life.
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Pick the number of turns N to match the power supply once NI is fixed by the field requirement: large-N/low-I gives cheap thin cables but higher voltage, small-N/high-I gives low voltage, better copper packing and bulky connections - and N also drags resistance, inductance, stored energy and cooling geometry along, so the supply match is the starting constraint, not the only one.
NI fixed; N chosen from supply V/I window (Diamond dipole example: 40 turns, 1500 A, 500 V circuit)Source quote & editorial note
The value of number of turns (N) is chosen to match power supply and interconnection impedances.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 35-36
Editorial note, tabletop extrapolation: The reference machine's 538 turns were set by its supply; for a next machine, pick the surplus supply first and wind N = NI_required/I_supply - then check voltage compliance, inductance (and its dump-path consequences, dg-218) and cooling before committing.
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Power-distribution cables are generally limited to a current density of about 1.5-2 A/mm^2 - the source's benchmark for what conductors carry without engineered cooling.
j (power cables) < 1.5-2 A/mm^2 (source's general figure)Source quote & editorial note
Power distribution cables... are generally limited to a current density of <1.5 to 2 Amps/mm2.
Editorial note, tabletop extrapolation: An orientation point, not a coil rating: magnet coils differ from distribution cables in bundling, enclosure and heat path. The coil-specific limits are dg-092's - voluminous enclosed coils are held to 1 A/mm^2, and water cooling is what opens the range upward.
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Choose water-cooled coil current density near the canonical j = 10 A/mm^2 (economic optimum in worked example was flatter, ~4 A/mm^2; the higher value trades operating cost for smaller, cheaper coils).
j_design ~ 10 A/mm^2 water-cooled (economic optimum ~4 A/mm^2)Source quote & editorial note
the optimum is flat and appears to be j=4 Amps/mm2. However, a higher design value (the canonical j=10 Amps/mm2 value) is generally chosen.
Editorial note, tabletop extrapolation: For a home machine the source's trade often runs toward the low end: hand-wound coils and metered power favor the ~4 A/mm^2 economic optimum, and the reference machine's tubing coil runs lower still. Window space and magnet size push the other way - which is why the canonical 10 exists - so do the two-line cost comparison for your own copper and power prices.
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Compute coil water pressure drop with the Darcy-Weisbach relation P = 0.433*f*(L/d)*(v^2/2g), using the Darcy friction factor f = 64/Re for laminar flow (Re < 2000) and the smooth-tube turbulent solution for Re > 4000; design in the turbulent regime for good heat transfer.
P[psi] = 0.433*f*(L/d)*(v^2/2g); Re = v*d/nu; nu(water, 20 C) ~ 1.08e-5 ft^2/s (1.0e-6 m2/s); f = 64/Re (Re < 2000); avoid designing in the 2000-4000 transition bandSource quote & editorial note
f = 64/Re for laminar flow Re < 2000. For turbulent flow (Re>4000), the friction factor is gotten by solving a transcendental equation.
Editorial note, tabletop extrapolation: The straight-passage core of hydraulic sizing for any hollow-conductor or tubing-wound coil - add bends, fittings and manifold (minor) losses on top, and confirm with a flow test; the formula alone is the floor, not the whole recipe.
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Water temperature rise through a coil is dT(C) = 3.8*P(kW)/q(gpm); design for <10 C rise, and never exceed ~30 C rise (with 20 C inlet) if you want long potted-coil life.
dT[C] = 3.8*P[kW]/q[gpm] - standard water heat-capacity arithmetic in US units, not from the quote; quoted targets: < 10 C desirable, < 30 C maximum (20 C inlet) for long potted-coil lifeSource quote & editorial note
Desirable temperature rise... < 10 deg. C. Maximum allowable temperature rise (assuming 20 deg. C. input water) < 30 deg. C for long potted coil life.
Editorial note, tabletop extrapolation: One-line flow-rate calculator: a 1 kW coil on a next machine needs ~0.4 gpm for a 10 C rise.
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Keep cooling-water velocity below 15 ft/s in coil passages; above that, flow-induced vibration erodes the water channel over time.
v_water < 15 ft/s (4.6 m/s)Source quote & editorial note
For water velocities > 15 fps, flow vibration will be present resulting in long term erosion of water cooling passage.
Editorial note, tabletop extrapolation: The cited source's upper design guideline when sizing pump and passage diameter for a hollow-conductor coil; onset of vibration and erosion also depends on bend severity, passage geometry, material and water chemistry, so use a lower limit where conductor-manufacturer guidance or testing warrants.
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Doubling the number of parallel water circuits cut required pressure drop by a factor of eight in the source's sizing (P ~ 1/Nw^3, valid when each circuit's length and flow both scale as 1/Nw at fixed passage diameter and friction factor): subdivide the coil rather than buy a bigger pump.
P ~ 1/Nw^3 under fixed d and f with length and flow per circuit ~ 1/Nw; recompute per branch with real lengths, Reynolds-dependent f and manifold lossesSource quote & editorial note
Pressure drop can be decreased by a factor of eight if the number of water circuits are doubled.
Editorial note, tabletop extrapolation: Argues for manifolded pancake sub-coils on a next machine instead of one long series water path through 538 turns.
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Cooling-passage pressure drop falls dramatically with hole diameter - roughly as 1/d^5 in the fixed-flow, fixed-friction-factor turbulent approximation - so a slightly larger hole slashes pump requirements, and an undersized (out-of-tolerance) hole blows the hydraulic budget.
P ~ 1/d^5 (fixed volumetric flow, ~fixed Darcy f; laminar flow gives ~1/d^4)Source quote & editorial note
If the design hole diameter is increased, the required pressure drop is decreased dramatically. If the fabricated hole diameter is too small... pressure drop can increase substantially.
Editorial note, tabletop extrapolation: When choosing hollow conductor for a next machine, weigh bore against copper cross-section (a bigger hole raises electrical resistance) and flow-test each pancake before potting - the fabricated bore, not the drawing, sets the pressure drop.
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Wind each water circuit from one continuous length of conductor - no splices buried in the potting (the quoted requirements) - with the lecture's companion QA practices: a chip-free winding area, and a pre-winding ball test blowing a ball of <= 80% of the cooling-hole diameter through the passage (per its coil-quality pages: scan re-read queued).
ball diameter <= 0.8 * cooling-hole diameterSource quote & editorial note
A single water circuit in a coil assembly should be wound from a single continuous length of conductor. Splices 'buried' within the potted insulation should not be allowed.
Editorial note, tabletop extrapolation: For a next machine wound from copper refrigeration tubing: buy one continuous coil per water circuit, keep the shop swarf away from the winding, and verify the bore is clear before the tubing is buried in the stack.
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Impulse-test coils for intermittent turn-to-turn shorts during fabrication: pulse a capacitor into the coil and watch the ringdown on a shielded pickup loop, starting at ~10 V/turn and raising to 200 V/turn or 2 kV maximum - a healthy coil's waveform only scales in amplitude, while frequency/damping changes or 'hash' at the peak indicate a short. After potting, hipot to twice the operating voltage plus 1 kV with drainage current under 2 mA/kV.
impulse: 10 V/turn up to 200 V/turn or 2 kV; hipot: 2x operating voltage + 1 kV, leakage <= 2 mA/kVSource quote & editorial note
The procedure consists of starting with a low voltage pulse (~ 10 Volts/turn) and increasing the voltage until one reaches 200 Volts/turn or 2 kV maximum and observing the waveform. ... A sick coil will exhibit waveforms whose frequency and/or damping rate changes as the voltage increases or will exhibit hash at the peak of the damped sinusoid. ... After potting, the coil should undergo a hipot test. ... Specifications normally call for raising the voltage in the coil to twice the operating voltage plus one kV. The maximum drainage current is usually set at 2 mAmps/kV.
Editorial note, tabletop extrapolation: A pulse source, capacitor and scope let the builder screen the next machine's coils before they are trapped under the yoke - run the impulse test during fabrication, before the coil goes on the core, and photograph the low- and high-voltage waveforms as the baseline. Both tests put hazardous voltage on the coil: use rated, current-limited test gear, discharge and ground between steps, and keep others clear.
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Measure actual coil water flow at the real supply pressure and water temperature rather than trusting handbook calculations - bends that are tight relative to the passage size add flow impedance the straight-pipe formulas miss.
Source quote & editorial note
Water flow calculations made for the preliminary design may be unreliable for a coil designed with many tight turns... due to the added flow impedance of tight radius turns.
Editorial note, tabletop extrapolation: A bucket-and-stopwatch flow test at operating pressure is the real spec for the reference machine's 538-turn tubing coil (many turns; check its bend radii against the passage size). Record water temperature - viscosity matters most if any branch runs laminar - and measure each parallel branch separately, since a total-flow test hides an imbalance.
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Use non-conducting cooling water hoses at least 1 m long between manifold and coil to limit leakage current, make the water inlet fitting smaller than the outlet, and put the flow-interlock orifice on the return manifold.
hose length >= 1 m, non-conductingSource quote & editorial note
Water hoses should be at least one meter long and use nonconducting material to prevent current leakage from the magnet. The water “in” fittings should be smaller than the water “out” fittings ... If a flow interlock (orifice plate) is used, it should be attached to the return manifold.
Editorial note, tabletop extrapolation: The reference machine's water-cooled copper-tubing coil sits at supply potential; a meter of non-conducting hose per lead limits leakage current, and an interlock on the return detects a blocked circuit - cheap practices worth copying at home scale. They reduce specific risks; they are not shock protection as a whole, which still rests on earthing and supply-side protective devices.
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Fit each coil water circuit with a thermal interlock switch (Klixon) set near 89 C, mounted on the water-return end of the current-carrying conductor via a hard-soldered block, wired to kill the power supply.
trip ~89 C, reset ~70 C, one interlock per water circuit, all in seriesSource quote & editorial note
The normal set-point of Klixons is about 89 C. It will generally reset at about 70 C ... One thermal interlock is installed on each water circuit ... All the interlocks on one magnet are connected in series. ... The Klixon is preferably mounted on the water return lead of the coil ... always mounted on the current carrying portion of the conductor ... mounted to a block hard-soldered to the conductor.
Editorial note, tabletop extrapolation: A thermal snap-switch soldered to the coil exit tube, wired in series with the supply enable, is cheap, high-value protection against cooking a winding on a lost-water event - alongside the flow interlock (dg-202), not instead of it. Set-point and switch rating are the designer's to verify against the winding's own insulation limit.
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Insulate coils to scale (the source's ranges): inter-turn insulation 0.3-1.0 mm; ground insulation 0.5-3.0 mm depending on the applied voltage.
inter-turn 0.3-1.0 mm; ground 0.5-3.0 mm (the varnish/Kapton thicknesses and 0.63-0.8 fill factors were uncited - removed pending re-read)Source quote & editorial note
Inter-turn insulation thickness is normally between 0.3 mm and 1.0 mm, the ground insulation thickness should be between 0.5 mm and 3.0 mm depending on the applied voltage.
Editorial note, tabletop extrapolation: Sets expectations for how much winding window the insulation eats on a hand-wound 538-turn coil - then compute the actual packing factor from the chosen conductor's finished insulated dimensions and the real winding layout, since fill depends on shape, pattern and voids, not on insulation thickness alone.
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Wind hollow conductor with a bending radius at least four times the conductor width: at three widths the source expects 3.6% keystoning - local cross-sectional distortion at the bend - and recommends four widths so the effect can be ignored.
R = 3A -> ~3.6% keystoning (local distortion, not cumulative per-bend growth); use R >= 4A for the source's rectangular hollow conductorSource quote & editorial note
For a bending radius of three times the conductor width we can expect a keystoning of 3.6% ... we can ignore the effect of keystoning by systematically choosing a bending radius four times larger than the conductor width.
Editorial note, tabletop extrapolation: For bending round copper tubing on a homemade coil the analogous risks are ovalization and bore pinch: use tube-specific minimum-bend-radius and ovality limits (diameter, wall, temper and tooling all matter), inspect or flow-test the formed passage, and watch the insulation at the bends.
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Dimension the coil pack with cross-section A = N*I/(j*fc), an aspect ratio (height:width) between 1:1 and 1:2, and a packing factor fc of 0.6-0.8.
A = b*c = N*I/(j*fc) - the standard winding-window equation, correct with fc as the conductor-area fraction (not from the quote); quoted ranges: c:b between 1:1 and 1:2, fc = 0.6-0.8Source quote & editorial note
An aspect ratio of c:b between 1:1 and 1:2 should be chosen, and the packing factor fc somewhere between 0.6 and 0.8.
Editorial note, tabletop extrapolation: Turns the amp-turn number into an actual coil window size before you buy tubing or start winding.
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Split coils into more parallel water circuits before enlarging the pump: pressure drop scales as 1/Kw^3 (doubling the number of circuits cuts dp by a factor of 8) and as 1/d^5 in channel diameter.
dp ~ 1/Kw^3; dp ~ 1/d^5Source quote & editorial note
This implies that for a given flow, the pressure drop is reduced by a factor of eight by doubling the number of cooling circuits.
Editorial note, tabletop extrapolation: Explains why splitting a big coil into 2 or 4 hydraulic circuits lets a garage chiller pump do the job - under the model's conditions: total flow and total conductor length fixed, circuits dividing both equally; then pressure drop falls as the cube of the circuit count. Confirm the friction regime still holds after the split.
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Feed hollow-conductor coils with demineralized water at resistivity > 0.1 MOhm*m, pH 6-6.5, and dissolved oxygen below 0.1 ppm, with filters near the magnet; poor water quality eventually causes shorts and corrosion leaks.
rho > 0.1e6 Ohm*m; pH 6-6.5; O2 < 0.1 ppmSource quote & editorial note
Water resistivity higher than 0.1x10^6 Ohm m; pH-value between 6 and 6.5; dissolved oxygen below 0.1 ppm
Editorial note, tabletop extrapolation: If a next machine uses water-cooled coils at supply potential, ordinary tap water misses all three quoted limits. A deionizing cartridge loop is the standard way to hold resistivity, but the spec is three-dimensional - oxygen and pH need their own control - and the source pairs the water spec with filters near the magnet.
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Convectively cooled power-distribution cables are limited to j <= 1.5 A/mm^2 - the source's figure for that service.
j_air <= 1.5 A/mm^2Source quote & editorial note
power distribution cables are convectively cooled and are limited to <= 1.5 Amps/mm2
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 128-129
Editorial note, tabletop extrapolation: For the reference machine's circuit: any leg - bus, jumper, lead - running above ~1.5 A/mm^2 without an engineered cooling path will run warm, so size leads generously. Above the line the options are any real cooling: water, forced air, conductive sinking, or intermittent duty with temperature monitoring (dg-220).
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Use the source's normally-good current density j = 10 A/mm^2 for water-cooled magnet coils and a packing fraction of ~0.5 for small conductors; the lecture's first-pass sizing also takes average turn length ~3x the magnet core length.
j = 10 A/mm^2 (water-cooled); f ~ 0.5; l_ave ~ 3*L_magSource quote & editorial note
Normally, a good value for the current density is j = 10 Amps/mm2 for water cooled coils... The value of the packing fraction is typically f ~ 0.5 for small conductors.
Editorial note, tabletop extrapolation: Lets the builder size a next machine's coil cross-section on one sheet of paper: gross winding area ~ NI/(j*f) = NI/5 mm^2 for water-cooled copper - a first pass the thermal calculation then confirms, and the 10 A/mm^2 presumes genuine water cooling (dg-092's geometry conditions).
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Design coil water circuits for turbulent flow (the lecture's Re >= 4000 criterion) but keep flow velocity <= 4 m/s to avoid vibration and erosion of the copper passage, and hold coil temperature rise dT <= 30 C to protect epoxy insulation - the lecture tightens toward ~15 C where field stability matters.
Re >= 4000; v <= 4 m/s; dT <= 30 C (15 C for stability)Source quote & editorial note
Flow velocity v <= 4 m/sec to avoid flow vibration and erosion... An acceptable coil temperature rise which protects the coil epoxy encapsulation from damage is dT <= 30 C.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 134-135
Editorial note, tabletop extrapolation: Direct water-cooling design window for a next machine's hollow-conductor coil; also warns that a lazy laminar-flow circuit cools far worse than the handbook film coefficient suggests.
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Estimate the coil power-weight tradeoff with kW x tons = 0.118 x (mega-ampere-turns)^2 x (mean turn length in inches)^2 for copper: the product of dissipation and weight is fixed by NI and geometry, so more copper always buys less heat.
kW x tons(Cu) = 0.118 x (MA-turns)^2 x (mean turn length in inches)^2 - the squared length follows from P*M ~ (NI)^2*l^2 and matches the 0.118 coefficient; the quoted line's missing exponent is likely transcription (scan re-read queued)Source quote & editorial note
Kilowatt-Tons = (0.118)Cu (Mega-ampere turns)^2 (inches mean turn length)
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Editorial note, tabletop extrapolation: Directly applicable trade study tool: the product of coil dissipation and coil weight is fixed by NI and geometry, so more copper always buys less heat.
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Wind coils to an approximately rectangular (square-ish) cross section around the poles; a coil that is too flat or too tall intercepts more leakage flux and wastes turns.
Source quote & editorial note
The coils should be wound so that they occupy approximately a rectangular cross section around the poles ... Either too flat or too tall a coil intercepts more leakage flux and thus wastes turns.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable guidance for a next machine's coil geometry.
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Limit close-wound naturally air-cooled coils to 750 A/in^2 of conductor continuously, 1000 A/in^2 for intermittent runs.
J <= 750 A/in^2 (1.16 A/mm^2) continuous, air-cooled; <= 1000 A/in^2 intermittentSource quote & editorial note
operate close-wound naturally air-cooled coils at a current density not exceeding 750 amps per square inch of conductor area. For intermittent operation this may be raised to 1000 amps per sq. in.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable thermal sizing for coils matching the quoted conditions - close-wound, naturally air-cooled: 750 A/in^2 continuous, 1000 intermittent. A different winding style (open spacing, forced air, tubing with internal flow) carries different limits - dg-092's geometry table is the map.
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Favor large conductor cross-section and high current over many turns at high voltage; this simplifies both insulation and winding.
Source quote & editorial note
Most coil designs favor large conductor areas and correspondingly high amperages; this reduces total voltage and simplifies both the insulation and the winding problems.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable when choosing wire gauge and supply for a next machine's coils.
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Wouters: flat donuts of 1/16 in. copper sheet with 1/4 in. copper pipe soldered to the outer edges, interleaved between pancake windings as cooling plates, should operate steadily at about 1300 amps per square inch.
J ~ 1300 A/in^2 (2.0 A/mm^2) with interleaved water-cooled donut platesSource quote & editorial note
flat donuts of 1/16 in. copper sheet ... having a 1/4 in. copper pipe soldered to the outer edges ... such coils should operate steadily at 1300 amps per sq. in.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 4
Editorial note, tabletop extrapolation: A cheap construction to reach for when a next machine's pancake coils run hot: 1/16-inch copper donut plates with soldered edge tubing between pancakes. The 1300 A/in^2 is the historical design target for that geometry, not a number to adopt - recompute I^2R, water flow and temperature rise, the thermal path through the insulation, and solder and tube reliability, then measure winding temperature in operation. [Note revised 2026-08-23: earlier note called it a directly applicable upgrade that 'nearly doubles' allowable excitation.]
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Beware thermal margins on hobby-scale coils: the 6-inch's 6000-turn #13-wire coils reached iron saturation (~20 kG) below 10 A but overheated in under an hour at that current.
6-in example: 6000 turns #13 DSC wire, ~20 kG at <10 A, <1 hr thermal limitSource quote & editorial note
These windings saturate the iron (~20 KG) at somewhat less than ten amperes; at this current the temperature becomes excessive in less than an hour
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 4
Editorial note, tabletop extrapolation: Directly applicable cautionary datum: quote coil ratings as (current, time-to-overheat) pairs, not just maximum field.
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Never open the magnet coil circuit at high current without surge protection (thyrite resistor or electrolytic dump tank) across the coil.
Source quote & editorial note
The magnet coil circuit must never be broken at high currents, of course, unless adequate surge protection is provided.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 5
Editorial note, tabletop extrapolation: Directly applicable: any magnet coil whose stored energy exceeds a few joules needs a dump path across the winding - freewheel diode, varistor, or resistor - rated for the coil's stored energy, peak current and clamp voltage. Without one, opening the circuit at current can arc the switchgear.
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Size the Dee tank circuit from the Dee capacitance: on the cited machine ~76 pF of Dee against a 0.87 uH secondary resonates up to 19.5 MHz (411 keV protons at its 1.28 T maximum field), with both inductors wound from 1/4 inch copper tubing coaxially - 6 cm diameter primary outside a 4 cm secondary - and coupling set by swapping primaries of different turn counts.
cited machine: C_dee ~ 76 pF, L >= 0.87 uH -> f up to 19.5 MHz; 1/4 in copper tubing; 6 cm dia primary over 4 cm dia secondary; interchangeable primaries set couplingSource quote & editorial note
the Dee may be oscillated with voltage amplitudes of up to approximately 3000V relative to the grounded Dummy Dee. The Dee capacitance is approximately 76 pF. The secondary coil inductance of 0.87 uH or more in parallel with the Dee capacitance yields a resonance as high at 19.5 MHz, which is the maximum cyclotron frequency corresponding to 411 keV protons in the maximum magnetic field of 1.28 T. ... These inductors are 1/4 inch copper tubing, wound coaxially, with the 6 cm diameter primary coil outside the 4 cm diameter secondary coil. The inductance of the primary coil can be changed by replacing the coil with one having a different number of turns, several of which have been constructed
Editorial note, tabletop extrapolation: Concrete worked values at the same scale, but measure your own machine's total capacitance (dee + stray + coil) and size the coil from L = 1/((2*pi*f)^2 * C_total); the swappable-primary approach lets you retune coupling without rebuilding the tank. The 411 keV is that machine's figure at its own field and extraction radius.
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Watch coil insulation temperature: the coil manufacturer's table halves expected insulation life roughly every 8 C (8-40 years at 79 C, 4-20 at 87 C) with 130 C the maximum allowable; ORNL alarmed at 70-80 C, and coils take 1-3 hours to reach thermal equilibrium.
life ~ halves per ~8 C and 130 C max allowable (manufacturer's table, this coil); alarm 70-80 C; t_equilibrium ~ 1-3 hSource quote & editorial note
An alarm warns the operator when the coil temperature has reached a predetermined value, usually 70 to 80 C ... one to three hours are required for the temperature to reach equilibrium ... the maximum life of the magnet coil insulation, which the manufacturer estimates will vary with temperature as follows: [table: 79 C, 8-40 years; 87 C, 4-20 years; ... 130 C maximum allowable]
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 33
Editorial note, tabletop extrapolation: Directly applicable: put a thermocouple in the next machine's winding and log it; a coil that is fine at 30 minutes can still cook at 2 hours. The 130 C figure is this manufacturer's rating for this insulation - a next machine's ceiling is its own insulation's thermal class.
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Put filter and tank inductors in the direct airstream of a cooling fan; coils outside the airflow run hot even when the semiconductors are fine.
Source quote & editorial note
It is important for the coils should be in the air stream of one of the cooling fans (they will run hot if not).
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 28
Editorial note, tabletop extrapolation: Applies to the homemade dee-tank coil: assess its RF loss and temperature under the intended loaded-Q and coupling conditions (resonator circulating current depends on Q and coupling, not on the DC feed), and give it forced air if it runs hot.
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Do not put exposed nickel in a high-RF-current path: a nickel-plated 19 MHz copper-tube tank coil ran at 350 C (near nickel's Curie point) where the identical bare-copper coil ran at 65 C. A nickel underlay beneath chrome or silver is suspect unless the top conductive layer is continuous and several skin depths thick at the operating frequency.
ferromagnetic plating: delta shrinks with permeability; Ni (mu~500) delta = 0.00025 in at 1 MHz vs Cu 0.0025 inSource quote & editorial note
This operated normally at 65 C but when an identical coil, which had been nickel plated, was substituted, the operating temperature rose to 350 C.
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 4
Editorial note, tabletop extrapolation: Reject nickel-plated hardware anywhere RF current flows in the resonator, coil, or ground-return path unless the overplate is verified thick and continuous - or validate by measuring loss and temperature.
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Specify electrical-grade copper for RF parts: common phosphorus-deoxidized copper tube (0.015-0.08% P) runs only 60-90% IACS conductivity, versus ~100-101% minimum for certified electrical grades (C11000/C10100).
P-deox Cu tube: 60-90% IACS; electrical grade: ~100-101% IACS min (certify, don't assume); Rs ~ 1/sqrt(sigma), so the conductivity gap is worth ~6-23% in RF surface resistanceSource quote & editorial note
Most commercially available copper tube contains 0.015% to 0.08% phosphorus as a de-oxidising agent, so that its conductivity may range from 60% to 90% I.A.C.S.
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 6
Editorial note, tabletop extrapolation: Buy the tank-coil tubing as electrolytic/electrical-grade (C10100/C11000) copper with certified conductivity, not generic plumbing tube - worth roughly 6-23% lower RF surface resistance depending on where the plumbing tube fell in its range.
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Practical single-layer air-core coils typically reach true Q up to about 800; very few circuits need Q above 900, and designs much over 1000 usually force abnormal physical dimensions.
typical practical true Q up to ~800; Q much over ~1000 usually means abnormal dimensionsSource quote & editorial note
typically have true Q values of up to about 800. Very few practical circuits require a Q above 900. Attempting to design a coil with a True Q much over 1,000 usually results in a coil with abnormal physical dimensions
Murphy, The Elusive Q of Single-Layer Air-Core Coils — CQ Magazine, May 1999 (1999) — p. 1
Editorial note, tabletop extrapolation: Do not budget the resonant step-up on textbook thousands: measure or model the loaded Q of the actual resonator under representative coupling (loaded Q sits well below the coil's unloaded Q), then size the amplifier for 5-13 kV dees from that measurement.
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Expect a Q meter to read below true coil Q: the instrument measures circuit Q, and the coil's distributed capacitance loads the reading down.
Q_measured < Q_true (distributed-capacitance error); circuit Q != coil QSource quote & editorial note
the presence of the coil's distributed capacity causes the Q observed by the Q meter to be lower than the true Q of the coil
Murphy, The Elusive Q of Single-Layer Air-Core Coils — CQ Magazine, May 1999 (1999) — p. 1
Editorial note, tabletop extrapolation: For the cited Q-meter method, treat the reading as a lower bound and keep leads and fixture capacitance minimal. A VNA measurement is a different animal: state whether loaded or unloaded Q is being extracted, calibrate and de-embed the fixture, and include the distributed capacitance in the fit - VNA errors can bias either direction.
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Q increases with coil diameter and with frequency within the source's tested single-layer geometries, so for a given inductance at HF prefer the physically largest coil practical.
Q rises with dia (3-30 MHz charts: 1.0 in dia ~300-500 vs 4.0 in dia ~2000-3000) and with sqrt-like frequency dependenceSource quote & editorial note
Q increases with coil diameter (see figs. 1-4). Q increases with coil length, rapidly when the L/d ratio is small ... Q increases with frequency
Murphy, The Elusive Q of Single-Layer Air-Core Coils — CQ Magazine, May 1999 (1999) — p. 1-2
Editorial note, tabletop extrapolation: At 9 MHz a 3-4 inch diameter tank coil in the charted geometries reads Q over 1000. At fixed frequency and capacitance the dee voltage scales as sqrt(P*Q) - doubling Q at the same drive buys about 40% more voltage, not double - so treat Q gains as helpful, and verify with the loaded Q actually measured.
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Wind single-layer HF coils with conductor diameter between 0.45 and 0.70 times the center-to-center turn spacing; the source notes not all commercial stock coils meet this condition.
0.45*S <= wire_dia <= 0.70*S (S = center-to-center turn spacing)Source quote & editorial note
The conductor diameter must be within the range of 0.45 and 0.70 times the center-to-center distance between adjacent turns (not all commercial stock coils meet this condition).
Murphy, The Elusive Q of Single-Layer Air-Core Coils — CQ Magazine, May 1999 (1999) — p. 2
Editorial note, tabletop extrapolation: For a 9 MHz matching/tank inductor, space the turns so the wire fills 45-70% of the pitch - close-winding bare tubing costs Q (proximity effect is the standard explanation, beyond this source's scope) - and check any stock coil against the ratio before trusting its rated Q.
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Maximum Q occurs at a coil length-to-diameter ratio between about 0.35 and 0.45, decreasing rapidly below that ratio and more slowly above it - aim near the optimum band.
Q peaks at L/d ~ 0.35-0.45; falls fast below, slowly above - stay near the band, erring slightly long if forced off itSource quote & editorial note
Maximum Q occurs at a coil L/d ratio of between (depending on other coil design parameters) 0.35 and 0.45, decreasing rapidly below that ratio and more slowly above
Murphy, The Elusive Q of Single-Layer Air-Core Coils — CQ Magazine, May 1999 (1999) — p. 2-3
Editorial note, tabletop extrapolation: Make the resonator coil short and fat (length a bit under half its diameter), not the long skinny solenoid that fits most easily in a corner - and not a pancake either: below the optimum Q collapses quickly.
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Do not trust simple coil design equations outside their validity range: L/d below 0.35, fewer than about 4 turns, or wire-to-spacing ratios outside 0.45-0.70.
Callender/Medhurst Q equations valid only for L/d >= 0.35, n >= ~4, 0.45 <= dia/S <= 0.70Source quote & editorial note
The equations do not hold for coils with a length-to-diameter ratio of less than 0.35:1, coils with less than about 4 turns, or coils with conductor diameter-to-turn spacing ratios of less than 0.45:1 or greater than 0.70:1.
Murphy, The Elusive Q of Single-Layer Air-Core Coils — CQ Magazine, May 1999 (1999) — p. 3
Editorial note, tabletop extrapolation: A 2-3 turn link or coupling loop at 9 MHz is outside the formulas; measure it rather than calculate it.
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Estimate dee capacitance by summing parallel-plate sections of the dee-to-chamber geometry - the memo's three-section sum gave 77.5 pF calculated (70.5 pF top+bottom, 7.04 pF edge) against the quoted 78.1 pF measured on an L-C meter: 'Nice agreement seen!'
C_total = 2*A_top*eps0/d_top + A_edge*eps0/d_edge; Rutgers: 70.5 pF (top+bottom) + 7.04 pF (edge) = 77.5 pF vs 78.1 pF measuredSource quote & editorial note
Measurement of the capacitance with an L-C meter yields a value of 78.1pF. Nice agreement seen!
Editorial note, tabletop extrapolation: Directly usable on the reference machine's 8-inch dee: sum simple parallel-plate terms for top/bottom/edge and verify with a cheap L-C meter before winding the tank coil.
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Peak-to-peak dee voltage of an inductively coupled tank follows Vp-p = 2*sqrt(2*P*L/(Rs*C)), i.e. it scales as the square root of forward power; the square-root trend held over all measured power ranges (5 W to 1300 W).
Vp-p = 2*sqrt(2*P*L/(Rs*C)); Vpeak = sqrt(2*P*L/(Rs*C))Source quote & editorial note
the trend of DEE voltage to follow the square root law of the input RF power is accurate over all measured power ranges
Editorial note, tabletop extrapolation: The sizing equation for the reference machine's LDMOS upgrade - with P as the power actually DELIVERED to the tank: at a good match forward power approximates it; otherwise net out the reflected fraction first. Doubling dee voltage costs 4x power, so 1.3 kV to 5-13 kV needs a 15-100x power increase unless L/C or Rs improves (dg-239's knobs).
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Do not budget a tank's effective series resistance from the coil alone: the Rutgers coil computed ~50 mOhm (1.3 mOhm/inch of 1/4-inch Cu tube), but the assembled system behaved 'as if Rs had the value of 800 mOhm' - an INFERRED effective series resistance sixteen times the coil's, which the memo attributes to the stainless chamber return, the stainless Conflat stem support, and the feedthroughs.
Rutgers: Rs_coil ~ 0.05 ohm estimated, Rs_system 0.8 ohm measured (16x). The factor is specific to that return path, stem, feedthroughs and frequencySource quote & editorial note
as if Rs had the value of 800mOhm - sixteen times that of the expected coil Rs ... take into account the stainless steel vacuum chamber return, the stainless steel Conflat DEE stem support and RF feed throughs.
Editorial note, tabletop extrapolation: When predicting a next machine's dee voltage, include every RF current path - chamber return, stem, feedthroughs, contacts - and prefer copper returns where possible; then measure the assembled tank's Q and infer Rs from it rather than assume a multiplier. [Note revised 2026-08-23: earlier note told the builder to 'expect ~1 ohm scale Rs', a number that belongs to Rutgers' geometry.]
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On the source apparatus the direct HV probe stopped tracking above ~200 W forward power (the P6015 departed from the sqrt-P trend, behaving like a high-resistance breakdown) while the chamber's capacitive pickup kept following the theoretical trend - so they calibrated the pickup against forward power at low level and used the pickup alone at high power.
Rutgers: Dee Vp-p = 3710 x pickup Vp-p (R^2 = 0.994), used on that apparatus to at least 1300 WSource quote & editorial note
after a power level of 200 watts, the measured voltage of the P6015 probe departed from the trend and dropped below the expected value. It is as if an additional resistance is introduced. The behavior was similar to that of a high-resistance break-down ... while the P6015 probe's value deviated from the trend, the induced voltage on the chamber's capacitively coupled pickup continued to followed the trend which was consistent with the theoretical model ... the induced voltage on the capacitive pickup facing the DEE was calibrated against forward power at lower levels. Extrapolation allowed us to measure forward power levels up to 1300 watts
Editorial note, tabletop extrapolation: The measurement chain for the LDMOS upgrade, rebuilt on the reference machine's own hardware: calibrate its pickup against an independently validated dee-voltage measurement over an overlapping safe range, confirm linearity and unchanged tuning, and never transfer the 3710 ratio or the power breakpoints between machines.
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A high-voltage probe loads the tank measurably - the Tektronix P6015 added 3.0 pF and shifted the resonant frequency accordingly - so retune or correct for probe capacitance whenever a probe touches the dee stem.
delta-C_probe = 3.0 pF (P6015)Source quote & editorial note
the P6015 probe introduced 3.0pF of capacitance; the tank circuit was indeed reduced in frequency corresponding to 3 pF
Editorial note, tabletop extrapolation: With the reference machine's ~78 pF-class dee, 3 pF is a ~2% frequency pull - enough to detune a high-Q tank, so calibrate with the probe on, then remove it and retune.
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Measure mutual inductance between coupling loop and tank coil by connecting them in series aiding then series opposing: the difference of the two measured inductances is 4M.
L_aiding - L_opposing = 4M; M = sqrt(Rs*Z)/(2*pi*f) at match (Rutgers: M ~ 0.02-0.07 uH)Source quote & editorial note
The connections to one of the coils are then interchanged and the equivalent inductance is measured again. The difference between the two measured inductances is then 4M.
Editorial note, tabletop extrapolation: A bench L-C meter trick for characterizing the coupling loop: measure series-aiding and series-opposing, difference is 4M. The M a matched loop NEEDS follows from M = sqrt(R_tank*Z_source)/omega with the tank's measured series resistance and the source impedance at the operating frequency - compute it for the actual tank rather than expecting a stock tens-of-nH answer.
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At critical coupling (maximum voltage transfer), the measured loaded Q is exactly half the unloaded Q0; measure Q from the FWHM of a weakly-probed S21 sweep, but a simple reflected-power meter showing zero reflection is a sufficient indicator of critical coupling.
Q_measured/Q0 = 1/(1 + (M^2*w^2/R2)/R1); Q_loaded = Q0/2 at critical coupling; Q = f0/dF_FWHMSource quote & editorial note
is exactly 1/2 of Qo when the primary is critically coupled corresponding to the value giving maximum response ... a simple reflected RF power meter will suffice to show a perfect match - indicating critical coupling.
Editorial note, tabletop extrapolation: The builder can tune their coupling loop with just an SWR bridge: adjust loop position/taps until reflected power nulls, and check Qloaded = Q0/2 with a NanoVNA S21 sweep.
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The Rutgers tank measured Q0 ~ 920 at its ~15 MHz test (loaded Q ~ 460 at match, confirming critical coupling) - a copper-refrigeration-tube coil's demonstrated performance at that frequency.
Q0 = omega*L/Rs; their numbers (9.42e7 rad/s = 15 MHz, 1.1 uH, 0.107 ohm) evaluate to ~970 - consistent with the measured 920Source quote & editorial note
From Fig.12 we determine Qmeasured at a distance of 11mm to be 460. This implies a Qo of 920.
Editorial note, tabletop extrapolation: A benchmark to scale, not a floor: for the reference machine's ~9 MHz tank, skin-effect scaling of the same coil suggests Q0 ~ sqrt(9/15)*920 ~ 700-class; a measured Q0 far below the scaled expectation is the excess-loss flag (bad joints, steel in the return path) worth hunting.
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On the tested 12-inch resonator, every loop distance and tap setting that presented (50+j0) ohms at resonance empirically gave the same peak dee voltage for a given forward power - matched couplings were equivalent, so the builder optimized for mechanical convenience.
Source quote & editorial note
Empirically it was found for a given forward power into each of the (50+j0) Ohm points, the peak capacitor voltage was always the same.
Editorial note, tabletop extrapolation: Good news for coupler design: don't agonize over loop position vs tap point - but on a new tank, after nulling reflected power, verify dee voltage and coupler temperature once per geometry before treating settings as equivalent; a nominal match can hide coupler or cable loss.
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For a given RF power the only knobs that raise dee voltage are minimizing Rs or increasing tank inductance L while decreasing dee capacitance C to hold the resonant frequency.
Vp-p = 2*sqrt(2*P*L/(Rs*C)) => maximize L/C ratio, minimize Rs at fixed f0 = 1/(2*pi*sqrt(LC))Source quote & editorial note
minimizing Rs, or increasing L2 while simultaneously decreasing C2 (to maintain the resonant frequency) are the only parameters that can be adjusted to increase the DEE voltage for a given amount of RF power.
Editorial note, tabletop extrapolation: For a next machine, shrinking dee-to-liner capacitance (larger dee-to-lid spacing) and a bigger low-loss coil raise dee voltage before amplifier watts do - bought, not free: more L usually brings more conductor and more Rs, and dee-to-lid spacing spends the magnet-gap budget (dg-163). Optimize the L/C-versus-Rs package together, then buy watts.
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On the cited 12-inch machine's resonator (L = 1.1 uH, C = 78.1 pF, estimated AC resistance 50 mOhm), ~1000 W forward power produced ~15 kV p-p dee voltage; the chamber withstood 2000 W but the tank, housing, chamber and dee stem became very warm.
1000 W -> ~15 kVp-p measured; 2000 W withstood with significant heatingSource quote & editorial note
inductance of 1.1uHy, capacitance of 78.1pF, and the estimated AC resistance of 50mOhm ... Preliminary tests with the new generator show that the cyclotron chamber is capable of withstanding 2000 watts of input power. The tank, tank housing, cyclotron chamber and DEE stem become very warm. It is not necessary to operate at 2000 watts, as shown above 1000 watts produces a peak-to-peak DEE voltage of approximately 15kV.
Editorial note, tabletop extrapolation: Scales the reference machine's plan only under ideal sqrt-power scaling at unchanged loaded shunt impedance: 500 W -> ~10.6 kVp-p, comfortably in the 5-13 kV target - but measure the actual dee voltage with a calibrated pickup; thermal management of stem and coil becomes the real issue.
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The source replaced reliance on a thick collector shield with a large series inductance (an RF choke) in the collector lead to keep dee RF from coupling into the beam-current electrometer.
Source quote & editorial note
the original purpose of the shield was to prevent RF from coupling to the pickup ... We agreed a large series inductance (an RF Choke) should mitigate this concern.
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 1
Editorial note, tabletop extrapolation: For nA-level collection near a ~9 MHz dee, treat the choke as one element of a verified filter: choose it from measured impedance and self-resonant-frequency data at the RF frequency, keep whatever shielding the noise floor turns out to demand, and validate by running RF with no beam - displacement currents into an unshielded tip can dwarf the beam signal.
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If using an ion-source chimney, verify the first half-turn clears the chimney body: with a 0.5-in dee gap and Rs = 0.8 ohm, calculated first ions clear at ~200 W RF (50 W is far too low, 500 W comfortable).
First-turn radius from x,y solutions with E = Vpeak/gap; thresholds: 50 W too low, ~200 W first ions clear, 500 W sufficientSource quote & editorial note
an input RF power level of 50 watts is too low, and 500 watts should be sufficient. The first ions are expected to clear the chimney at approximately 200 watts.
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 5
Editorial note, tabletop extrapolation: A geometry trap for a next machine: any chimney or source structure must be smaller than the first half-turn diameter set by the dee voltage, or beam dies before the first gap crossing.
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Set RF frequency from the cyclotron resonance relation: for protons f(MHz) = 1.52 x B(kilogauss); tune B (not f) during operation to find resonance.
f = eB/(2*pi*m); protons f(Mc) = 1.52*B(kG); deuterons and alphas (4He2+) f = 0.76*B(kG)Source quote & editorial note
Protons: f (megacycles) = 1.52B (kilogauss) ... The actual technique used to control resonance in a cyclotron is to vary the magnetic field, with the applied frequency held constant.
Livingston & Blewett, Particle Accelerators (1962) — p. 156
Editorial note, tabletop extrapolation: The reference machine's 0.59 T (5.9 kG) gives 8.97 MHz, confirming their ~9 MHz choice; for a next machine pick B first, then f = 1.52*B.
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If beam peaks with the source displaced off-center, suspect unequal accelerating voltage along the dee faces (transmission-line droop, measured up to 5 percent) driving orbit-center precession; displacements over 2 in have been needed on large machines.
D-face voltage droop up to 5%; compensate by radial source offsetSource quote & editorial note
there will be a somewhat lower potential at the ends of the D faces nearest the lines ... measured in some cyclotrons to be as great as 5 per cent ... a displacement of the ion source of over 2 in. has been necessary.
Livingston & Blewett, Particle Accelerators (1962) — p. 164
Editorial note, tabletop extrapolation: Make the source mount adjustable in both directions and tune position for beam, not for geometric center. Size the travel from RF-field and orbit modelling for the actual dee geometry - the large machines needed over 2 inches; what a tabletop machine needs is its own calculation, and generous commissioning range is cheap.
Cited in: Beam Dynamics: An Interactive Laboratory
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Electric gap focusing helps only in the first few turns and only for ions crossing while the RF field is DECREASING; separately, the practical phase migration for an accelerated ion runs from zero to -pi/2 and back - one half-cycle of total excursion, the quote's limit.
phase focusing quadrant: field decreasing during transit; total phase excursion ~pi radians; internal targets tolerate up to ~3*pi/2Source quote & editorial note
the practical maximum migration in phase will be from zero to -pi/2 and back to zero, a total phase migration of pi radians or one half-cycle.
Livingston & Blewett, Particle Accelerators (1962) — p. 166-171
Editorial note, tabletop extrapolation: With a 3-4% field droop and 160 turns-scale acceleration, the reference machine's dee voltage sets how much phase slip they can afford: higher V = fewer turns = more field-shape tolerance.
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Raising dee voltage is the standard lever for marginal resonance - fewer turns, more phase-slip budget - but it trades against spark breakdown and RF power, and it cannot fix a frequency mismatch or an unsuitable field profile; most machines end up accepting a slightly smaller exit radius and energy to keep intensity.
N_turns ~ T_final/(2*e*V_dee); minimum V_dee vs energy and field droop delta per Cohen (Fig. 6-25)Source quote & editorial note
Increasing the D voltage requires fewer turns for acceleration to maximum energy and will compensate for a larger phase shift. However, D voltage is usually limited by ... power and spark breakdown.
Livingston & Blewett, Particle Accelerators (1962) — p. 172
Editorial note, tabletop extrapolation: At ~1.3 kV and ~150 keV the reference machine's ions make ~60 turns; doubling dee voltage halves turns and dramatically relaxes both field-uniformity and vacuum (scattering) requirements.
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Choose dee-to-lid clearance for the working dee voltage: MIT's 1.25-in clearance (5-in lid gap) capped dee voltage at ~70 kV by breakdown, and the source's remedies are greater clearance plus round, smooth contours and clean, polished surfaces.
MIT: 5-in gap between lids, 2.5-in dee height, 1.25-in clearance -> ~70 kV limit (~56 kV/in working gradient)Source quote & editorial note
The gap between chamber lids was chosen to be 5 in., leaving 1 1/4-in. clearance between D's and lids ... resulting in a D-voltage limit of about 70 kv due to breakdown. ... The limit can be raised by designing for greater clearance between D's and chamber lids and by providing round, smooth contours and clean, polished surfaces.
Livingston & Blewett, Particle Accelerators (1962) — p. 175, 189
Editorial note, tabletop extrapolation: At 1.3 kV the reference machine has large margin against this failure mode. For a next machine at several kV, treat MIT's ~56 kV/in at breakdown as one calibration point, not an allowable: analyze peak surface fields, round and polish, assemble clean, and expect to condition (see dg-253) - no universal safe kV/in exists for vacuum gaps.
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Water-cool powered dees: cooling tubes spaced as closely as 2-3 in prevented local heating and warping of MIT-class dees under power; some cyclotrons also shape the dee profile to follow the shrinking beam envelope, wide in the center and tapering toward the outer edge.
cooling-tube pitch 2-3 in on MIT-class powered deesSource quote & editorial note
it has been found necessary to have these tubes spaced as closely as 2 to 3 in. to prevent local heating and warping of the D's under power. ... In some cyclotrons the D's have been shaped to conform roughly to such a beam envelope, having wide inner vertical aperture in the central region and tapering to a narrower width at the outer edge.
Livingston & Blewett, Particle Accelerators (1962) — p. 175
Editorial note, tabletop extrapolation: At tens of RF watts the builder likely needs no water, but check rather than assume: what matters is local RF current density and the thermal path, not total power. Dee thermal drift detunes the resonator - keep dee structures stiff and thermally anchored, and watch tuning drift as power rises.
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Match the exposed ionization-column length to the dee aperture: MIT's optimum was 5/8 in for a 1.6-in aperture, the Carnegie 60-inch's 1-3/8 in for 4-in dees (ratios ~0.39 and ~0.34) - an over-long column loads the RF circuit with off-focus ions and drags down dee voltage.
two historical optima at ~0.34-0.39 x internal dee aperture - observed ratios, not a lawSource quote & editorial note
At MIT, with an internal D aperture of 1.6 in. the optimum length of ionization column was 5/8 in. For 4-in.-wide D's in the Carnegie Institution 60-in. machine it was 1 3/8-in.
Livingston & Blewett, Particle Accelerators (1962) — p. 178
Editorial note, tabletop extrapolation: Hood or collimate the reference machine's source with the exposed column ADJUSTABLE, starting near a third of the aperture height, and optimize against extracted beam and dee voltage together - the historical ratios locate the starting point; the machine's own optimum may sit elsewhere.
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Livingston & Blewett's oscillator practice: feed the dees through quarter-wave resonant lines (dee on the inner-conductor end), drive push-pull, and watch the push-push mode - with the quoted only-general-rule on parasitics: the simpler the structure and the shorter the leads, the fewer the parasitics.
f_pushpull = 1/(2*pi*sqrt(L(C+2C'))); push-push mode has higher Q and no dee-to-dee voltageSource quote & editorial note
The only general rule is: The simpler the physical structure and the shorter the leads and connections, the less subject is the oscillator to parasitics.
Livingston & Blewett, Particle Accelerators (1962) — p. 185-187
Editorial note, tabletop extrapolation: If a next machine goes two-dee push-pull, watch for the push-push mode (no dee-to-dee voltage, oscillator happily locked); a single-dee-plus-dummy design sidesteps that mode entirely - one reason small machines favor it.
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Anticipate the blue-glow multipactor discharge: it clamps dee voltage to a few hundred volts, heats surfaces and liberates gas, and only fast pumping plus continued outgassing (and an oscillator that can drive through it) breaks the cycle.
Source quote & editorial note
This loading of the D circuit by discharge currents holds the D potentials down to a few hundred volts ... Unless the loading is removed, the chamber will continue to operate in the low-voltage, blue-glow discharge condition indefinitely.
Livingston & Blewett, Particle Accelerators (1962) — p. 188
Editorial note, tabletop extrapolation: The reference machine's dee operates in the range where these discharge phenomena live: the ~100 V-class multipactor band is crossed at every start, and blue-glow gas discharge appears when pressure and surfaces allow. Surface conditioning, low pressure, and drive that can snap up fast are the standard escapes - and whether a given stall is multipactor or gas discharge is diagnosed, not assumed (dg-1273).
Cited in: The Vacuum Budget of a Cyclotron
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Fit one or more trimmer capacitors adjustable by remote control under full power - a movable plate on the chamber side wall facing a dee edge, with excellent RF contact to the wall and ~1 percent frequency range - to trim the relative resonant frequencies of the two dee circuits and adjust relative dee voltage.
tuning range ~1% in frequencySource quote & editorial note
A technique frequently used to adjust or trim the relative resonant frequencies of the two D-line circuits is to use one or more trimmer capacitors which can be adjusted by remote control under full power operation. Such a variable capacitance can be provided by a movable plate on the side wall of the chamber facing one edge of the D. It must have excellent electrical contact to the walls for the radiofrequency currents and a range of motion sufficient to tune over about 1 per cent in frequency. The availability of such a tuning device makes it possible to adjust relative D voltage as desired for optimum operation.
Livingston & Blewett, Particle Accelerators (1962) — p. 188
Editorial note, tabletop extrapolation: A bellows-actuated plate near the dee gives the builder live resonance trim without opening the chamber - invaluable when thermal drift walks the dee frequency.
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Expect high-voltage conditioning of a freshly opened chamber: assemble clean (no dust, grease, or fingerprints; never steel wool or coarse abrasives), round and polish the high-field contours - and still expect conditioning, which no amount of smoothing or polishing eliminates; the oscillator must be able to ride through the sparking without manual resets.
Source quote & editorial note
It is common experience, however, that no amount of smoothing or polishing will eliminate the necessity of some high-voltage conditioning under vacuum. Clean laboratory techniques in preparing a chamber for reassembly after opening are essential; dust should be controlled and all grease removed (even fingerprints), and under no circumstances should steel wool or coarse abrasives be used in cleaning. The oscillator circuit must be capable of driving the cyclotron through these varied conditions of sparking and discharge, without the necessity of tuning or of manual resetting of overload relays.
Livingston & Blewett, Particle Accelerators (1962) — p. 189
Editorial note, tabletop extrapolation: After every chamber opening, ramp dee voltage gradually with vacuum and arc-rate monitoring until sparking subsides before expecting stable beam; how long that takes is the machine's answer, not a fixed budget.
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Prefer a self-excited oscillator closely coupled to the high-Q dee circuit, so frequency follows dee warping and loading automatically; the grounded-anode push-pull variant with crossed neutralizing capacitors is, in the book's account, simple, compact, and free of delicate tuning requirements - the quoted advantages.
Illinois 42-in: two '880' tubes, ~60 kW total input; grounded-anode, cross-neutralized, low-Q grid coilSource quote & editorial note
The most significant advantage of this circuit is its simplicity and compactness along with the freedom from delicate tuning requirements or precise construction.
Livingston & Blewett, Particle Accelerators (1962) — p. 190-193
Editorial note, tabletop extrapolation: The same logic favors a drive that follows the dee on the reference machine: self-excited, or a PLL tracking the resonator - similar in spirit though not identical in dynamics, since a PLL adds its own loop behavior. Either way, mechanical drift retunes the drive instead of killing the beam.
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Historical cyclotron flange-seal practice: gasket in a machined groove, ~50 percent thicker than the groove depth (about 33 percent compression), 1/4-in section adequate for even the largest seals; neoprene preferred because most rubbers have unacceptable vapor pressures and deteriorate with greases; lay a thin copper-foil strip half-over the gasket where RF current must cross the joint.
gasket thickness ~ 1.5x groove depth; 1/4-in section adequate for largest flangesSource quote & editorial note
about 50 per cent thicker than the depth of the groove to allow for compression ... 1/4-in. gaskets have proved adequate for even the largest seals ... Conductivity for rf currents through such a seal can be assured by half-covering the gasket with a thin copper-foil strip. ... Most natural or artificial rubbers have unacceptable vapor pressures and also deteriorate when used with lubricating greases. Neoprene is free of these faults and is widely used in cyclotrons.
Livingston & Blewett, Particle Accelerators (1962) — p. 199-201
Editorial note, tabletop extrapolation: The copper-foil RF bridge over elastomer joints prevents mysterious Q loss and local heating and transfers directly. For the gasket itself, a modern machine should size grooves from the O-ring manufacturer's vacuum-service squeeze and gland-fill tables - the historical 1.5x ratio is the era's flat-gasket practice, not an O-ring spec.
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Set the RF frequency slightly below the central-field cyclotron frequency but above the edge-field value - the quoted window for a declining field; the phase error then migrates one way and back across the acceleration (dg-571's phase-turnaround strategy is the professional form of the same move).
f_edge < f_rf < f_centerSource quote & editorial note
apply a radio frequency oscillating voltage to the electrode that is slightly less than the cyclotron frequency given at the center of the field, but greater than [that] near the edges.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 20
Editorial note, tabletop extrapolation: A concrete tuning rule for the builder: do not tune RF to the central field alone - place it inside the quoted window and find the best point empirically by beam current; the phase-history reasoning is the theory behind the knob, not a substitute for turning it.
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If RF is tuned exactly to the central frequency of a radially decreasing field, ions slip toward 90 degrees of phase quickly - on the order of a dozen turns in the source's estimate for most cyclotrons - after which they stop gaining energy; exact-center tuning therefore demands very high dee voltage.
source's estimate: ~12 turns to 90 deg slip with f_rf = f_center - context-dependent (field profile, harmonic, energy gain per turn all enter)Source quote & editorial note
It would only take a few cycles, on the order of 12, for most cyclotrons to have reached this velocity.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 20
Editorial note, tabletop extrapolation: Explains failed runs where beam dies at small radius, and quantifies how little phase budget a mistuned machine has - for the actual machine, integrate the slip turn by turn from the measured B(r) and dee voltage rather than using 12 turns as a threshold.
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Use one driven dee against the grounded chamber wall (dummy dee) instead of two dees: it halves the RF feedthrough count and the whole chamber becomes the return electrode - the standard simplification for small machines.
Source quote & editorial note
it has one dee-shaped copper electrode, and the grounded vacuum chamber functions as the other electrode
Editorial note, tabletop extrapolation: The reference machine already does this, and it stays attractive for a next machine - one HV feedthrough fewer, the chamber as return electrode - unless push-pull two-dee RF is wanted for higher energy gain per turn. A common choice among documented small machines, not a rule.
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Iowa State's dee geometry: thin sheet-copper dees 22.5 cm in diameter and 2.4 cm high, separated by a 1.5 cm gap and water-cooled through the supporting stems - about 0.89 of their pole diameter.
dee dia 22.5 cm vs 25.4 cm pole face (0.886); dee height 2.4 cm; dee-dee gap 1.5 cmSource quote & editorial note
The dees, made of thin sheet copper, arc 22.5 cm in diameter, 2.4 cm high, and they are separated by a gap of 1.5 cm.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 7
Editorial note, tabletop extrapolation: A documented dee geometry near the reference machine's scale - note it exceeds an 8-inch pole, so it fits 10-inch-class machines as-is: scale the proportions, not the dimensions. Dee cooling need tracks the dissipated RF power and construction, not a fixed kilowatt line: compute it from the RF budget (dg-313) and watch dee temperature during commissioning.
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Budget extraction realistically: the Argonne 60-inch extracted about 30% of the internal beam at the exit radius, and the quoted efficiency figure ran 10% at 120 uA of deflected deuterons, rising to 15% at 200 uA.
extraction ~30% of internal beam; beam power / RF DC input ~ 10-15%Source quote & editorial note
This value is about 10% for 120 uamp of deflected deuterons, increasing to 15% for a 200 uamp beam. About 30% of the internal beam at the exit radius is extracted.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 19
Editorial note, tabletop extrapolation: Sets expectations if a next machine attempts a deflector: capturing a third of the circulating beam was a mature machine's result, so plan around numbers of that order - and account for where the rest goes (septum heating, sputtering, and at higher energies activation), rather than booking the loss as free.
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Set the extraction gap by the empirical vacuum-breakdown limit d[mm] >= 1.41e-2 * U[kV]^1.5 (clean flat surfaces): 10 kV needs >=0.45 mm, 30 kV >=2.3 mm, 50 kV >=5 mm; smaller gaps arc, much larger gaps waste extraction field.
d[mm] >= 1.41e-2 * (U[kV])^(3/2)Source quote & editorial note
The voltage breakdown limit determines the necessary gap width. The empirically determined limit (valid for clean, flat surfaces) is d[mm] >= 1.41 x 10^-2 * phi[kV]^(3/2).
Wolf (ed.), Handbook of Ion Sources (1995) — p. 379
Editorial note, tabletop extrapolation: Direct rule for source-to-puller spacing - clean DC gaps are the law's home turf: a few-kV gap needs sub-mm minimum, with real margin because sputtered metal films spoil the 'clean surface' assumption fast. For dee-to-ground RF clearances use it only as a lower-bound sanity check: edges, insulators, RF conditioning and enhancement move the practical limit (dg-353, dg-662).
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Dielectric strength of polymer insulation drops steeply with thickness -- Teflon FEP holds 240 kV/mm at 0.025 mm but only 70 kV/mm at 5 mm -- so rate thick insulators from thick-sample data, never from thin-film numbers.
Teflon FEP: 240 kV/mm @ 0.025 mm; 70 kV/mm @ 5 mm (still ~350 kV across 5 mm in theory; derate heavily in practice)Source quote & editorial note
Dielectric strength / Thickness: 240 kV/mm at 0.025 mm; 70 kV/mm at 5 mm.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 523
Editorial note, tabletop extrapolation: When insulating the reference machine's extraction or dee leads, design from certified data for the actual material, thickness, frequency and environment - a bulk breakdown number is a test-condition figure, not a working rating. Grade the field at edges, design creepage and surface flashover paths separately, and qualify the finished assembly under vacuum with a conservative withstand test.
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For automated matching prefer an L-network over T or Pi: only one L-C combination per load simplifies the tuning algorithm; one L-network cannot match all impedances, so the cited system switches between two complementary L configurations with an RF switch, giving a wider matching range.
2 complementary L-network topologies + RF switch = wider matching range (coverage set by component ranges - verify against the actual load domain)Source quote & editorial note
Compared to T or Pi networks, the L network uses only one combination of inductance and capacitance. This simplifies the microcontroller tuning algorithm. The disadvantage is that one L network cannot match all possible load impedances. Figure 3 shows two L network types with complimentary matching ranges on the Smith Chart. The IMS uses an RF switch to select one of the two L networks, allowing a wider matching range.
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 11
Editorial note, tabletop extrapolation: If the builder automates their dee match at 9 MHz, a stepper-driven L-network is the simplest topology for the search algorithm; verify the two configurations' combined range covers the tank's actual impedance excursions (a Smith-chart sweep or simulation) before committing.
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Sample line power through a directional coupler sized so the detector never exceeds its rating: the source pairs a ~30 dB coupler with an AD8307 log detector for 200 W measurements, but 200 W is 53 dBm and 30 dB of coupling still delivers 23 dBm - above the AD8307's +17 dBm rated maximum - so budget additional attenuation between coupler and detector: at least 36 dB total for 200 W, 40 dB for 500 W, plus margin.
P_detector = P_line - coupling - pad; 200 W = 53 dBm -> 23 dBm after 30 dB; pad so P_detector <= +17 dBm at maximum power with margin for mismatch peaksSource quote & editorial note
The coupling factor is high, ~1000 or 30 dB, to minimize main line power loss ... enables 200 W power measurements using the AD8307 logarithmic detector IC
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 18
Editorial note, tabletop extrapolation: For the reference machine's 100-500 W upgrade: a homebrew 30 dB coupler plus AD8307 board works with a calibrated pad (10 dB or more) between them; include coupler tolerance and mismatch peaks in the level budget, and calibrate the chain end to end.
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Build the HF coupler the Kaune way: ferrite toroids wound with AWG 26 wire surrounding two 2-inch sections of RG-8 coax form the coupling transformers (the core type, directivity figures, and the exact shield/ground arrangement are the thesis's details - scan re-read queued).
FT-82-67 toroids, AWG 26 windings, 2-in RG-8 through-line sections; directivity 35 dB at 3.5 MHz, 28 dB at 30 MHzSource quote & editorial note
Ferrite toroids wound with AWG 26 wire and surrounding two 2 inch sections of RG-8 50 Ohm coaxial cable form the coupling transformers.
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 18-19
Editorial note, tabletop extrapolation: A cheap coupler build bracketing the reference machine's 9 MHz band - built from the source's full schematic, not the one-line summary: the shield treatment and grounding are what make the directivity, so replicate them exactly, then bench-test directivity, insertion loss and core heating at 9 MHz through the intended power and mismatch range before trusting it.
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Coupler directivity bounds SWR measurement: with 28 dB directivity a perfectly matched load can read SWR up to ~1.08, with 35 dB up to ~1.03 - the leakage vector can also CANCEL true reflection, so finite directivity is an uncertainty band, not a fixed floor.
residual reflection magnitude = 10^(-directivity/20): 0.040 at 28 dB, 0.018 at 35 dB -> apparent SWR up to ~1.08 / ~1.04 on an ideal matchSource quote & editorial note
the SWR measured using this directional coupler is 1.08 and 1.03 for 28 dB and 35 dB of directivity, respectively
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 19-20
Editorial note, tabletop extrapolation: Do not chase - or trust - SWR readings within the bridge's directivity band: near-1.0 does not prove a good match any more than 1.08 proves a bad one. Characterize the actual homebrew bridge's directivity first; then readings inside its band are 'unresolved', not data.
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Calibrate homebrew power sensors against a real standard: the thesis's setup compared its sensors with a Bird 43 thruline wattmeter over 30-100 W (its lower-range procedure and lookup-table details are the thesis's - scan re-read queued).
AD8307: 0.025 V/dB slope, ~2.0 V intercept; two-range calibration 0-30 W and 30-100 WSource quote & editorial note
Figure 42 - 30 W to 100 W Power Calibration Setup using Bird 43 Wattmeter
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 57-58
Editorial note, tabletop extrapolation: A Bird 43 (owned or borrowed) transfers power calibration to permanently installed cheap sensors - within the installed element's frequency range, power range and its own accuracy spec, so record which element was used. Take the AD8307's slope and intercept from its datasheet and the actual unit's measured response, not nominal folklore.
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A workable auto-tune algorithm: alternately step the inductor and capacitor toward the SWR minimum, stopping at SWR < 1.5:1 (4% reflected power); the source system matched loads from initial VSWRs up to 26:1 across 3.5-30 MHz.
SWR 1.5:1 <=> |Gamma| = 0.2 <=> 4% reflected; source matching range: up to 26:1 initial VSWR, 3.5-30 MHzSource quote & editorial note
actuates stepper motors to alternately adjust a variable capacitor and a variable inductor to reduce VSWR to less than 1.5:1 ... The antenna tuner system can match loads of up to 26:1 initial VSWR within a frequency range of 3.5 MHz to 30 MHz.
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 6-8, 40
Editorial note, tabletop extrapolation: Coordinate-descent on C then L is not guaranteed to converge on an interacting high-Q load - test it against the dee resonator before trusting it - and set the LDMOS amplifier's reflected-power shutdown from that device's own specification, not from the 1.5:1 convention.
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Cyclotron resonance frequency is f0 = 15.2 * B[T] * Z / A MHz - about 10 MHz per tesla region for protons (15.2 MHz at 1 T).
f0[MHz] = 15.2 * B[T] * Z/ASource quote & editorial note
fo = qBo/2pi mi = (1.52x10^7) Bo(tesla)/A
Humphries, Principles of Charged Particle Acceleration (1986) — p. 524
Editorial note, tabletop extrapolation: One-line check of the reference machine's operating point: 0.59 T -> ~9.0 MHz for protons; sets the next machine's RF band for any target field.
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Relativistic phase slip caps a fixed-frequency cyclotron at Tmax = sqrt(16*q*V0*mi*c^2/pi) with optimal detuned injection - so the maximum energy grows only as the square root of dee voltage (100 kV -> ~31 MeV for deuterons; the practical cure is more volts per turn).
Tmax = sqrt(16*q*V0*mi*c^2/pi); f_rf/f_g0 = 1/(1+Tmax/2mi c^2)Source quote & editorial note
the final kinetic energy is maximized by taking Vo large... a high gap voltage accelerates particles in fewer revolutions so that there is less opportunity... to get out of synchronization.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 530-531
Editorial note, tabletop extrapolation: At sub-MeV this limit is distant - by this formula a 10 kV dee puts the proton ceiling near 7 MeV - but the same physics governs field-flatness tolerance: fewer turns forgives more field error.
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Low-energy protons orbit at 15.23 MHz per tesla (f = qB/2*pi*m); scale RF frequency linearly with the orbit-averaged field for a classical proton cyclotron on the fundamental harmonic.
f(MHz) = 15.23 * B(T) for protonsSource quote & editorial note
Low energy proton in 1 T field: 15.23 MHz
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 29
Editorial note, tabletop extrapolation: The single most-used number in the reference machine's notebook: 0.59 T -> 9.0 MHz; a 1.2 T higher-field successor -> 18.3 MHz, still comfortable amateur-radio-technique territory.
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Estimate turn number as N = T_final/(n_gaps*V0*sin(phi)) and turn spacing as dr/dN ~ r*(T1/T); low energy gain per turn means thousands of turns and micron-scale outer-orbit separation, which is what makes extraction hard.
N = T/(n*V0*sin(phi)); dr/dN ~ r*dT_turn/(2T) nonrelativistically (exactly r*(T+mc^2)/(T*(T+2mc^2))*dT_turn); source's example: 250 MeV at 17 keV/turn -> N ~ 15,000, spacing ~ 20 umSource quote & editorial note
250 MeV protons; 17 KeV/turn: N~15,000... 250 MeV protons r=0.3m: dr/dN ~ 20 microns!
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 43
Editorial note, tabletop extrapolation: For the builder: 1 MeV at 2 kV per gap (2 gaps) is ~250 turns with final-orbit spacing ~0.25 mm at r = 12 cm - which is why higher dee voltage directly eases both extraction and vacuum requirements.
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The classical fixed-frequency cyclotron is limited to under ~25 MeV protons because phase slip accumulates at ~360*(gamma-1) degrees per turn; at 21 MeV that is ~8 deg/turn, losing a peak-phase ion in 11 revolutions unless energy gain per turn is enormous (360 kV for the LBL 60-inch).
dphi/dn = 360*(gamma-1) deg/turn; classical limit E < ~25 MeVSource quote & editorial note
dphi/dn=360 [gamma-1] -> 8 deg. An ion on peak phase is lost in 11 revolutions. Only solution- very high energy gain per turn - 360kV
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 51
Editorial note, tabletop extrapolation: At 1 MeV the instantaneous slip is only ~0.4 deg/turn, but slip accumulates over every turn, so what that buys depends on volts per turn: a machine gaining a few kV per turn spends thousands of turns getting to 1 MeV and can run out of phase well below the textbook ceiling. The design check is the summed slip across all turns against the +/-90 deg window, not the per-turn number.
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A single real dee working against its image in a grounded plate is a working small-machine RF architecture - the quoted machine's arrangement, tuned by physically twisting the inductor onto the cyclotron frequency; its commercial-amp drive chain is the same paper's setup (dg-118; chain details: scan re-read queued).
f = 1/(2*pi*sqrt(LC)), C fixed by dee geometry, L adjusted (deformable coil) to tuneSource quote & editorial note
The second DEE has been faked using the image of the real DEE on a grounded conductor ... By twisting the inductor, we can change the inductance to match our inductance requirements.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 11
Editorial note, tabletop extrapolation: This is the reference machine's exact topology, in use on a comparable documented machine; the deformable-inductor trim is a simple tuning mechanism worth copying on a next machine.
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High Q demands precise, stable tuning - the cited machine measured Q = 1600 unloaded, and the source stresses that high-Q circuits need high mechanical precision.
Q = f0/delta_f = 2*pi*E_stored/E_lost per cycle; at 9 MHz a Q of 1600 would mean ~5.6 kHz bandwidth (worked example, not the reference machine's measured value)Source quote & editorial note
high precision is necessary for a coil or circuit with a high Q value ... The Q of this cyclotron was measured at 1600, under no loading.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 11-12
Editorial note, tabletop extrapolation: A benchmark, not an expectation: measure the reference machine's own unloaded AND loaded Q, compare against a loss model to decide whether joints are costing Q, and judge retuning needs from measured thermal drift against the loaded bandwidth - Q alone predicts neither the drift rate nor the need for active tuning.
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Know which breakdown regime you're in: for the source's typical cases, 'vacuum' breakdown (field emission, particulates) lives below ~1e-5 torr and 'gas' breakdown (Paschen) above ~1e-4 torr - contextual rules of thumb, not sharp boundaries; gas species, pd, electrode geometry and condition, and RF frequency all move them.
source's typical cases: vacuum regime < ~1e-5 torr; gas regime > ~1e-4 torr; the decade between is mixedSource quote & editorial note
For typical cases of interest, 'vacuum' pressure is lower than 10-5 torr, and 'gas' pressure higher than 10-4 torr.
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 23
Editorial note, tabletop extrapolation: A gas-fed cyclotron chamber often sits in exactly this transition decade, so the spark limit can move with operating pressure: measure holdoff with the actual gas flowing at operating pressure as well as at base vacuum, and interlock conservatively - which direction the limit moves depends on where the geometry sits relative to the Paschen minimum.
Cited in: The Vacuum Budget of a Cyclotron
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Condition ('bake out') the tank with RF applied gradually - increasing the power and the length of application, never leaving RF on for prolonged periods through a discharge, which risks cracking the glass dee insulators; the report's completion point is vacuum holding below ~1e-4 mm with ~2 kV of steady RF.
condition until P < 1e-4 torr with RF steady at ~2 kVSource quote & editorial note
r.f. power should never be left on for prolonged periods under these circumstances, else the risk is run of cracking the glass dee insulators. The power and length of application should be gradually increased
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 10
Editorial note, tabletop extrapolation: Directly applicable startup ritual at the reference machine's 1.3 kV dee level - ramp in short bursts with current-limited RF, arc detection and pressure monitoring. The report reads failure to reach its endpoint as organic contamination (grease, oil, rubber) in the tank; leaks and ordinary outgassing can mimic it, so inspect or run an RGA before blaming contamination.
Cited in: The Vacuum Budget of a Cyclotron
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Use single-dee construction (the grounded tank is the other 'dee') to simplify tank and oscillator; add a symmetric grounded dummy-dee edge for better ion focusing only after the machine works.
Source quote & editorial note
the 'single-dee' construction; this has many advantages ... Better ion focussing can be obtained by installing a 'dummy' grounded dee edge symmetric to the insulated dee, but this is a refinement
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 8
Editorial note, tabletop extrapolation: Exactly the reference machine's architecture. The dummy-dee edge is the source's named refinement for better ion focusing - a natural next-machine upgrade once the basic machine works, which is the sequencing the source itself implies ('but this is a refinement').
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Wouters recommends a grounded-grid self-excited oscillator arrangement for confining RF currents to intended paths, and - the quoted requirement - the dee-to-ground capacitance must be counted as the major portion of the tank-circuit capacitance (his circuit trims frequency with a small parallel capacitor; circuit details: scan re-read queued).
C_tank ~ C_dee-ground + C_trim; step-up by tapping plate down the coilSource quote & editorial note
The dee-to-ground capacity appears as the major portion of the capacitance in the tank circuit, which must be calculated taking this into account
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 8
Editorial note, tabletop extrapolation: Even with a modern solid-state chain, the builder must treat dee capacitance as the resonator's dominant C when designing the matching network; the confine-the-RF-current lesson is timeless.
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Provide short, broad RF ground paths, especially in the ground circuits, and keep the tube close to the tank but out of the magnetic field (the quoted requirements); Wouters' specific construction - the tube through a large hole in a copper ground sheet extended to the tank wall - is his implementation (scan re-read queued).
Source quote & editorial note
it is important to provide short, broad paths for current flow, especially in the ground circuits ... While the tube should be placed as close to the tank as possible, it must yet be kept away from the magnetic field
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 8-9
Editorial note, tabletop extrapolation: Directly applicable to the reference machine's amplifier: wide copper sheet or strap grounds and a short feed run, with magnetically SENSITIVE parts kept out of the fringe field - the tube in the quote; in modern gear whatever actually cares (fans, ferrites, meters - dg-670's shield-or-relocate).
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Choke and bypass every circuit that connects to a tank element so RF cannot reach the meters and supply lines - the quoted requirement; Wouters' operating recommendations on control accessibility sit elsewhere in the paper (scan re-read queued).
Source quote & editorial note
All circuits connected to tank elements should have adequate choking and bypassing to prevent r.f. from reaching the meters and supply lines.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 9
Editorial note, tabletop extrapolation: Directly applicable: the reference machine's beam-current, bias and gauge lines all deserve feedthrough RC/choke filtering at 9 MHz - with 'adequate' proven by measurement: an RF sniff at the meter terminals with the transmitter running.
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Treat the cyclotron's hazardous supply voltages as deadly - 'proper precautions must be taken, even during preliminary testing': interlock switches on power-supply covers and grounding hooks by the machine (the quoted measures); Wouters' screened oscillator enclosure belongs to his RF section (scan re-read queued).
Source quote & editorial note
The voltages employed on the various cyclotron components are deadly; proper precautions must be taken, even during preliminary testing ... Interlock switches on the power supply covers and grounding hooks
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 9
Editorial note, tabletop extrapolation: Directly applicable home-lab safety baseline for the HV systems of a next machine - covers interlocked, hooks in reach, and the full discharge discipline around them (dg-522).
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Thin chamber lids over a wide flat span bow inward under vacuum, changing dee capacitance (detuning the RF) and reducing flashover voltage - the source machine tack-welded internal support posts under its lids to stop it.
the source machine's case: 3/16-in lids over a ~2 ft span bowed enough to need postsSource quote & editorial note
the top and bottom of the chamber to bow in, which affected the capacitance of the dee and reduced the maximum voltage that the dee could withstand before flashing over.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2
Editorial note, tabletop extrapolation: Directly relevant to any thin-lid chamber on a next machine squeezed into a small magnet gap: design the lids to a calculated stiffness (the lid-deflection calculator) from the start. Internal posts clear of the beam spiral and the RF high-field region are one remedy; thicker or dished lids and external ribs are others, and each needs its own deflection, buckling, venting and weld checks. [Note revised 2026-08-23: earlier note planned posts as the remedy.]
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A single dee plus grounded dummy dee doubles the required dee-to-ground voltage compared to two dees, but reduces RF feedthrough cost and complexity (two become one) - often the right trade at amateur scale. [Corrected 2026-08-23: 'the right trade' was stated without the 'often'.]
1 dee: V_required x2, feedthroughs /2Source quote & editorial note
Having only one dee rather than two doubles the voltage requirement, but reduces the cost and complexity of having two RF feedthroughs in the vacuum chamber.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2
Editorial note, tabletop extrapolation: Supports the single-dee choice for a next machine unless attainable dee voltage, insulation or the coupling scheme becomes the binding constraint.
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HV coax cable is an arc-energy reservoir - Mammoflex M-1 stores 56 pF/ft, so 20 ft holds ~0.4 J at 30 kV; persistent arcing was finally fixed only by removing excess cable and shortening the run to ~5 ft (~0.1 J).
E = 0.5*C*V^2; source: 56 pF/ft, ~20 ft, ~0.4 J at 30 kV (0.50 J by the formula at exactly 20 ft); shortened run ~5 ft ~ 0.1 JSource quote & editorial note
Mammoflex M-1 HV cable has C of 56 pF per foot ... ~20 feet total ~0.4 Joules at 30 kV ... Removed excess cable. Run is now ~ 5 feet total
Editorial note, tabletop extrapolation: For any HV feed on a next machine (deflector, source bias): keep cable runs short. Stored cable energy is delivered into an arc in the first instant, faster than any supply limiter acts - it adds to what the supply and other capacitances feed the fault, it does not replace them. Series resistance at the load (dg-286) limits the follow-on current.
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Protect HV circuits in stages: a large series resistor near the supply (150 Mohm) plus a second resistor at the chamber (5 Mohm), coax shields grounded through 68-ohm 2 W resistors, and the resistor/feedthrough housed in acrylic tubes covered with grounded copper mesh.
150 Mohm supply-side + 5 Mohm chamber-side series resistors; 68 ohm shield-ground resistorsSource quote & editorial note
We've encased the resistor in a grounded shield, and the coax shields go through 68 Ohm, 2 watt resistors ... 150 Meg HV resistor ... HV Vacuum Feed Through is now inside an acrylic tube covered with copper mesh.
Editorial note, tabletop extrapolation: A staged-resistance pattern for electrostatic HV feeds (deflector, PIG source bias) whose load draws no standing current: series megohms limit arc current at the price of regulation under load, so it does not transfer to circuits that must deliver current. Even with this shielding the arcs stopped only after the cable-energy fix (dg-285) - resistors limit damage, they don't prevent flashover.
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A tabletop cyclotron RF chain can be assembled from commercial units - the Houghton chain: function generator (HP 33120A) -> RF power amp (ENI 155LCRH) -> ham autotuner (LDG AT-200PC) -> Bird 43A wattmeter -> dee - with fr = 1/(2*pi*sqrt(L*C)) as the first-cut resonance estimate for the tuned circuit.
fr = 1/(2*pi*sqrt(L2*C))Source quote & editorial note
HP 33120A Function Generator - ENI 155LCRH Power Amp - LDG AT-200PC Tuner - Bird 43A RF Power Meter - Dee
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 12-14
Editorial note, tabletop extrapolation: Essentially the reference machine's current architecture. A ham antenna tuner can match a dee-shaped load in this frequency range - but its voltage ceiling is construction- and tuning-dependent: expect the ~kV class rather than the 5-13 kV a dedicated resonator supports (the LDMOS upgrade path), and MEASURE the dee voltage (dg-quoted methods in the dee-coupling deep dive) instead of inferring it from the tuner's rating.
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Through an autotuner chain, tens of watts yields low-kV dee voltage: Houghton reported 1700 Vpp from 26 W and 800 V from 10 W at ~3.5 MHz. [Corrected 2026-08-23: earlier text called the two points 'roughly consistent with sqrt(P) scaling'; they are not (ratio 2.1 vs 1.6 expected), and the 800 V figure's convention (peak, peak-to-peak, RMS) is not preserved in the source.]
26 W -> 1700 Vpp; 10 W -> 800 V (convention unstated). sqrt(P) scaling holds only at unchanged coupling and loaded Q; these points differ from it by ~30%Source quote & editorial note
3.55 MHz 1700 Vpp (26 W) ... 3.48 MHz 800 V (10 W)
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 17-19
Editorial note, tabletop extrapolation: A benchmark for the order of magnitude the reference machine's autotuner path reaches (its ~1.3 kV from a 5 W amplifier is in the same band), not a curve to read values off: state the voltage convention, tuning and loading before comparing, and do not infer a plateau from two points.
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Low dee voltage caps the usable field and energy through orbit count: at 800 Vpp, no beam peaks appeared for fields above ~0.5 T, where reaching full radius takes more than the ~44 orbits that worked - consistent with turn-count-limited survival at their pressures (the quote reports the disappearance; the survival reading is the team's interpretation).
N_orbits = T_final/(e*Vpp); 35 keV / 800 eV ~ 44 orbits was the practical survival limitSource quote & editorial note
No peaks for magnetic fields larger than H2+ at 0.5 T -> 35 keV; 44 orbits at 800 Vpp
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 21
Editorial note, tabletop extrapolation: Quantifies why the reference machine's dee-voltage upgrade matters: at 1.3 kV their protons need ~hundreds of turns to reach interesting energies, and ~44 turns was already the survival ceiling at Houghton's pressures.
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Use a resonant tank because Q = wL/Rac multiplies stored voltage for modest power, and the highest dee voltage for a given forward power occurs at critical coupling, where Qloaded = Q0/2.
Q = omega*U_stored/P_loss (the slide's Q = wL/R_AC is the series-equivalent form); highest dee voltage for given forward power at critical coupling: Q_loaded = Q0/2 (the quoted condition)Source quote & editorial note
To develop high voltages with modest RF power. The highest voltage for given power occurs when: Qloaded = 1/2 Qo
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 18
Editorial note, tabletop extrapolation: The one-slide justification for the builder to move from an antenna-tuner match to a true high-Q tank circuit in a next machine.
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Rutgers' record operating point: 2 kW forward power produced 8.4 kV peak dee voltage on the 12-inch machine (measured via calibrated pickup and Bird thruline wattmeter).
2 kW -> 8.4 kV peak (~16.8 kVp-p)Source quote & editorial note
Record Input Power 2kW: 8.4 kVpeak
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 19
Editorial note, tabletop extrapolation: Anchors the power budget with one measured point: 2 kW bought 8.4 kV peak on that 12-inch tank. Scaling to the reference machine's planned LDMOS runs through ITS shunt impedance (dg-313's formula with measured Q and C): at comparable impedance, 500 W supports roughly 1/2 the voltage (P ~ V^2), a ~4 kV class - measure, then budget.
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Validate the dee-voltage calibration with beam: Houghton's calculation put first ions squeaking past the source structure at 165 W, and beam current dropped abruptly to zero at 170 W as RF power was ramped down - a 3% agreement between geometry-based prediction and observed cutoff on that machine.
predicted threshold 165 W vs measured beam cutoff 170 W at 14.864 MHzSource quote & editorial note
Calculation showing first ions squeak by at 165 Watts ... Beam current abruptly dropped to zero at 170 watts !
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 20
Editorial note, tabletop extrapolation: A free end-to-end CONSISTENCY check for the builder: the power at which beam vanishes ties the trajectory model, the dee-voltage estimate and the RF chain together at one point. It is a cross-check, not a probe-independent voltage measurement - source emission, phase, pressure and detector sensitivity all sit inside the observed threshold - so use it alongside a calibrated pickup, not instead of one.
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Thermal drift of the dee, chamber and tank coil during operation shifts the resonant frequency; Houghton automated retuning by phase-comparing the drive RF with the dee pickup to derive a DC error signal.
phase(drive) - phase(pickup) -> DC error -> actuator; prefer driving a motorized trim capacitor (tune the CAVITY to the beam-synchronous frequency) - letting a PLL drag the SOURCE frequency detunes acceleration unless the shift stays inside the beam-phase toleranceSource quote & editorial note
the DEE, chamber, tank coil, etc. heat up and slightly change the resonant frequency ... A DC 'error signal' is derived from comparing the phase of the driving RF to the Phase of the DEE pickup.
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 21
Editorial note, tabletop extrapolation: At 100-500 W expect real warm-up drift and MEASURE it: the measured drift against the loaded bandwidth decides whether hand-touchup, a slow motor loop, or nothing is needed. The cyclotron constraint is the point - the RF must stay synchronous with qB/(2 pi m), so the resonator follows the beam frequency, not the other way round.
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Infer dee voltage from beam physics: for the first half revolution the source sets E(r) = (qB^2/2m)r^2 = (1/2)Vp-p - the eV-units form; in SI, K = q^2B^2r^2/(2m) with K = qVpp/2 at peak phase, so Vpp = qB^2r^2/m - a probe-independent 'beam inferred dee voltage' plotted alongside pickup and rectifier data.
K = q^2 B^2 r^2/(2m); K = q*Vpp/2 at peak phase -> Vpp = q B^2 r^2/m; r is the first half-turn ORBIT radius, related to the measured landing position through the central-region geometrySource quote & editorial note
Beam Inferred DEE Voltage ... In the 1st half revolution E(r) = (qB^2/2m) r^2 = 1/2 Vp-p
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 33
Editorial note, tabletop extrapolation: The builder can cross-check a dee-voltage estimate by measuring where the first half-turn lands - the beam is the most honest voltmeter - provided the landing radius is converted to orbit radius using the actual source-to-probe geometry, and the ion is assumed to cross near peak phase (real phases read low).
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Prebreakdown current in HV vacuum gaps is field emission from microscopic whiskers (runaway as local field approaches ~1e10 V/m, enhancement beta = lambda^2/ln(lambda)); slow 'conditioning' - holding voltage while microampere pulses burn off the sharpest points - raises the measured threshold, so condition new electrodes gradually.
Fowler-Nordheim j ~ E_l^2 exp(-6.43e9*phi^1.5/E_l); E_local ~ 1e10 V/m for runaway; beta = lambda^2/ln(lambda) for whisker aspect lambda; conditioning partially lost after 24 h off or air exposureSource quote & editorial note
A large increase in current occurs only as the local field approaches 10^10 V per meter... After several minutes of current flow at the constant voltage, a remeasurement of the threshold voltage shows that it has increased. This phenomenon is called conditioning.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 111-113
Editorial note, tabletop extrapolation: Bring the reference machine's dee and extraction voltages up gradually on first pump-down, watching for micro-discharge pulses. Conditioning raised the measured threshold in the source's account; the gain is not permanent capital - re-condition after venting rather than assuming the old ceiling still holds.
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At an insulator-cathode junction, terminate the insulator at ~31.5 degrees to the cathode - the measured zero-surface-charge angle, voltage-independent, with positive charging below it and negative above; screening the cathode end or covering it with a semiconducting layer raised breakdown voltage ~2.5x, and roughening the insulator surface near the cathode added ~40% (near the anode: little effect).
junction angle ~ 31.5 deg (zero surface charge, voltage-independent); cathode-end screening/semiconducting layer: x2.5; roughen near cathode: +40%; ensure intimate metal-insulator contact (conductive coating on insulator end)Source quote & editorial note
They found that at a critical angle of 31.5 deg, the surface charge was zero; this angle was independent of the applied voltage. The surface charges were positive at smaller angles, but negative at larger ones. ... Fryszman and colleagues found that by screening the section of the insulation surface near the cathode or covering this section with a semiconducting layer, the breakdown voltage was raised by a factor of approximately 2.5. ... Roughening the surface of the insulator in a region adjacent to the cathode increased the breakdown voltage by about 40 %. Roughening the surface adjacent to the anode had little effect.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 113-114
Editorial note, tabletop extrapolation: For the next machine's source stalk - a DC cathode-junction context like the studies' - cone the insulator toward the negative electrode and consider recessing the triple junction behind a screen. The factors come from separate experiments and are not multiplicative, and a dee-stem RF feedthrough alternates polarity every half cycle: there, treat all of this as qualitative guidance to be tested, not booked margin.
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Vacuum surface flashover is set by the insulator material, not the electrodes: over a 2.2-cm butt-jointed cylinder, stainless+Pyrex held 100 kV while copper+Pyrex held only 44.5 kV and most ceramics 40-50 kV - which works out to roughly 2-4.5 kV/mm of creepage on that fixture, and breakdown stress falls further for longer insulators.
2.2-cm insulator in vacuum: SS/Pyrex 100 kV; Cu/polystyrene 75 kV; Cu/Teflon 50 kV; Cu/steatite 50 kV; ~2-4.5 kV/mm creepage, sublinear with lengthSource quote & editorial note
Gleichauf also found that the breakdown voltage was strongly dependent on the material of the insulator but independent of the material of the electrodes.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 113-114
Editorial note, tabletop extrapolation: The source's fixture works out to 2-4.5 kV/mm of creepage - a first sanity check for an extraction stalk, not a design allowable: flashover depends on triple-junction geometry, finish, contamination and conditioning, and does not scale linearly with length (the source's own longer insulators held less per mm). Size real hardware by test, with margin.
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Never leave a thin gas/void gap in series with a solid dielectric: the field in the void is multiplied by the solid's dielectric constant k (stress ~ V*k/d for a thin gap), so it sparks first -- fill every gap between conductor and insulator with a compatible potting or liquid dielectric.
E_gap = V*k/(d + x*(k-1)) -> V*k/d for thin gap x << d; grading works: graded bushing held 1 MV over 30 cm vs 0.6 MV over 90 cm conventionalSource quote & editorial note
Air spaces exist in solid and liquid dielectrics... the air will have the higher stress, possibly causing sparkover through the air space... The stress in the air gap can thus be k times that in the solid.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 116, 119
Editorial note, tabletop extrapolation: The classic failure of home-built HV feedthroughs: a loose PTFE sleeve over a rod arcs in the annular air film. Fill the gap - potting or liquid dielectric - so no gas layer sits in series with the solid. Evacuating the annulus removes the Paschen path but leaves field-emission breakdown and surface flashover, so vacuum is not a substitute for filling.
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Coaxial HV feedthrough geometry: peak field sits on the inner conductor at E_max = V/(r_i*ln(r_o/r_i)), minimized when r_i/r_o = 1/e ~ 0.37; and keep the radius of curvature at the outer conductor's edge no smaller than the inner conductor's radius so the edge stress stays below the bore stress.
E_max = V/(r_i*ln(r_o/r_i)); optimum r_i/r_o = 1/e; edge radius of outer electrode >= r_i; concentric spheres optimum R_o/R_i = 2Source quote & editorial note
The optimum ratio as r_i/r_o = 1/e. This optimum ratio minimizes the stresses within the coaxial electrode arrangement, independent of the material of the dielectric used. ... In order to keep stress at Z below that at X in Fig. 4.15, the radius of curvature at Z should not be less than the radius of the inner cylinder.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 117, 122-124
Editorial note, tabletop extrapolation: Preliminary ideal-coax sizing for the reference machine's HV stalk: a grounded 25-mm-bore port gives a ~9.2-mm center conductor at the 1/e optimum - then check the complete feedthrough (ends, dielectric interfaces, triple junctions) electrostatically, and never leave a sharp-edged washer or nut on the HV end.
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Sputtered cathode metal deposits on the HV stalk and can in time cause premature breakdown: practiced mitigations are shadow shielding (INEL's nested coaxial aluminum tubes), a conical insulator facing the cathode to block ions passing through the grid (UIUC), and corrugated insulator surfaces to lengthen the surface-leakage path.
design options: shadow shields between plasma and insulator; corrugated/conical insulator profile; expect W/Fe/Al sputter films; clean with diamond file or sandblast (sandblasting can ruin polished grids)Source quote & editorial note
This phenomenon causes the cathode grid material from the IEC device to be deposited on the high-voltage (HV) stalk. That can in time cause premature breakdown at the stalk. ... The electrode is surrounded by a coaxial aluminum tube, which in turn is shadowed by a coaxial large diameter, aluminum tube. ... The stalk is a conical-shaped insulator facing toward the cathode grid that is expected to block the ions passing through the cathode grid. ... The corrugated surface is intended to lengthen surface current path lengths, preventing premature surface breakdown.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 87, 105, 109
Editorial note, tabletop extrapolation: In the reference machine's small chamber everything sees the source; a washer-stack or skirt shielding the feedthrough ceramic from the chimney slit is the same shadow-shield idea and should lengthen time between cleanings - validate on the actual geometry, since much of the sputtered flux travels as neutral atoms and simple line-of-sight shielding is the right first-order defense.
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Trade focusing against phase slip explicitly: you may drop Bz at large radius for extra focusing only if the ions have few turns left there, so raise the Dee voltage to cut the number of revolutions - fewer turns also means shorter path length and fewer gas collisions.
Source quote & editorial note
The axial component of the magnetic field can be decreased at larger radii in order to increase the radial (focusing) component, provided the ions only have a few revolutions left once they reach this portion of the field.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 27-28
Editorial note, tabletop extrapolation: One candidate for the reference machine's next big win: at ~150 keV on a low Dee voltage the turn count is large, and cutting it relaxes both the phase budget and gas-scattering exposure. Whether Dee voltage or field shaping pays more on a given machine is a diagnosis - measure what actually limits the beam first; the quote's own condition is narrower: late-radius focusing tricks need few turns remaining.
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When scanning the magnet at fixed RF frequency, current peaks can appear not just at the fundamental field B0 but at B0/3, B0/5, etc. (odd subharmonics) for each q/m species present - the cited thesis found spikes at or very near these theoretical resonances.
candidate peaks at B0, B0/3, B0/5, ... for each q/m; whether a peak is measurable depends on source abundance, capture and detectionSource quote & editorial note
the location of current spikes at a given field strength always occur at or very near the theoretical resonances... at B/3, B/5, and so on.
Editorial note, tabletop extrapolation: Essential for interpreting the reference machine's magnet scans: a peak at one-third field is likely a subharmonic, not a mystery species. H2+ vs H+ assignments need more than one matching peak - or an independent species diagnostic - since different q/m patterns can overlap.
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Raise dee voltage to raise beam current: fewer turns to a given radius means less path length and fewer gas collisions, and measured current increased with dee voltage at fixed field and pressure.
N_turns ~ E_final/(2*q*V_dee); higher V_dee -> shorter path -> higher transmitted currentSource quote & editorial note
It can be seen that in general, an increase in dee voltage results in a higher beam current.
Editorial note, tabletop extrapolation: For a fill-gas machine, dee volts are a strong current knob - the measured trend here: fewer turns, less path, fewer collisions. Whether they are THE binding knob depends on what limits the machine that day: source output, pressure, phase acceptance and detuning all compete (dg-359, dg-525). Measure before spending.
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Find resonance by a coarse-to-fine frequency sweep - the Houghton thesis used 0.5 MHz steps over the band, then 0.1 MHz, then 0.01 MHz around the peak - plotting dee-voltage gain (voltage gain between the RF amplifier and the dee), which peaks at resonance; the thesis's plot shows the maximum (~80x, read from its Fig. 37) at f0 = 3.55 MHz.
sweep steps 0.5 -> 0.1 -> 0.01 MHz (Houghton's sequence; scale the final step to the measured linewidth); gain ~80x at f0 = 3.55 MHz per Fig. 37Source quote & editorial note
the RF generator was adjusted in steps of 0.5 MHz ... adjusted in steps of 0.1 MHz near the maximum voltage ... a third sweep was performed using steps of 0.01 MHz ... The data points represent the voltage gain between the RF amplifier and the dee. The voltage gain will be a maximum at the resonant frequency. For this plot, f0=3.55MHz.
Editorial note, tabletop extrapolation: A simple, scope-only resonance-finding recipe after any mechanical change to a next machine's dee or stem: coarse-to-fine, with the fine step sized to the resonance linewidth rather than copied - and use a rated or noncontact voltage pickup on the dee side.
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Houghton's autotuner-matched dee circuit measured Q = 16.1 (f0/dF = 3.55/0.22 MHz; their earlier chamber measured 22) - far below the Q a directly coupled copper tank can reach.
Q = omega0/delta-omega_FWHM = 3.55/0.22 = 16.1Source quote & editorial note
the quality factor of the Houghton College cyclotron was determined to be Q=16.1. The previous chamber and dee constructed in 2006 had a quality factor of 22.
Editorial note, tabletop extrapolation: Quantifies the architecture choice: the reference machine's antenna-tuner match delivers kV-class dee voltage at low measured Q, and multi-kV wants a high-Q tank coil. The caveat travels: a low measured LOADED Q reflects the whole coupled system, matching-network losses included - so measure Q on the actual assembly and compare loaded with loaded when weighing the upgrade.
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Manual and analyzer-based resonance measurements disagreed at Houghton (3.55 vs 3.63 MHz, ~2 percent); the thesis attributes this to the HV probe near the dee adding capacitance and shifting the resonant frequency.
probe proximity shifted f0 by ~0.08 MHz (~2%) in the Houghton caseSource quote & editorial note
the resonant frequency occurred at f0=3.55 MHz ... Its results were f0=3.63 MHz at a SWR of 1.4:1 ... when the CT2591 HV probe was placed near the dee, the overall capacitance changed slightly. This would, of course, change the value of the resonant frequency.
Editorial note, tabletop extrapolation: When cross-checking NanoVNA SWR sweeps against powered probe measurements, probe loading is the first hypothesis for a small frequency disagreement - confirm it (adding the probe should lower the frequency, repeatably) before ruling out coupling, calibration-plane or mechanical causes; Houghton's 2 percent is their number, not a generic tolerance.
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Calibrate the pickup probe against a real HV probe: Houghton compared the CT2591 HV probe with the pickup probe, found real dee voltage roughly 11,300x the pickup voltage (linear fit, at 3.55 MHz), and had to recalibrate every time the frequency was adjusted since frequency affects the pickup reading.
V_dee ~ 1.13e4 x V_pickup (Houghton, linear fit at 3.55 MHz) - factor is frequency-dependentSource quote & editorial note
By comparing the CT2591 HV probe with the pickup probe, a scaling factor can be determined ... It was determined that the real voltage was roughly 11,300 times the pickup voltage. The frequency of the RF system will affect the values recorded by the pickup probe. For this reason, the probe had to be recalibrated every time the frequency was adjusted. The results given here were for a frequency of 3.55 MHz. ... A linear fit was performed and indicated that the real voltage was roughly 11,300 times the pickup voltage at an RF frequency of 3.55 MHz.
Editorial note, tabletop extrapolation: The pickup scale factor is frequency-dependent - the builder must recalibrate their pickup whenever they retune, not assume one constant.
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A tabletop machine can make measurable beam at very low RF power once matched: Houghton's commissioning test at SWR 1:1 and 15.43 W forward (3.55 MHz) yielded a 1.5 pA resonance peak near 0.23 T, protons collected at roughly 5.95 cm corresponding to 9.2 keV.
15.43 W forward, SWR 1:1, 3.55 MHz -> 9.2 keV protons at r ~ 5.95 cm, 1.5 pA resonance peak near 0.23 TSource quote & editorial note
First, the RF system was tuned to a resonant frequency of 3.55 MHz while the filament was set to 2.0 A and floated at -100 V relative to the chamber. At these settings, a SWR of 1:1 and forward power of 15.43 W were measured. ... there is a resonance peak with a magnitude of 1.5 pA at around 0.23 T. ... Collection took place at a radius of roughly 5.95 cm corresponding to proton energies of 9.2 keV.
Editorial note, tabletop extrapolation: Reassurance for commissioning a next machine: hunt for first beam at tens of watts with a clean match before scaling power - on the cited machine, detection sensitivity rather than RF power was the limiting factor at first beam.
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Higher dee voltage raises the fixed-frequency energy ceiling by reducing the number of turns (and thus accumulated relativistic phase slip); the particle survives while phase slip < pi/2, giving a maximum around 15 MeV for protons at 50 kV peak-to-peak.
accept while phase shift < pi/2; ~15 MeV max for protons at 50 kVppSource quote & editorial note
higher potential on the dees results in fewer orbits and a shorter time of acceleration, allowing for a higher maximum kinetic energy... gives a maximum of 15 MeV for protons with 50 kV peak-to-peak
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 24-26
Editorial note, tabletop extrapolation: At the reference machine's ~150 keV the relativistic shift is small (gamma-1 ~ 0.02%), but phase slip accumulates over the whole turn count, so low volts-per-turn can still spend the +/-90 deg budget well below the textbook ceiling (dg-273's summed-slip check). This rule sets the fixed-frequency ceiling for any future MeV-class ambition.
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Houghton's ion-source filament circuit: a standard AEI hairpin electron-microscope filament floating at about -90 V, heated by 2 A, with RF pickup on each filament lead shorted to ground through a 0.001 uF capacitor.
filament bias -90 V, heater 2 A, 0.001 uF RF bypass on each leadSource quote & editorial note
A standard AEI hairpin electron microscope filament floating at approximately -90 V is heated by 2 A of current ... RF pickup on each filament lead is shorted through a 0.001 uF capacitor to ground.
Editorial note, tabletop extrapolation: A replaceable-filament pattern worth copying next to a live dee: bias the filament, and RF-bypass every lead at the feedthrough - but size the bypass for the actual RF impedance and current, and use capacitors rated for the DC bias plus transients rather than copying 1 nF.
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The paper's machine oscillates the Dee at amplitudes up to approximately 3000 V against the grounded dummy Dee, and normal operation takes 10-40 W of RF - two statements about the same tank (its maximum and its routine point), not a measured pairing of the two.
10-40 W forward RF -> up to ~3 kV Dee amplitude; typical running 2100 VppSource quote & editorial note
the Dee may be oscillated with voltage amplitudes of up to approximately 3000V relative to the grounded Dummy Dee ... For normal operation, 10-40 W of RF power are required
Editorial note, tabletop extrapolation: Tells the builder that Dee voltage is a tank-Q problem, not a brute-force power problem: a modest amplifier into a good resonator beats a big amplifier into a lossy one - and dg-313's formula computes the actual watts-per-kV pairing for any target.
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Operate at as low an RF frequency as other constraints allow - ORNL's 1950s reasoning: far more oscillator engineering information existed below 15 megacycles.
prefer f < ~15 MHz where B and size permitSource quote & editorial note
It was believed desirable to operate at as low a frequency as possible because of the larger amount of engineering information available for oscillators in the region below 15 megacycles/sec.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 15
Editorial note, tabletop extrapolation: The reference machine's 9 MHz benefits from the modern form of the same effect: HF amateur-radio technique and parts are abundant below ~30 MHz. Today's sweet spots follow ham bands and ISM frequencies rather than a 15 MHz line; the transferable point is choosing field and frequency where the RF art is cheap.
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Budget dee excitation power from P ~ pi*f*C*V^2/Q with V the PEAK dee-to-ground voltage: the 86-inch's measured curve gave 96 kW of RF for 400 kV dee-to-dee with C = 176 pF, f = 13.5 MHz, loaded Q = 3700 (unloaded 12,300). [Corrected 2026-08-23: the earlier text did not say which voltage it meant, and the two readings differ by a factor of four. With those parameters the formula gives ~81 kW for 200 kV dee-to-ground (400 kV dee-to-dee, the source's figure, in sensible agreement with the measured 96 kW) and ~323 kW if 400 kV is read as dee-to-ground. State the convention, and peak versus RMS, every time this formula is used.]
P = pi*f*C*V_pk(dee-to-ground)^2/Q: with Q = unloaded Q0 this is resonator wall dissipation; with loaded Q_L it approximated the 86-inch's total RF input at their coupling (measured 96 kW vs 81 computed). For amplifier sizing use Q0 for the walls, then add coupling and beam losses and margin. 86-inch: f = 13.5 MHz, C = 176 pF, Q_loaded = 3700 (unloaded 12,300), V = 200 kV per deeSource quote & editorial note
This curve indicates that 96 kW of rf power is required for exciting the dees to 400 kv. ... The oscillator input was 162 kw.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 16, 25
Editorial note, tabletop extrapolation: Formula transfers once the conventions are fixed: at 9 MHz, ~50 pF and unloaded Q ~ 1000, 5 kV peak dee-to-ground dissipates ~35 W in the resonator - tens of watts, the FLOOR an amplifier must clear with margin for coupling loss, detuning and arcs. Double the voltage, four times the power.
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There is a calculable minimum (threshold) dee voltage to reach a given energy in a given field profile; design the RF system to exceed it with margin rather than discovering it empirically.
V_dee,min = f(E_final, B(r) profile); see ORNL-1196 Fig. 4 / Y-757Source quote & editorial note
It is possible to calculate the various effects quantitatively and to predict the minimum dee voltage required to obtain a given energy in a particular cyclotron.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 17-19
Editorial note, tabletop extrapolation: Directly applicable design step for a next machine: compute threshold voltage for the target energy and field taper before freezing the RF chain power budget.
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When beam current was pushed up on the source machine, sparking ended the climb: momentary readings above 2 mA were too unsteady to hold, so the sustained spark-free level - not the peak meter reading - is what that machine could deliver.
Source quote & editorial note
momentary beam meter readings exceeded two milliamperes but operation at this level was very unsteady due to sparking; further increases were not attempted
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 24
Editorial note, tabletop extrapolation: Test discipline for a next machine's dee-voltage conditioning: rate the machine at the level it holds quietly under a defined acceptance protocol (duty cycle, thermal soak, vacuum stability, RF interlocks), not at the level it touches momentarily.
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Expect gross RF-to-beam efficiency in the few-percent range: the 86-inch measured 2.6-9.3% gross (beam kW over oscillator DC input) and 30-44% counting all accelerated ions, with efficiency rising with dee-to-dee potential and beam power - the quoted trend.
gross eff = beam kW / oscillator DC input kW; 86-inch: 2.6-9.3% gross, rising with V_dee and beam powerSource quote & editorial note
As measured, efficiency tends to increase with dee-to-dee potential and with beam power.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 24-26
Editorial note, tabletop extrapolation: The order of magnitude transfers as expectation-setting: most RF power goes to resonator and ion-loading losses, so size a next machine's RF from resonator dissipation (dg-313), not from beam power.
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Use broad, clean, firmly clamped low-impedance contacts at every high-current RF joint: the ORNL 86-inch used two 12-in split silver-plated, water-cooled copper rings clamped around the dee stems, with the stems silver-plated over the adjustment range.
Source quote & editorial note
two 12 in. split silver-plated, water-cooled copper rings which can be clamped securely around the stems; the dee stems are also silver plated over the adjustment range
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 53
Editorial note, tabletop extrapolation: Scaled down: any sliding or bolted joint in the reference machine's dee-stem/coil path should be a broad, clean, firmly clamped contact - poor joints are a common and avoidable Q killer in small resonators; whether plating or water cooling is warranted follows from contact loss and temperature, not from the 86-inch's spec.
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Bring cooling water into RF-hot structures through insulating hose or RF-choke coils of the tubing itself: this machine insulated its dc-biased dees with roughly seven-foot lengths of two-inch rubber hose, and replaced the ceramic 'Lapp' water-lead insulators that failed at 200 kV with choke coils wound from copper tubing.
water leads: ~7 ft of 2 in rubber hose (DC bias) / copper-tube RF choke coilsSource quote & editorial note
Since the dees are insulated to operate at a dc bias, ... two-inch rubber hose about seven feet long are used to insulate the dees and to connect to the inlet and outlet headers at the extension wall. ... The ceramic 'Lapp' coils originally used for introducing cooling water to the tube and the plate line failed whenever the oscillator voltage was increased to give 200 kv. They have since been replaced with choke coils wound from copper tubing.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 55, 59
Editorial note, tabletop extrapolation: The principle - a conductive-liquid line into an RF-hot electrode must itself be an insulator or a choke - applies whenever a next machine adds cooling or bias plumbing to the dee. A hose is not automatically insulation: the water column conducts, so check coolant conductivity and path length for leakage current, the choke's impedance and self-resonance at the RF frequency, and creepage and pressure rating.
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The ORNL 86-inch supply architecture: multiple supplies each with a fused disconnect switch in its output, so the operator could remove a faulty unit from service without disturbing the remainder.
Source quote & editorial note
a fused disconnect switch in the output of each supply permits the operator to remove a faulty unit from service without disturbing the remainder
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 61
Editorial note, tabletop extrapolation: Modular paralleled supplies (or PA pallets) with individual protection can give a home machine graceful degradation - but that takes design, not just fuses: current sharing or ORing, backfeed isolation, DC-rated load-break disconnects, fault coordination, and a written de-energization procedure before anyone touches a unit. Never hot-swap hardware that wasn't designed and tested for it.
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Bias the dees negative - insulated, DC-biased dees were the 86-inch's cure for oscillator starting difficulties due to ion loading - so the self-excited oscillator starts cleanly.
insulated dee + negative DC bias, interlocked to RF (magnitude tuned in commissioning)Source quote & editorial note
Oscillator starting difficulties due to 'ion loading' are avoided by the use of insulated negatively-biased dees.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 7, 47
Editorial note, tabletop extrapolation: Directly applicable if a next machine's RF start-up stutters or the dee glows at low voltage: insulate the dee for DC and feed a negative bias through an RF choke. The same lever also bears on multipactor (dg-324), which lives in the same low-voltage start regime. The source records the method; the bias magnitude is found on the machine.
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One machine's design point for dee-to-liner spacing: its selected 100 kV peak required about 1.5 in of vacuum clearance (~26 kV/cm), taken at the minimum because magnetic gap is precious.
cited design point: ~1.5 in clearance at 100 kV peak (~26 kV/cm); not a linear scaling lawSource quote & editorial note
The selected value of 100 kv peak voltage requires about 1.5-in. clearance from dee-to-liner ... Since the magnetic gap is so precious ... this minimum value is taken for design.
Editorial note, tabletop extrapolation: The reference machine's 1.3 kV is electrically trivial by this calibration - its clearances are set by beam aperture and mechanical tolerance. For a 20-50 kV dee on a next machine, set clearance from electrostatic analysis of the actual geometry (edges, finish, conditioning, pressure regime), not by scaling kV/cm linearly.
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MAXIMUM energy gain per dee crossing is q*2*V0*sin(N*theta/2) for dee angular width theta at harmonic N - the particle's phase only reduces it - so half-dees and cut-away lips tax energy gain, and the tax grows with harmonic number.
dE_max per crossing = q*2*V0*sin(N*theta/2); actual gain carries the particle phase on topSource quote & editorial note
the maximum voltage gain/dee is Vd = 2*V0 sin(theta/2); for particles rotating on subharmonics of the dee frequency the angular width of the dee is n*theta to the particle
Editorial note, tabletop extrapolation: Directly applicable when trimming a next machine's dee for probe or source clearance: keep the dee close to 180 degrees or compute the sin(N*theta/2) penalty for the harmonic in use. Fundamental-mode trims are gentle - 15 degrees off costs about 1% at N = 1 - but the same trim costs more at higher harmonics.
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High dee voltage at practical drive power comes only from a high-Q resonant circuit - the quote; ORIC's implementation treats the dees and stems as a quarter-wave line foreshortened by dee capacitance, tuned via C, stem length, or stem impedance - the report's model, common for stem-fed dees though not universal.
dee system = lambda/4 line foreshortened by C_dee; tune via C, l, Z0Source quote & editorial note
The high dee voltage required in cyclotrons can be achieved for practical driving power only by using a high-Q resonant circuit.
Editorial note, tabletop extrapolation: Directly applicable framing for the reference machine's matching network: every dB of resonator Q lost to bad joints or lossy insulators is paid in amplifier watts.
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If multipactor blocks RF turn-on, either bias the dees or accept a more complex drive scheme; anticipate the problem at design time rather than after assembly.
Source quote & editorial note
it is possible to bias the dees to prevent multipactoring, and a more complex booster oscillator circuit is required
Editorial note, tabletop extrapolation: Directly applicable: multipactor lives in the low-voltage, MHz regime every starting tabletop dee passes through, so anticipate it - designing the dee stem so DC-bias insulation CAN be added is cheap at design time and expensive after. Whether the bias is actually needed is learned at first RF turn-on.
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The notebook's LDMOS build mounts the RF power board to its copper spreader with screws only - no solder - with heat-sink compound between the copper spreader and the aluminium heat sink.
Source quote & editorial note
No solder to hold the board to the spreader, the screws are enough. Heat sink compound between copper spreader and aluminum heat sink.
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 10
Editorial note, tabletop extrapolation: A workable pattern for a kW-class dee driver assembled from LDMOS boards - but the transistor/module manufacturer's mounting spec wins: check flange flatness, clamping force, and which interfaces want grease, pads, solder, or dry metal contact for the specific device.
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The cited LDMOS deck stabilized its low-frequency end with degenerative drain-to-gate feedback whose series inductances were literally 1.5 cm of #20 wire per side (~15 nH in that layout) - not wound coils.
L = 15 nH = 1.5 cm of #20 AWG wire, drain-to-gate, in series with feedback resistorSource quote & editorial note
the part description says '15 nH, connecting wires to R14 and R15, 1.5 cm each #20 AWG,' implying that they are just wires, not even coiled.
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 15
Editorial note, tabletop extrapolation: Relevant if building a broadband solid-state dee driver: these devices carry enormous low-frequency gain, so low-end stability needs deliberate design - feedback networks of this kind are one tool, verified by stability analysis or measurement on the actual amplifier; neither the 15 nH value nor certain oscillation without it transfers between layouts.
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Measure the actual harmonic spectrum before choosing any output filter - the source's classic way is a spectrum analyzer with about 40 dB of attenuation between amplifier and instrument: in this push-pull LDMOS deck the second harmonic was naturally attenuated by the topology, but the third came out only 8-10 dB down, and that is what the filter must attack.
spec: spurious 43 dB below carrier below 30 MHz, 60 dB for VHF; measured 3rd harmonic only 8-10 dB downSource quote & editorial note
many amplifiers use a push-pull topology that tends to attenuate the second harmonic. For those amplifiers, it is often the third harmonic that has the highest amplitude ... The classic way is with a spectrum analyzer ... you would want to have about 40 dB of attenuation between the amplifier and the measuring device. ... The real issue was the third harmonic, though; in general, it was only down 10 dB down and on some bands only 8 dB down.
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 19
Editorial note, tabletop extrapolation: A cyclotron dee tank is narrowband, but the rule holds: measure what the PA actually emits before designing filtering or worrying about interference from a garage machine. Take the sample through a power-rated coupler or sampler and compute the pad from actual PA power against the analyzer's rated input - at 1.4 kW (61.5 dBm) a bare 40 dB still leaves +21.5 dBm, too hot for most analyzers.
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In the source's solid-state PA, harmonic energy went to a dissipative diplexer rather than a reflective low-pass filter, because reflecting that energy back into the FET outputs risked driving the oscillations the designer had worried about in the power-deck design; weigh the same choice when a PA's stability data flag reflective harmonic terminations.
5-7 pole diplexers with crossovers at 2.7 / 6 / 11 / 25 / 42 MHz; 6-pole LPF at 65 MHz where 3rd harmonic was lowSource quote & editorial note
reflecting all that energy back into the output of the FETs risked driving the oscillations I had worried about in the detailed design of the power deck... I chose the diplexer
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 19-20
Editorial note, tabletop extrapolation: Relevant if the builder drives the dee with a broadband solid-state PA instead of a tube - but a harmonic diplexer does not protect the FETs from the dee's reactive load at the fundamental. That protection is matching, reflected-power shutdown and, where needed, an isolator; the diplexer only tames the harmonic terminations.
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Budget real tuning time after the first build: in the cited amplifier, cutoffs and crossovers designed too close to the operating frequencies produced excessive passband insertion loss and high VSWR, and virtually every part value changed during tuning - three months of it.
design settings used: Chebyshev, T-type, 0.005 dB passband ripple, >43 dB stopband <30 MHz, 60 dB aboveSource quote & editorial note
a fundamental flaw in my design settings had been that all the crossover and cutoff frequencies were too low, causing too much insertion loss and high VSWR in the passband.
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 20
Editorial note, tabletop extrapolation: Schedule measurement-and-adjustment time for any homemade filter bank, dee tank or matching network as a first-class line item; which DIRECTION values move is what the measurements tell you - this author's all-upward shift was his design's particular error, not a law.
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Add a series current-limiting resistor (20 ohm, 50 W) in the 50 V feed to the controller pass transistor and use 1000 V mica capacitors rather than 500 V in high-power filter positions; both failures happened in service.
20 ohm / 50 W series resistor; 1000 V micas replacing 500 VSource quote & editorial note
I also added a limiting power resistor (20 ohms at 50w) in series with 50v to the TIP102 as a precaution...with this resistor in place, a short on the 12v line will limit the current and prevent a catastrophic failure. ... I used 500v micas but slowly but surely I am changing them to 1000v specs because they are more robust.
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 31-32
Editorial note, tabletop extrapolation: Cheap fault-tolerance for a homebuilt RF deck, as the source built it. Check the fault arithmetic before copying: 50 V across 20 ohm is 2.5 A and 125 W, above the resistor's continuous rating, so the part rides through brief faults only - pair it with a fuse or fast shutdown rather than treating it as continuous-duty protection. Voltage-derating the filter caps matters more with the reactive load a dee presents.
-
Budget the losses between amplifier deck and load: the cited chain measured about 1.4 kW at the deck and delivered about 1.3 kW at saturation after T/R switches, harmonic filters and couplers - roughly a 7% tax in that installation.
1.4 kW at deck -> ~1.3 kW after T/R switches + filters + couplersSource quote & editorial note
the maximum output power I've measured ... is about 1.4 kW. After going through T/R switches, filters and couplers, you can expect about 1.3 kW at saturation
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 4
Editorial note, tabletop extrapolation: Size the RF chain from a component-by-component loss budget (relays, filters, couplers, feedline, matching, resonator) measured or taken from datasheets - the cited 7% is one chain's number; a cyclotron drive's tax depends on what sits in its line, so derive the PA headroom rather than assigning a stock percentage.
-
Do not assume silver plating lowers RF loss: much commercial silver plating runs near half the conductivity of pure copper, and a plating of about half the base conductivity produces the maximum possible increase in RF resistance.
electroplated Ag conductivity 0.13-95% IACS vs 105% for pure silver; worst case: sigma_plate ~ 0.5*sigma_baseSource quote & editorial note
a plating having about half the conductivity of the copper base will cause the greatest increase in overall resistance ... the conductivity of much of the commercial silver plating is about half of that of pure copper
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 1
Editorial note, tabletop extrapolation: Before specifying silver on the dee or coil, get the plating process's conductivity data and compare thickness to skin depth at 9 MHz; an uncharacterized jobbing-shop bright-silver finish risks raising resonator loss, while a verified high-conductivity deposit can lower it.
-
For a low-loss RF finish, plate with high-conductivity copper at least two skin depths thick at the operating frequency, then protect it with only a very thin low-conductivity layer or a low-loss lacquer.
t_Cu >= 2*delta; delta_Cu [um] ~ 66/sqrt(f_MHz) (22 um at 9 MHz, so plate >= ~45 um / 1.8 mil)Source quote & editorial note
a layer of high conductivity copper plating at least two skin depths in thickness, at the operating frequency, then protecting this against corrosion by a very thin layer of low conductivity plating or a layer of low-loss lacquer
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 10
Editorial note, tabletop extrapolation: For dees, stems, and tank coils at 9 MHz: copper at least ~45 um thick plus a thin low-loss protective finish beats unspecified decorative plating; properly specified high-conductivity silver can do better still, and nickel remains excluded on permeability grounds (dg-222).
-
A lower-conductivity plating hurts most at about 1.5 skin depths of the plated metal (the composite's resistance maximum); the mirror-image minimum for higher-conductivity plating is the companion result in the same analysis.
R_max at t ~ 1.5*delta_plating for sigma_plate < sigma_base; R_min at t ~ 1.5*delta for sigma_plate > sigma_baseSource quote & editorial note
The resistance of the composite conductor reaches a maximum value when the thickness of the plating is approximately one and one half times the skin depth for the plated metal.
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 3
Editorial note, tabletop extrapolation: Assess a proposed coating by computing the multilayer surface impedance with the coating's own conductivity AND permeability against its own skin depth - the trap case is a mid-thickness medium-conductivity layer, and magnetic coatings (nickel!) cannot be cleared by nonmagnetic skin-depth arithmetic; very thin protective flashes are usually small in effect at 9 MHz, verified by that same calculation rather than assumed harmless.
-
A thin gold flash (10 microinches) over silver is porous; the cited work found at least 200 microinches of gold necessary for adequate protection of the silver beneath.
t_Au >= 200 uin (~5 um) for adequate protection in the cited deposits; not established as pore-freeSource quote & editorial note
A gold flash (10 micro-inches) is often used although many workers have shown that the deposits are not pore-free and that at least 200 micro-inches of gold are necessary to provide adequate protection.
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 7
Editorial note, tabletop extrapolation: For RF contact fingers and connectors on the resonator, distrust thin gold flash: specify a qualified contact-plating system at proven thickness. Lacquer belongs only on non-contact surfaces, and only after RF-loss and vacuum-outgassing checks - never on a current-carrying contact interface.
-
Tarnished silver is a real contact-resistance hazard: silver-plated wire contacts rose from 6 milliohms to 200 milliohms after two hours in a hydrogen-sulfide atmosphere.
R_contact: 6 mOhm -> 200 mOhm after 2 h H2S exposureSource quote & editorial note
the contact resistance of two silver-plated wires rose from 6 milliohms to 200 milliohms after two hours' exposure to hydrogen sulphide.
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 7
Editorial note, tabletop extrapolation: Where sulfur contamination is credible (some shop atmospheres, rubber outgassing, industrial air), protect silver-plated RF joints or periodically inspect and measure their resistance - raised contact resistance heats under the resonator's high circulating RF current.
-
Smooth the RF surface: machining leaves a low-conductivity Beilby layer and 'hill and dale' current paths, so chemically or electrolytically polish conductors to lower RF loss.
Source quote & editorial note
Several reasons have been given for the decrease in conductivity below the bulk values, including: (a) the Beilby layer ... (c) the hill and dale effect ... This last problem has been investigated fully by Benson who recommends chemical or electrolytic polishing to produce a smooth surface and lower losses.
Fowler, Radio Frequency Performance of Electroplated Finishes — Proc. IREE Australia (1970) — p. 8
Editorial note, tabletop extrapolation: Polishing dee edges and stems lowers RF resistance. Smooth, clean, well-conditioned electrodes may also reduce field emission, but the breakdown voltage must be established by field analysis and testing - do not book the second benefit in advance.
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Give the amplifier controller hardware safety monitoring of temperature, load failure, and harmonic-filter outputs, with ALC feedback limiting the driver; the source's output chain also carries an LPF/SWR block, i.e. reflected-power sensing.
Source quote & editorial note
safety monitoring of temperature, load failure, and diplexer HPF outputs, and ALC feedback for driver
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 1
Editorial note, tabletop extrapolation: A directional coupler with fast drive-cut on high reflected power is a strong defense when the cyclotron dee arcs or drifts off resonance mid-run - one protection among the source's set (thermal, load-failure), not a complete answer on its own.
-
Use regulated, temperature-compensated gate bias to stabilize quiescent current, and feed VDD to each drain separately so high DC currents stay out of the RF output transformers (no DC core bias).
Source quote & editorial note
regulated and temperature compensated bias, separate VDD feeds to the output transistor drains to keep high dc currents out of the RF transformers
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 2
Editorial note, tabletop extrapolation: Directly applicable to a homebrew 9 MHz LDMOS deck: thermal-tracking bias holds the operating point against drift, and DC-free transformers remove one saturation mechanism - still verify RF flux density and transformer temperature at full drive.
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The QST author added degenerative (negative) feedback to the broadband MOSFET amplifier only after a 'smoke in the cockpit' failure about 350 contacts into service - build it in from the start.
Source quote & editorial note
the design underwent several changes along the way, including the addition of degenerative feedback after a 'smoke in the cockpit' incident after about 350 contacts had been made.
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 2-3
Editorial note, tabletop extrapolation: A dee resonator is a narrowband, sometimes-detuned load: design feedback in from day one with a stability analysis over the expected load range, and pair it with real mismatch protection - drain-current limiting and reflected-power foldback - since feedback alone is not a detuned-load defense.
-
Follow the LDMOS package's mounting specification and compute the whole junction-to-coolant thermal path: the source's construction flow-solders the output transistors to a thick copper heat spreader, which then mounts to the heat sink - use a spreader where flange heat flux demands it, and solder the package only when its assembly spec permits.
Source quote & editorial note
Rather than mounting the output transistors directly to a heat sink, they are first flow soldered to a thick copper heat spreader, which is then mounted to the heat sink.
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 3
Editorial note, tabletop extrapolation: At 100-500 W a copper spreader under the LDMOS pallet is cheap thermal margin; the reference machine's earlier MOSFET amplifiers died in service without a firm post-mortem, and die-temperature margin is the inexpensive insurance either way.
-
In the cited push-pull Class AB deck the third harmonic came out only 8-10 dB down (the topology suppresses the second), so output low-pass filtering was mandatory there - and the presumption for any new PA is measure first, then filter to what the measurement shows.
cited amp: 3rd harmonic -8 to -10 dBc before filtering; ARRL Lab table for the finished amp: 48-66 dB harmonic suppression across bandsSource quote & editorial note
But the real issue was the third harmonic, which was only 10 dB down generally and on some bands only 8 dB down!
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 3
Editorial note, tabletop extrapolation: At 9 MHz the 27 MHz third harmonic can couple into a spurious dee-resonator mode if one lies nearby; filter between amp and matching network, sized from the measured spectrum.
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Prefer a diplexer (absorptive) harmonic termination over a plain reflective low-pass on a solid-state HF amplifier when stability is in question: harmonic energy reflected back into the FET outputs can drive oscillations.
Source quote & editorial note
favored the diplexer design for solid state amps in the HF range, because reflecting all that energy back into the output of the field effect transistors (FETs) risked driving the oscillations
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 3
Editorial note, tabletop extrapolation: The dee's off-resonance reflection is a fundamental-frequency problem the diplexer does not solve: give the LDMOS reflected-power foldback or shutdown and, if needed, an isolator, and characterize the dee's impedance across its detuning range. The diplexer buys clean harmonic terminations - that is all.
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Treat the drain-trace tap point of the output transformer as a tuning element: its physical position along the trace sets the output match.
Source quote & editorial note
The position of the connection point at the drain trace is critical as it affects the match.
Buckler, A Solid State 1.25 kW Linear Amplifier — QST, January 2015 (2015) — p. 4
Editorial note, tabletop extrapolation: When copying an LDMOS pallet layout, preserve the cited design's output-transformer tap geometry, and if anything about it changes, remeasure the output match - the source says position is critical; how sensitive, at what power, is a measurement on the actual build.
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In the cited 12-inch geometry modelled in LANL's Poisson Superfish at 10 kV peak dee voltage, a dummy dee (grounded bar) of 3/8-inch thickness gave satisfactorily low distortion of the accelerating field lines.
dummy dee thickness 3/8 in = 9.5 mmSource quote & editorial note
A peak DEE voltage of 10kV was chosen. First the ion source was not included as to see the distortion in the field lines due to the DEE-Dummy DEE asymmetry. The distortion is satisfactorily low with a dummy DEE of 3/8-inch thickness.
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 2
Editorial note, tabletop extrapolation: Supports the single-dee/dummy-dee topology at the reference machine's scale: a ~10 mm grounded bar is a proven starting geometry that frees chamber space - re-run the electrostatic model for a new machine's own dee, gap and pole geometry.
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MIT's measured beam envelope: width limited by the dees' internal aperture out to about one-third of final radius, then narrowing nearly linearly to the exit slit - their amplitudes damping from 0.8 in initially to ~0.1 in at the slit.
adiabatic damping (n^(-1/4)-class) is the standard interpretation; MIT's measured center-to-exit damping factor ~0.12Source quote & editorial note
the beam width was found to be limited by the internal aperture of the D's out to about one-third of the final radius and then to narrow in a nearly linear fashion out to the exit slit.
Livingston & Blewett, Particle Accelerators (1962) — p. 163-167
Editorial note, tabletop extrapolation: Give the first third of radius generous vertical aperture - that is where the envelope filled the dee aperture on MIT's machine - and let the outer region run tighter, which also helps RF economy. Confirm on the actual machine (witness strips, dg-695) rather than assuming the same profile.
-
Use graphite for arc bodies, cones, and dee feelers near the source - it runs hot with minimal sputtering and evaporation; feeler extensions ('auspullers') on the dee faces opposite the source have been used to improve beam intensity - they decrease the physical spacings, raise the electric field at the source, and change the first electric lens's dimensions and focal properties.
Source quote & editorial note
Graphite is coming into wide use for cones, arc bodies, and also for D feelers or accelerating electrodes; it operates at high temperatures with a minimum of sputtering or evaporation. ... Extensions on the D faces opposite the source, called 'feelers' or 'auspullers,' have been used to improve beam intensity; they decrease the physical spacings and increase the electric field at the source. They also change the dimensions and focal properties of this first electric lens.
Livingston & Blewett, Particle Accelerators (1962) — p. 166-178
Editorial note, tabletop extrapolation: Graphite source parts run hot without spraying metal; a feeler on the dee edge is a cheap first-turn-capture upgrade with historical standing - though even the source notes quantitative evidence on its focusing effect was thin, so tune it empirically.
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There is no magnetic vertical focusing at the machine center (n=0 by symmetry); the first turns survive because the dee-gap electric field acts as an electrostatic immersion lens - so central-region electrode geometry and RF phase matter most in the first few turns.
n(r) ~ r^2 near center -> no magnetic focusing at r=0; gap E-field provides focusing, modified by transit timeSource quote & editorial note
There is no vertical magnetic focusing at the center of the magnet. By a fortunate coincidence, electrostatic focusing by the accelerating fields is effective for low-energy ions.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 524, 526
Editorial note, tabletop extrapolation: Explains why source-to-dee geometry (chimney position, puller gap, aperture height) dominates beam capture on small machines: at the center magnetic vertical focusing vanishes and only builds as n grows off zero with radius, so the electric gap lens is what the first turn or two get. Central-region electrode design is where capture is won on the documented machines.
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Particulate contamination on the cathode dominated vacuum breakdown in this test: at the source's 95 MV/m maximum field, 40 of 52 particle-contaminated sites broke down against 1 of 16 clean sites - strong enough association to make cleanliness a first-order control, though material, conditioning and geometry still matter.
at 95 MV/m (source's figure): contaminated sites 40/52 broke down vs clean 1/16Source quote & editorial note
most uncontaminated cathode sites did not break down at 95MV/m (figure 4.8). Excluding the two sites for which tests were halted prematurely (as explained in the caption of figure 4.8), 40 of 52 contaminated sites broke down, while only 1 of 16 uncontaminated sites broke down at or below the maximum field
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 78
Editorial note, tabletop extrapolation: A big lever on the reference machine's dee-voltage ceiling: gloves, solvent cleaning, and dust-free assembly of dee and stem are cheap holdoff - one major control among several, not a guarantee.
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Practical vacuum-gap breakdown fields span 5-200 MV/m, and smaller gaps withstand higher fields: in the source's data, fields above 100 MV/m were reached only with gaps under 150 microns - so do not credit millimeter-scale gaps with those numbers.
breakdown range 5-200 MV/m; >100 MV/m observed only at gaps < 150 umSource quote & editorial note
breakdown occurs between 5 and 200 MV/m ... In general, smaller gaps can withstand higher fields. ... Note that cathodes can reach fields higher than 100 MV/m, but, observing the maximum voltage, only with a gap smaller than 150 microns
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 78, 95
Editorial note, tabletop extrapolation: At 13 kV across the reference machine's ~6 mm gap the mean field is ~2 MV/m, comfortably low - but mean field is only the first check. Local enhancement at edges and asperities, particles, insulator surfaces and gas pressure can still start an arc, so treat sparking there as a diagnostic checklist, not an impossibility.
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Spark conditioning has a physical basis: in the early-processing regime each breakdown is overwhelmingly likely to raise that cathode site's breakdown field (successive/previous ratio > 1), with gains shrinking toward a saturation field.
E_breakdown(n+1)/E_breakdown(n) > 1 in early processing; gains shrink toward a saturation fieldSource quote & editorial note
In the 'early processing' regime, breakdown is overwhelmingly likely to increase the breakdown field of a cathode site.
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 91-92
Editorial note, tabletop extrapolation: Ramp the next machine's dee voltage slowly and accept the limited, current-limited micro-discharges that come with first processing - that conditioning is what raises the ceiling. Deliberately provoking arcs as 'cleaning' is a different matter: arcs can damage electrodes and insulators, and current limiting does not control the stored-energy delivery into the fault (dg-285). Let conditioning happen; do not manufacture it.
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Insulate the dee support stem by slipping a glass (pyrex) sleeve completely over it from the dee edge to at least 2 inches beyond the vacuum seal.
insulating sleeve extends >= 2 in beyond the sealSource quote & editorial note
slipping a 1/4 in. pyrex tube completely over the 3/16 in. copper dee support rod from the dee edge to at least 2 inches beyond the seal
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 7
Editorial note, tabletop extrapolation: The cited machine's construction: a continuous Pyrex sleeve over the dee support rod, extending well past the seal for creepage. For a new machine, design stem insulation from peak RF voltage, surface-flashover behavior and the sleeve-to-stem annulus (sealed or vented?) rather than copying the geometry - and note glass sleeves bring their own charging and thermal-stress habits under RF.
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Round every high-voltage edge and check it against Emax = 0.9V/(r*ln((r+a)/r)); the Rutgers team used 290 kV/inch as their aluminum design figure and chose a 0.1875-in minimum edge radius to keep the peak field at 170 kV/inch, about 60% of it.
Emax = 0.9V/(r*ln((r+a)/r)); source team's Al design figure 290 kV/in; their r_min = 0.1875 in -> 170 kV/inSource quote & editorial note
Aluminum=290 kV/inch ... We settled on a minimum radius of R=.1875 inches ... Emax=170 kV/inch
Editorial note, tabletop extrapolation: The method transfers to 5-13 kV dees: radius all dee and stem edges and check the enhanced field with the formula. The 290 kV/in is one team's design number, not a material constant - vacuum holdoff moves with gap, finish, contamination and conditioning - so copy their margin practice (peak field well under the adopted figure), not their number.
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Support the dee against the dummy dee with machinable-ceramic spacer strips - Houghton used four, ~2.53 x 0.77 x 0.18 cm, setting a 0.635 cm acceleration gap - after a discharge from the dee to the chamber wall damaged the earlier glass insulation.
gap = 0.635 cm; 4 ceramic strips 2.53 x 0.77 x 0.18 cmSource quote & editorial note
a discharge from the dee to the chamber wall damaged the glass insulation and 'dee' electrode ... Four machinable ceramic strips, each roughly 2.53 cm long, 0.77 cm wide and 0.18 cm thick, hold the two dees together at the appropriate separation gap of 0.635 cm.
Editorial note, tabletop extrapolation: Machinable ceramic (Macor-class) spacers are the pattern to copy for the reference machine's dee-to-dummy-dee gap; ceramics still flash over and track, so verify surface-field and creepage margins for the actual gap and voltage rather than treating the material as spark-proof.
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Design the chamber, dee, dummy dee and filament to disassemble with screws rather than glue or solder - the 2006 Houghton chamber's glued glass insulation could not be repaired after a dee-to-wall spark, forcing a complete rebuild.
Source quote & editorial note
This design strategy made it impossible to fix a single component of the apparatus, such as the insulation, without replacing the entire piece.
Editorial note, tabletop extrapolation: A next machine should assume sparks and insulator damage happen across a machine's life: modular fastening where practical turns rebuilds into part swaps - the source's glued chamber is the cautionary case. Where glue or solder is structurally necessary, design the bonded assembly itself as the replaceable unit.
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Vent every blind screw hole in the dee - Houghton drilled a small side hole into each with a No. 55 drill bit - so trapped air and water don't slowly outgas into the vacuum.
No. 55 drill (~1.3 mm) side vent per screw holeSource quote & editorial note
To vent the screw holes, a small hole was drilled in the side of each screw hole using a No. 55 drill bit. The screw holes need to be vented so that they do not trap air or water and slowly outgas when the dee is placed in the vacuum chamber.
Editorial note, tabletop extrapolation: Directly applicable to any screwed-together dee: unvented blind holes are virtual leaks that slow pumpdown and add residual gas load - size and place vents for conductance and cleaning access.
Cited in: The Vacuum Budget of a Cyclotron
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Insulate the filament (1-3 V DC) from the dee, which sits at 1-2 kV RF in this machine class, with a ~0.18 cm machinable ceramic plate; barrel connectors epoxied to the ceramic carry the leads.
dee RF 1-2 kV vs filament 1-3 V; 0.18 cm ceramic insulatorSource quote & editorial note
the RF voltage on the dee is typically between 1 and 2 kV, far greater than the 1-3 V DC placed across the filament. Thus, the filament and wires must be adequately insulated from the dee ... Insulation was supplied by a 2.33 cm by 2.71 cm machinable ceramic rectangle approximately 0.18 cm thick. ... Two barrel connectors, each 1.28 cm long and 0.32 cm in diameter, were glued to the ceramic insulator using Hysol Loctite 1C vacuum epoxy
Editorial note, tabletop extrapolation: Matches the reference machine's ~1.3 kV operating point today. At the planned 5-13 kV, do not just scale the creepage proportionally: reassess peak field and vacuum surface flashover for the actual geometry and check the feedthrough's rating.
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Build the Dee/dummy-Dee pair from one 1.27 cm thick, 0.6 cm wide aluminium ring of 15.6 cm OD, cut into a 7.8 cm Dee and a 3.2 cm dummy Dee separated by 0.635 cm ceramic spacers, skinned with 0.13 cm sheet and supported on three KF-16 feedthroughs at 120 degrees.
ring 15.6 cm OD, 1.27 cm thick; Dee 7.8 cm wide, dummy 3.2 cm; accelerating gap 0.635 cm; skins 0.13 cm; 3 supports at 120 degSource quote & editorial note
Ceramic spacers hold the Dee and Dummy Dee apart with a gap of 0.635 cm. The entire Dee electrode assembly is supported by three KF-16 electrical feedthroughs through ports at 120 degrees from each other. ... A circular ring of 6061 T6 aluminium, 1.27 cm thick, 0.6 cm wide, and 15.6 cm outside diameter, formed the walls for both the Dee and Dummy Dee. Two 5052 aluminium sheets, 0.13 cm thick, were fastened to the top and bottom of the ring with vented screws.
Editorial note, tabletop extrapolation: Direct fabrication prior art at exactly tabletop scale; the single-Dee-plus-dummy topology needs live RF on only one electrode - the design rationale for fewer HV feedthroughs - and the vented screws are the kind of vacuum detail worth copying wholesale.
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Electric-field defocusing near the center loses roughly 90% of starting ions to the dee surfaces; reduce the loss by raising dee voltage so ions make fewer turns and accumulate less phase shift.
higher V_dee -> fewer turns -> smaller phase slip and center lossSource quote & editorial note
some 90% of the initial supply of ions are lost to the dee surfaces. The loss may be reduced by increasing the dee voltage, thus reducing the number of turns an ion makes
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 18
Editorial note, tabletop extrapolation: Directly applicable: at 1.3 kV the reference machine's protons make many turns, and the quoted machine cut its central losses with more dee volts. A strong transmission lever - alongside central-region geometry (dg-348), which shapes what the first turns even see; measure which binds before spending (dg-303).
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The historical design furnace-brazed five loops of flattened 7/8-in copper tubing to 1/8-in copper dee sides; both cooled designs proved satisfactory, and the brazed-tubing one was much easier and less expensive.
Source quote & editorial note
The sides of the second set of dees are 1/8 in. copper with five loops of 7/8 in. copper tubing flattened and furnace brazed ... Both designs have proved satisfactory but the latter is much easier and less expensive.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 50
Editorial note, tabletop extrapolation: At 1.3 kV and tens of RF watts the builder probably needs no water - but decide from computed or measured dissipation and temperature, not from voltage. If a next machine's dee runs kilowatt-class RF, brazed-on flattened tubing is the historically cheap construction; substituting soft solder needs its own validation (joint temperature, strength, vacuum compatibility).
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Perforate the peripheral walls of dees and liner so the dee interior pumps fast, and face surfaces the stray beam can strike with graphite to protect copper and limit induced radioactivity.
Source quote & editorial note
The peripheral walls of the dees are perforated to permit high pumping speed. Graphite plates are attached to the inside of the dees ... to protect the copper from the stray proton beam.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 50, 7
Editorial note, tabletop extrapolation: Perforation transfers directly - pressure inside an unvented dee can sit far above gauge pressure (the dee interior is a conductance-choked volume). Graphite armor earns its place wherever stray beam dwells, at ANY energy: heating, sputtering and erosion first (dg-426's material lesson), with activation reduction joining the list at higher energies.
Cited in: The Vacuum Budget of a Cyclotron
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Prefer oil diffusion pumps over mercury for accelerator columns: mercury vapor promotes autoelectronic (field-emission) discharges from high-voltage electrodes, and fast pumping is needed for steady discharge conditions.
Source quote & editorial note
Fast pumping is required and it is desirable to use oil rather than mercury diffusion pumps as mercury seems to promote autoelectronic discharges from the electrodes.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 259-260
Editorial note, tabletop extrapolation: Moot for pump choice today; the observation transfers cautiously: the source found mercury vapor SEEMED to promote field emission from HV electrodes, and condensable conductive films on electrodes are a recognized breakdown risk generally - keep electrode surfaces free of deposition, sputtered films included (dg-261's clean-surface caveat).
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A canal-ray (obstructed glow) proton source: maximum current came from a discharge at about 20 kV, with the Faraday cylinder collecting on the order of 1 mA against 20 mA in the discharge - a 5% collected-to-discharge current ratio in that geometry.
cited apparatus: ~20 kV optimum; 1 mA collected / 20 mA discharge = 5% (collected current, species unresolved)Source quote & editorial note
the maximum current is produced from a discharge running at about 20,000 volts... the current collected by the Faraday cylinder F into which it can penetrate is of the order of 1 milliampere with 20 milliamperes in the discharge.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 260-261
Editorial note, tabletop extrapolation: Sets the historical scale: percent-class collected current from tens of mA of glow discharge - a budgeting anchor, not a conversion efficiency; aperture acceptance, extraction and species mix all live inside that 5%, so measure your own ratio before sizing the discharge supply.
-
Keep the anode-cathode annular gap too small for a discharge to build up in it - the cited source spaced its coaxial steel tubes about 4 mm apart - so the discharge concentrates naturally on the cathode canal hole; the cathode and tubes can run red-hot and radiate their heat.
cited geometry: ~4 mm annular clearance (that gas, pressure and voltage - validate the suppression gap for your own conditions)Source quote & editorial note
The space between the two steel tubes is too small for a discharge to build up there and it concentrates naturally on the hole in the cathode. ... The anode is a second steel tube A, supported axially inside the cathode and separated from it by about 4 mm ... the cathode C and the steel tubes can run red-hot
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 260-261
Editorial note, tabletop extrapolation: The 'gap smaller than the discharge can live in' principle is how a builder forces the source discharge to localize at the extraction aperture rather than wander - pick the clearance for the actual gas, pressure and voltage and verify it empirically; the 4 mm is the source's worked point.
-
A fresh hydrogen discharge beam is largely molecular ions, becoming nearly all protons only after extended running - condition the source before assuming beam species, and verify with magnetic analysis. The source's own kinematics: an H2+ at the full accelerating voltage is a pair of protons each carrying half the energy, so disintegration onset appears at about twice the voltage and the yield curve rises twice as steeply.
at fixed accelerating voltage: H2+ of energy E = two protons of E/2 (onset doubles, curve twice as steep); at fixed magnetic rigidity each constituent carries ~1/4 the proton energy; H2+ orbits at half the proton cyclotron frequencySource quote & editorial note
At first this beam consists very largely of molecular ions, but after running for some time it changes over and becomes nearly all protons ... The H2+ ion may be thought of as a pair of protons travelling together with an electron. The binding energy between them is negligible compared with the kinetic energy, which for either proton is one-half the energy of the particle. Hence a given current of molecular ions represents a current of protons of twice the magnitude, but with half the energy. We would therefore expect to begin to detect disintegration particles at about twice the energy found for the protons, and that the curve would rise twice as steeply.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 261-262, 269
Editorial note, tabletop extrapolation: For p-B11 the point survives translation with care: a proton-tuned cyclotron does not even hold H2+ in resonance (half the cyclotron frequency), but any acceleration mode that does deliver molecular ions yields constituent protons at a half (fixed voltage) or a quarter (fixed rigidity) of the expected energy - and p-11B is exothermic with no kinematic threshold, so what collapses is the cross-section-weighted yield, not an on/off threshold.
-
Degas an accelerating column by running a hydrogen discharge at about 20-60 kV, then pump out: in the source's experience the tube was then quite hard and stable up to 200 kV, and once degassed, about half an hour of running each morning restored steady state.
conditioning discharge ~20-60 kV; after pump-out, stable to 200 kV; ~30 min morning run restores steady state (source's experience)Source quote & editorial note
When it was once degassed it was only necessary to run for about half an hour in the morning to get the tube into a steady state. It was found to be most easy to degas the main accelerating electrodes and tube by admitting hydrogen till it was possible to run a discharge at about 20-60 kilovolts... on pumping out the hydrogen it is usually found that the tube is quite hard and stable up to 200,000 volts.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 265
Editorial note, tabletop extrapolation: A historical conditioning observation for electrode structures that must hold voltage - adapt, don't copy: ramp with current and stored-energy limits, remote operation, interlocks, and a measured breakdown-rate criterion, and remember DC column conditioning does not transfer one-to-one to RF dees.
-
If measured beam current is very low even close to the ion source (the large-turn-spacing region where probe masking cannot be the cause), be suspicious of the ion source first.
Source quote & editorial note
one should be suspicious of the ion source if the measured beam current is very low in the region close to the ion source, i.e. the regime of large turn spacing
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 1
Editorial note, tabletop extrapolation: A triage order for the reference machine's low-current debugging: measure current at small radius first; if it's already low there, put ion production and extraction at the top of the checklist - while still verifying RF capture, focusing, alignment and the probe itself, since the clue is suggestive, not exclusive.
-
Livingston & Blewett's worked hot-cathode arc source: 3 A discharge at 100 V, ~2 A electron beam from the exit hole, gas flow 2 cm3/min at atmospheric pressure - and a resonant ion beam that 'might be about 0.5 mA'.
arc 3 A at 100 V; electron beam ~2 A; gas 2 cm3/min (STP); resonant beam 'might be about 0.5 mA' (their words)Source quote & editorial note
arc current, 3 amp; arc voltage drop, 100 volts; electron beam from exit hole, 2 amp; gas flow, 2 cm3/min at atmospheric pressure. The resonant ion beam pulled from such a source ... might be about 0.5 ma.
Livingston & Blewett, Particle Accelerators (1962) — p. 175-178
Editorial note, tabletop extrapolation: The architecture point transfers at any size: a differentially pumped source cavity running much higher pressure than the chamber, fed through the exit hole (the Penning-table rules carry pressure numbers - dg-372). The single operating point is a sanity anchor for a similar source, not a spec or a promise of half a milliamp.
-
Heat the source cathode with DC or ~100 kHz AC rather than low-frequency AC, to avoid vibration damage in the magnetic field; keep oxygen out of the gas (it materially shortens cathode life) and expect reported service lives of 100-200 hr, ended by erosion of the emitting spot on the cathode.
cathode: heavy W or Ta rod; heating dc or ~100 kc; reported life 100-200 hr (erosion of an exit-hole-sized spot)Source quote & editorial note
The heating power is either dc or high-frequency ac (~100 kc) to avoid damage from vibration in the magnetic field at low frequencies. Cathode life is ... materially shortened by traces of oxygen. Lifetimes in service of 100 to 200 hr have been reported. The limit is due to erosion of a small area the size of the exit hole on the cathode surface, which represents the effective emitting surface.
Livingston & Blewett, Particle Accelerators (1962) — p. 177-178
Editorial note, tabletop extrapolation: A mains-frequency-heated filament in a 0.59 T field risks vibrating itself to death; DC heating and clean hydrogen are cheap reliability.
-
MIT's machine: base pressure better than 1e-6 mm Hg with no gas flow, about 2e-5 mm Hg operating with deuterium flowing - the ion-source gas load, not outgassing, set the working pressure on that machine (2400 l/s of pumping on a 2000 l volume).
MIT: 2400 l/s on 2000 l volume; base <1e-6 mm Hg, operating ~2e-5 mm Hg with D2 flowSource quote & editorial note
With no gas flow, chamber pressures of better than 1 x 10-6 mm Hg are obtained. With the deuterium gas flow from the ion source, the operating pressure is about 2 x 10-5 mm Hg.
Livingston & Blewett, Particle Accelerators (1962) — p. 198
Editorial note, tabletop extrapolation: Expect a large pressure rise when source gas flows: on a tight system the flow-on/flow-off ratio identifies the source as the load, while a rise WITHOUT flow is the leak-or-outgassing signature. What operating pressure a machine can afford is the beam-survival calculation's answer (the vacuum calculator's orbit mode), not MIT's 2e-5.
Cited in: The Vacuum Budget of a Cyclotron
-
Heat a spiral filament ion source with high-frequency AC: the cited machine used it to minimize destructive magnetic effects on the spiral - the heater current interacting with the main magnetic field produces alternating J x B forces that the filament cannot mechanically follow when the frequency is high.
Source quote & editorial note
The filament is heated to incandescence by a high-frequency a-c power supply. The high-frequency is used to minimize self-destructive magnetic effects in the spiral filament.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 7
Editorial note, tabletop extrapolation: A real failure mode for hairpin/spiral filaments in a strong main field. DC removes the alternating force entirely (at the cost of a static deflection), so the practical choice is high-frequency AC or DC depending on filament geometry - mains-frequency AC is the option to avoid; filament life is a chronic tabletop complaint either way.
-
Penning-source housekeeping numbers from the handbook's table: gas consumption ~0.2 sccm, source pressure 1-10 Pa, ignition needs 3-5 kV even though the running arc is 0.3-1.3 kV (1-5 kV for the high-arc column); the same table carries extraction voltages and chimney aperture/cathode-spacing ranges for the larger machines.
gas ~0.2 sccm; p_source = 1-10 Pa; V_ignition = 3-5 kV; V_arc = 0.3-1.3 / 1-5 kV (the table's two columns)Source quote & editorial note
Operating Data of Penning Ion Sources: Arc voltage 0.3-1.3 / 1-5 kV; Ignition volt. 3-5 kV; Gas pressure 1-10 Pa; Gas consumption 0.2 sccm.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 101
Editorial note, tabletop extrapolation: The reference machine's MFC should be sized and calibrated around the table's ~0.2 sccm scale, and the arc supply must tolerate a several-kV open-circuit ignition transient before folding back to run voltage - the table's ignition/run split is the reason.
Cited in: The Vacuum Budget of a Cyclotron
-
Match structural metals to their real vacuum temperature limits: stainless to ~1000 C (alloys with Ta/Mo above 900 C!), Mo to 2000 C (goes brittle, use TZM), Ta to 2600 C, W to 3400 C but nearly unmachinable, W-Re alloys are formable filament stock, graphite to 3500 C but outgasses and holds a memory effect.
service limits: Cu 600 C, Ti 800 C, SS 1000 C, Mo 2000 C, Ta 2600 C, Re 3150 C, W 3400 C, graphite 3500 CSource quote & editorial note
Copper is suited for low-temperature operation (600 C) and for cooled ion source parts. ... Stainless steel is an excellent material up to about 1000 C... It forms low-melting alloys with tantalum and molybdenum above 900 C... Tungsten... has the highest melting point of about 3400 C and is best suited for filaments.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 355
Editorial note, tabletop extrapolation: The trap in a source chimney is any hot joint touching stainless: the source's warning is that stainless alloys with BOTH tantalum and molybdenum above 900 C, so an intermediate piece helps only if the stainless contact itself stays below the reaction range - move the joint to a demonstrably cooler region or add thermal length. And check pairs, not just single-metal limits: graphite on hot tantalum can form carbides.
-
Pick hot-zone insulators by temperature and outgassing: Macor machinable but brittle, good vacuum behavior to ~1000 C; boron nitride excellent to 1200 C and usable to 1500 C where it starts to decompose and release large quantities of nitrogen - but it outgasses badly and absorbs water, so bake gently after air exposure; alumina is the high-temperature workhorse of the source's list.
Macor ~1000 C; BN 1200 C (to 1500 C, decomposing, N2 release); source's list also gives quartz ~1000 C, alumina 1400 C, zirconia 1600 C (conductive above ~1000 C)Source quote & editorial note
Macor or glass ceramic can be easily machined, but is very brittle. It has good vacuum behavior and can be used up to about 1000 C. ... Boron nitride is an excellent material for most applications for temperatures up to 1200 C. It can be used up to 1500 C but starts to decompose and releases large quantities of nitrogen. It outgasses badly and tends to absorb water, which can destroy the parts when heated too fast.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 356
Editorial note, tabletop extrapolation: BN filament insulators in a home source must be pre-baked and brought up to arc power slowly the first time after air exposure, or they crack and gas up the chamber.
-
Space-charge-limited extraction current density follows Child-Langmuir in practical units: j[mA/cm^2] = 1.72*sqrt(q*/u)*U[kV]^1.5/d[cm]^2 -- for protons at 10 kV across a 5-mm (0.5 cm) gap that is ~220 mA/cm^2, far above a hobby cyclotron's needs. [Correction, Aug 2026: the source prints the denominator as d[mm], but the 1.72 coefficient requires d in centimeters; the originally extracted example (~2.2 mA/cm^2) was low by 100x. Verified against the SI form of Child-Langmuir. The verbatim quote below preserves the source's own text.]
j[mA/cm^2] = 1.72*sqrt(q*/u)*(phi[kV])^(3/2)/(d[cm])^2Source quote & editorial note
In more practical units, this equation can be rewritten: j[mA/cm2] = 1.72 * sqrt(q*/u) * phi[kV]^(3/2) / d[mm]^2.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 376-377
Editorial note, tabletop extrapolation: Confirms the reference machine's nA beams are nowhere near space-charge limits; if extraction is weak the problem is geometry/plasma matching, not the Child-Langmuir ceiling.
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Design round-aperture extraction around an aspect ratio (aperture radius : gap) of S ~ 0.5; the source's Eq. 11 - built on its Refs. 11 and 12 - then estimates the per-aperture current limit I[mA] = 0.703*sqrt(q*/u)*U[kV]^1.5, and the plasma density must be matched to the field or the beam over/under-focuses.
S = r/d ~ 0.5; source Eq. 11: I[mA] = 0.703*sqrt(q*/u)*U[kV]^(3/2) - carries the cited references' corrections, not bare Child-Langmuir (ideal round-aperture CL at S=0.5 gives a coefficient near 1.35); divergence w0 = 0.5*(r/d)*(1 - 1.67*Pi_normalized), round aperturesSource quote & editorial note
For the cylindrically symmetric case the maximum current can be estimated from References 11 and 12 and the assumption of a certain aspect ratio (aperture radius to electrode separation). A good aspect ratio is on the order of S = 0.5.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 379
Editorial note, tabletop extrapolation: For the puller gap in a next machine, carry over the shape of the rule - aperture dimension about half the extraction gap, beam parallelism tuned by matching plasma density - but the cited numbers are for round apertures: model the actual chimney slit electrostatically or by simulation rather than substituting the slit half-width, and expect to adjust both arc density and geometry.
-
Size thermionic cathodes with the Richardson formula, where temperature is the STEEPEST knob - a 10% temperature change swings emission ten- to a hundred-fold, the quoted sensitivity - so regulate filament heating tightly.
j_sat = A*b*T^2*exp(-e*phi/kT) A/cm^2, A = 120.4 A/cm^2K^2; W: phi = 4.54 V, A*b = 60; Ta: phi = 4.12 V, A*b = 60; thoriated W (Th on W): phi = 2.63 V, A*b = 3.0Source quote & editorial note
The increase of the saturation current with temperature is very strong; a 10% change in temperature corresponds to a 10-fold increase of 20% to a 100-fold increase.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 38-39
Editorial note, tabletop extrapolation: The reference machine's hydrogen filament source lives or dies on filament temperature stability, so a finely adjustable constant-current supply is worth more than raw power. Area, work function and surface condition set the baseline the temperature knob multiplies - and space-charge-limited extraction caps what raw emission increases can deliver.
-
Budget filament heater power from radiation: refractory-metal filaments radiate roughly 20 W/cm^2 of surface at 2000 K, and nearly all input power leaves as radiation rather than end conduction, so the surrounding chimney/anode must take that heat.
P_rad ~ 20 W/cm^2 at 2000 K (W, Ta, Mo similar); at fixed temperature: I ~ d^1.5, V ~ l/sqrt(d)Source quote & editorial note
Most of the power put into a filament is radiated and very little is lost through the ends. Most high-temperature metals show similar radiation behavior (~20 W/cm2 at 2000 K).
Wolf (ed.), Handbook of Ion Sources (1995) — p. 39
Editorial note, tabletop extrapolation: A few cm^2 of hot filament dumps tens of watts into the reference machine's source body; the hood/chimney around the filament needs a conductive heat path to the pole or water cooling.
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Run refractory filaments at the lowest temperature that gives enough emission - evaporation-limited lifetime is savage: the handbook's tables give a 1-mm W wire ~8,300 h at 2500 K but ~46 h at 2900 K, and a 1-mm Ta wire ~7,000 h at 2400 K but ~350 h at 2600 K, with lifetime scaling linearly with wire diameter.
evaporation-limited estimates, 1-mm wire: W 2500 K -> 0.30 A/cm^2, 8.3e3 h; 2700 K -> 1.6 A/cm^2, 500 h; 2900 K -> 7.3 A/cm^2, 46 h. Ta 2400 K -> 0.65 A/cm^2, 7.0e3 h; 2600 K -> 2.7 A/cm^2, 350 h. Life proportional to diameterSource quote & editorial note
The increase of temperature for higher electron output is limited by the increasing evaporation of cathode material, which decreases the cathode lifetime. Tables 1.2 and 1.3 give the respective data for W and Ta.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 41-42
Editorial note, tabletop extrapolation: For a next machine, a fatter filament run cooler at ~0.1-1 A/cm^2 buys far more run time - but the tables are evaporation-limited upper estimates: in a real arc source, ion bombardment, sputtering and contamination can dominate, so measure actual filament life rather than banking on the table.
-
Discharge-type sources with good confinement reach >=50% gas efficiency (multicusp: >50% for hydrogen), while poorly confined sources run 10-20%; every neutral that escapes the chimney loads the main vacuum, so gas efficiency is a vacuum-design parameter.
gas efficiency: multicusp/e-bombardment <=50% (H2 >50%); plasmatron family 10-20% to 50%Source quote & editorial note
Gas efficiency: >50% for hydrogen and higher for other gases.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 57, 69, 110
Editorial note, tabletop extrapolation: At 0.2 sccm feed and 50% efficiency only ~0.1 sccm leaves the chimney as neutrals - but the extracted ions end their lives in the same vacuum envelope (implanted, neutralized, desorbed later), so higher gas efficiency shifts where and when the load appears more than it deletes it. It still pays: neutral leakage at the source is continuous and concentrated in the beam region, so better confinement is worth real pumping speed there even though total throughput is conserved.
Cited in: The Vacuum Budget of a Cyclotron
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Expect 10-100 h filament life in this source class; the Freeman template is a quiet 40-70 V, 1-3 A arc with a quite massive ~2-mm Ta or W cathode rod heated by ~130 A at a few volts. Erosion concentrates at the positive filament end, so changing heater polarity after some running time improves cathode lifetime; AC heating evens the wear but increases plasma instabilities and ion energy spread.
filament life 10-100 h (cited source class); Freeman: V_arc 40-70 V, I_arc 1-3 A, ~2-mm rod cathode, I_heat ~130 A; reverse heater polarity after some running timeSource quote & editorial note
The arc current is 1 to 3 A and the arc voltage just 40 to 70 V. A quite massive cathode rod, usually 2 mm in diameter and made of tantalum or tungsten, is heated with about 130 A and a few volts to the right temperature. ... The erosion of the filament is not uniform, but stronger at the positive end due to electron movement and higher plasma density. Changing the polarity of the filament after some time of operation improves cathode lifetime. Heating by ac has the same effect but increases plasma instabilities and the energy spread of the extracted ions. ... The lifetime of the source is given by the lifetime of the filament, which is between 10 and 100 h
Wolf (ed.), Handbook of Ion Sources (1995) — p. 73
Editorial note, tabletop extrapolation: For a next machine: a thick rod cathode instead of thin wire is the cheap lifetime upgrade, plus an arc-hours log. Polarity reversal on a ~130 A heater that may float at source potential is not a toggle-switch job - reverse only de-energized and discharged, through buswork or contactors rated for the heater current and the source-to-ground voltage.
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Standard extraction slit for slit-type arc sources is about 2 mm wide by 40 mm long; longer slits (90 mm cited; designs to 100 x 5 mm realized) lose current-density uniformity along the slit because of the bigger voltage drop along the cathode - though the source notes careful anode and field design has overcome this.
slit ~ 2 x 40 mm typical; 100 x 5 mm max realizedSource quote & editorial note
The extraction slit is usually about 2 mm wide and about 40 mm long. Larger slits are possible, such as 90 mm, but there are some disadvantages because the current density is not uniform along the long slit due to the bigger voltage drop along the cathode. By careful design of the anode and the magnetic field, however, it was possible to overcome this problem. ... The extraction slit is usually 40 x 2 mm but designs up to 100 x 5 mm have been realized.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 74, 76
Editorial note, tabletop extrapolation: For a cyclotron chimney, the ~2 mm slit width is the historical arc-source value to start from; the slit's length and total area still matter for gas load, arc stability and beam interception, so optimise chimney length and aperture for the actual puller and dee geometry against measured beam. [Note revised 2026-08-23: earlier note said only the few millimetres facing the dee gap matter.]
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PIG/Penning discharges split into two useful regimes: cold-cathode (arc above 1 kV at 0.5-5 A) and hot-cathode (arc below 1 kV at 1-50 A); the handbook adds that the magnetic field matters little above a minimum around 0.1 T, and that arc voltage rises as gas flow is cut until the discharge goes unstable.
cold cathode: V_arc > 1 kV, I = 0.5-5 A; hot cathode: V_arc < 1 kV, I = 1-50 A; B_min ~ 0.1 T; high-pressure regime 0.1-100 PaSource quote & editorial note
The cold cathode PIG source with arc voltages above 1 kV and currents between 0.5 and 5 A, and the hot cathode PIG source with arc voltages below 1 kV and currents between 1 and 50 A.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 81-82
Editorial note, tabletop extrapolation: The reference machine's center field clears the handbook's 0.1 T minimum, which makes an internal PIG a candidate - trading the fragile filament for a self-heated cathode running a sub-kV, multi-ampere arc. Suitability is more than field magnitude: geometry, cathode cooling at multi-ampere currents (dg-416) and pumping all vote; the regime table is the starting point, not the qualification.
-
Extracted current from a PIG source was proportional to arc current under the source's anode-extraction conditions, at roughly 10-100 (mA/cm^2) per ampere of arc; ion current density at the cathodes - and extractable density there - runs five to ten times the anode value. The arc supply is therefore the first knob for beam scaling, though extraction field, plasma meniscus and space charge set their own limits.
j_extracted ~ (10-100 mA/cm^2) per A of arc current; ion current density at cathodes is 5-10x that at anodeSource quote & editorial note
The ion current to the anode has about the same value as to the cathodes, which means that the ion current density at the cathodes is five to ten times the density at the anode surface, and, consequently, the extracted current densities show the same relation. The total extracted current of a PIG ion source is proportional to the arc current, and for extraction through the anode, about 10 to 100 (mA/cm2)/A.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82
Editorial note, tabletop extrapolation: With a ~1 mm^2 chimney slit, a 1-A arc offers ~0.1-1 mA of ideal aperture current - orders of magnitude above the reference machine's nA accelerated beams. That margin lives at the slit: capture, centering and transmission still take their share, so treat it as headroom, not proof the source can never be the bottleneck.
-
Cold-cathode PIG arcs are limited to about 1 kW per cathode by the onset of thermal electron emission (material- and design-dependent); titanium is the selected best-compromise cold-cathode material, tantalum if the cathodes run hot; a cathode is worn out when its sputter-erosion crater depth reaches about the anode bore radius, after which the discharge becomes unstable.
P_arc(cold) < ~1 kW per cathode; end of life: crater depth ~ anode bore radius; Ti best cold-cathode material, Ta if run hotSource quote & editorial note
The arc power for cold cathode operation is limited to about 1 kW per cathode, because of the start of thermal electron emission, and depends on the cathode material and the ion source design. ... Titanium has been selected as the best compromise. If the cathodes are allowed to run hot, tantalum has been shown to be a good choice. ... The cold and hot cathodes are worn out when the erosion crater's depth reaches around the anode bore radius. The discharge becomes unstable under these conditions.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 84-85
Editorial note, tabletop extrapolation: Gives a concrete inspection criterion: measure the cathode pit depth against the ANODE BORE radius (about half the bore diameter) each time the source is pulled, and machine spare cathode buttons in advance.
-
For long life use an indirectly heated block cathode: an auxiliary filament bombards the cathode's rear with ~1-kV electrons so cathode temperature is set independently of the arc, and the source reports the heated cathode's lifetime exceeding both cold and hot cathodes.
e-bombardment heating: 0-2 kV / 0-2.5 A onto cathode rear; filament itself 50-150 A at 2-8 VSource quote & editorial note
Electrons emitted from a filament and accelerated to about 1 kV heat the cathode from the rear side... The lifetime of the heated cathode exceeds that of cold or hot cathodes.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 86, 101
Editorial note, tabletop extrapolation: A next machine's source can hide a small filament behind a Ta-class block cathode, out of the hydrogen plasma - the filament stops being the consumable, and what erodes instead is the thick block face under PLASMA-ion sputtering (slow, by mass). The burn-down behavior, block material and electrical ratings are design choices to verify, not inherited guarantees.
-
Expect the open-filament arc to run 0.5-2 A at 100-500 V at ~1e-4 mm Hg; Wouters' procedure strikes it at 0.5-1 A and 100-200 V, with filament emission set to 10-20 mA at 200-300 V bias under high vacuum before admitting gas.
arc: 0.5-2 A @ 100-500 V @ ~1e-4 torr; emission set-point 10-20 mA @ 200-300 VSource quote & editorial note
at normal operating pressures of 10^-4 mm Hg, between 1/2 to 2 amps at 100 to 500 volts will be required
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 6, 10
Editorial note, tabletop extrapolation: A documented operating envelope for a simple hot-filament source at the reference machine's scale - a starting point whose actual values shift with geometry and field: commission against it, not to it.
-
Admit hydrogen so tank pressure rises by about 1e-4 mm above base while watching the arc current - the cited machine's commissioning procedure; the report's flow-control options include a needle valve, a thread-leak, and an electrically heated palladium leak.
delta-P(H2) ~ +1e-4 torr over base pressureSource quote & editorial note
hydrogen may be admitted to the tank, 'opening' the valve until the tank pressure rises by another 10^-4 mm, meanwhile watching the arc current
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 6, 10
Editorial note, tabletop extrapolation: Transfer the method, not the number: admit gas gradually while watching pressure and arc behavior, and find the reference machine's own setpoint with its calibrated gauge and pumping stack (its parker metering valve fills the needle-valve role). The 1e-4 mm rise is the source machine's figure - gauge species, gauge location and pumping speed make it non-portable.
-
Wouters suggests ~0.025-inch tungsten ('perhaps', his word) over fragile automobile-lamp filaments - a 0.025-in tungsten filament takes about 25 A DC - and floats the filament supply across a storage battery to filter the ripple that vibrates the filament.
0.025 in W filament ~ 25 A dc at a few voltsSource quote & editorial note
an automobile headlight filament has been used, but the breakage has been high ... perhaps .025 in. tungsten ... A .025 in. tungsten filament requires about 25 amps d.c.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 6-7
Editorial note, tabletop extrapolation: Filament sizing starts from emission demand and temperature, with Wouters' 0.025-in / 25 A as the documented anchor rather than a universal spec. The modern equivalent of the battery is a well-filtered DC filament supply - raw rectified current drives magnetically induced filament vibration in the cyclotron field.
-
Shield the ion-source filament from the dee's RF field with a small metal 'chimney' tube (1/4 in) and let the dee field extract ions through a small side hole facing the gap.
1/4 in chimney tube over filament, side extraction holeSource quote & editorial note
A quarter-inch tube called a 'chimney' sits on top of the filament, which shields it from the electric field of the dee. Ionized hydrogen is drawn out of a small hole.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 3
Editorial note, tabletop extrapolation: A worthwhile arrangement for a next machine: the chimney gives a defined source position and shields the filament from the dee field - the quote's stated purpose. Comparisons against a bare filament (loading, output) are the builder's to measure, not the source's claim.
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Beam current improved a factor of seven (10 -> 70 pA) at the same 1700 V / 26 W drive after moving to higher frequency (6.04 vs 3.55 MHz), an order of magnitude lower H2 partial pressure (2.2e-6 vs 1.5e-5 torr), lower base pressure, and a far smaller filament bias (-6 V vs -100 V) - a several-variables-at-once change, but one that cost no RF power at all.
6.04 MHz, 1700 V (26 W), H2 2.2e-6 torr, -6 V filament -> 70 pA; vs 3.55 MHz, 1700 Vpp (26 W), H2 1.5e-5 torr, -100 V -> 10 pASource quote & editorial note
3.55 MHz 1700 Vpp (26 W) H2 1.5 10-5 torr Total 4.0 10-5 torr -100 V filament ... 6.04 MHz 1700V (26 W) H2 2.2 10-6 torr Total 1.3 10-5 torr -6 V filament ... Higher frequency, lower H2 and base pressure, lower filament voltage
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 17-18
Editorial note, tabletop extrapolation: For the reference machine's current-hunting: before adding RF watts, cut chamber pressure and re-optimize filament bias - Houghton's gain cost zero watts - but change one variable at a time so you learn which knob actually paid.
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Kovalchick's IEC grid: inner-grid diameter chosen as one-fifth of the 21-cm chamber (4.2 cm), geometric transparency kept above the cited 92 percent threshold - three loops of 0.114-mm tungsten wire give 99.18 percent, calculated by comparing total wire cross-section to grid-sphere surface area.
d_grid ~ D_chamber/5; transparency = 1 - (pi*d_grid*N_loops*d_wire)/(4*pi*r^2) >= 0.92Source quote & editorial note
The grid was made of .0114 cm thick tungsten wire shaped into circles chosen to be one fifth of the chamber in size. The chamber diameter was 21 cm so the grid diameter was 4.2 cm. ... fusion efficiency is enhanced by transparency of at least 92 percent (Donovan). The inner grid is 99.18 percent transparent with three loops as calculated by comparing the cross section of the total grid wire used to the surface area of the grid sphere.
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 19-20
Editorial note, tabletop extrapolation: The transparency bookkeeping (wire cross-section vs aperture area) is the calculation method to transfer - but a circulating cyclotron beam hits a grid or slit repeatedly and directionally, so compute projected obstruction along the actual trajectory over many turns, not the spherical-area figure.
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In the cathode-grid circuit, the supply cannot tell an ion arriving from an electron leaving (both read as positive current), so grid supply current is not by itself an ion-current measurement; choose grid wire for high melting point, low sputter yield, and high work function to suppress parasitic thermionic emission where the grid runs hot.
I_supply = i_ion + i_electron; at a limited P_ext = V*I, emitted electrons spend budget that could go to ionsSource quote & editorial note
A power supply cannot differentiate between an ion reaching the cathode grid and an electron leaving it (they both appear as positive current on the ammeter).
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 135, 144
Editorial note, tabletop extrapolation: When metering beam current near a hot cathode, part of the reading can be electrons. High work function helps only against thermionic emission; a Faraday cup's secondary-electron escape needs its own fix - a suppressor electrode or magnetic suppression, validated on the actual geometry.
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Thermal limit of a wire electrode by radiation balance: I = A*eps*sigma*T_sag^4/V. The source works its 10-cm stainless grid example (A ~76 cm^2, eps ~0.15, sag at ~1500 K) to 9.5 mA at 200 kV against a 75 mA supply - but those printed inputs actually evaluate to ~327 W, i.e. ~1.6 mA at 200 kV, so the printed current does not follow from the printed inputs. Use the balance; recompute for your case.
I_max = A*eps*sigma*T_sag^4/V; the source's inputs (76 cm^2, eps 0.15, 1500 K) give ~327 W -> 1.64 mA at 200 kV, not the printed 9.5 mASource quote & editorial note
Assuming that sagging occurs at ~1,500 K and equating the black body radiation rate to the input power ... ~76 cm2 for a 10-cm grid made of 0.08 cm diameter with 5 latitudes and 12 longitudes ... the emissivity of the material (~0.15 for stainless) ... This gives 9.5 mA of ion current at 200 kV, whereas the power supply can produce 75 mA at 200 kV.
Editorial note, tabletop extrapolation: The same balance sizes any wire electrode, probe or beam stop in the reference machine's chamber - with its assumptions on the table: uniform temperature and radiation-only cooling. Compute A*eps*sigma*(T^4 - T_amb^4) against actual intercepted beam power, and check local hot spots and conduction separately.
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W-25%Re is the cited work's grid sweet spot: spot-weldable (unlike pure W), low sputter yield, high melting point (the book prints 2,800 K), validated at 30-130 kV and 30-180 mA for over 1,000 h - and the grid survived over 2 years where stainless wires lasted under a week.
W-25%Re: book's melting figure 2,800 K (standard alloy data put the W-25Re solidus near ~3300 K - verify against a datasheet); validated 30-130 kV, 30-180 mA, >1000 h; pure-W spot welding needs a Ni foil interlayer (the Ni then limits temperature)Source quote & editorial note
The stainless steel wires previously used by Murali lasted for under a week depending on the power load. In contrast, with the W-25%Re alloy, the grid lasted for over 2 years. ... It is relatively cheap, has a high melting point (2,800 K), a low sputter yield, and is easy to manufacture by spot welding. To test this material, the 10-cm grid was run at various voltages in the range of 30-130 kV and with the current range of 30-180 mA for over 1,000 h
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 145-146
Editorial note, tabletop extrapolation: W-Re thermocouple wire is commercially available in small quantities - a strong candidate for any sputtered electrode in the reference machine's source, with W-class durability and far better workability than pure tungsten; fabrication, activation and sputter behavior remain application-specific, so qualify it in place.
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DC glow discharges are organized by the pressure-distance product pd, not pressure alone; the glow regime runs ~300-1500 V at mA-level currents, and nearly the whole applied voltage drops in the few-mm cathode sheath.
breakdown V = f(p*d) (Paschen); glow: 300-1500 V, mA currents; cathode fall occupies first few mmSource quote & editorial note
The product of pressure and distance between the electrodes (pd) is a better parameter to characterize the discharge... The voltage is mostly in the range between 300 and 1500 V, but... the current is generally in the mA range.
Editorial note, tabletop extrapolation: When scaling chamber geometry or pressure for the p-B11 test cell, pd similarity is the right first knob - it organizes breakdown - but sustained-glow behavior also moves with gas, electrode material and area, and current density, so expect to re-tune rather than translate. Either way, sputter damage concentrates at the cathode sheath edge.
Cited in: The Vacuum Budget of a Cyclotron
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Know the V-I ladder of a low-pressure DC discharge -- background/saturation, Townsend dark discharge, corona at sharp points, breakdown, normal glow (V roughly constant over decades of current), abnormal glow, then glow-to-arc when the cathode overheats -- and note the hysteresis: the glow persists below its striking condition once lit.
sequence: dark -> Townsend -> breakdown -> normal glow (V ~ const) -> abnormal glow -> arc; hysteresis on the way back downSource quote & editorial note
A hysteresis effect occurs; wherein instead of retracing the path... the discharge maintains itself in the normal glow regime... at considerably lower currents... Only then does it make the transition back to the Townsend regime.
Editorial note, tabletop extrapolation: Explains the striking-vs-running asymmetry a source can show: ignition up on the breakdown branch, then sustaining down on the glow branch at much lower voltage - the Penning table's several-kV-ignite / sub-kV-run split (dg-372) is this physics - and why current-limited (ballasted) supplies are needed to stop glow-to-arc runaway. The actual voltages move with gas, pd and geometry.
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In a gridded low-pressure device, pressure controls ignition through the collision physics: the ion mean free path is ~7 cm at 2 mTorr and ~0.7 cm at 20 mTorr, and the striking voltage increases with decreasing pressure.
lambda_ion ~ 7 cm @ 2 mTorr, ~0.7 cm @ 20 mTorr (H2/D2); V_strike rises as p falls; operating window 2-15 mTorrSource quote & editorial note
The ion mean free path at 2 mTorr is ~7 cm, while at 20 mTorr it is around 0.7 cm... The striking voltage increases with decreasing pressure.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 92, 94
Editorial note, tabletop extrapolation: For any glow-driven ion supply in the p-B11 experiment, pressure is the ignition control: strike at higher pressure, then throttle the MFC to the running point - a device-specific procedure to commission, with the actual striking curve measured (Paschen-type behavior depends on pd, gas, geometry and surfaces, not the ion mfp alone).
Cited in: The Vacuum Budget of a Cyclotron
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A transparent wire cathode breaks down at about three times lower pd than a solid cathode at the same striking voltage (the cited comparison, spherical and planar alike) - recirculation through the grid is the working explanation; the Star-mode microchannel regime and transparency limits are the book's further account (scan re-read queued).
pd(solid)/pd(grid) ~ 3 at fixed V_strike; Star mode below ~0.5 Torr-cm; rigid grids practical only to ~95% geometric transparencySource quote & editorial note
For fixed Vs, the value of (pd) is seen to be about three times higher for both the spherical and the planar solid-cathode discharges than for the transparent grid-type cathode discharges.
Editorial note, tabletop extrapolation: If building an IEC-style p-B11 test stand, grid-opening geometry is a real trade study - larger openings mean fewer grid hits and longer grid life, finer mesh means better field definition - informed by the cited 3x pd result, with the Star-mode operating claims taken from the re-read source rather than summary memory.
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To ionize low-pressure gas for a beam-mode device, the source suggests it might be necessary to add a hot-filament electron emitter just outside the outer grid, biased slightly positive (~200 volts).
filament bias ~ +200 V, located outside outer gridSource quote & editorial note
it might be necessary to include a filament or other source of electrons to ionize the deuterium at low pressures. This filament should be placed just outside of the outer grid system and biased slightly positive (~200 volts)
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 7
Editorial note, tabletop extrapolation: Matches the reference machine's hydrogen filament philosophy: a modest bias on an emitter sustains ionization where a self-sustained discharge dies. Wire the POTENTIAL TOPOLOGY deliberately - what accelerates the electrons is the difference between emitter and the collecting electrode, so state the reference (the source does not say 'to ground') and set the electron energy against the ionization physics, not against the chamber wall by default.
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Guard the support structure of a negatively biased electrode so ions bombard only the intended electrode: the source's instruction is to electrically shield (insulate) the inner-grid support - in practice, recess the vacuum insulation behind a conductive shield at a controlled potential rather than leaving bare dielectric exposed to the plasma.
Source quote & editorial note
Care must be exercised to electrically shield (insulate) the inner grid metallic support structure so that ions will not bombard that portion of the apparatus.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 7
Editorial note, tabletop extrapolation: Same rule protects the reference machine's Faraday cup stalk and source supports: unshielded biased metal collects spurious current and sputters - and bare insulation over it charges up and distorts fields, so shield with guarded conductor, then insulate behind it.
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On the Houghton machine, filament bias (tested around -90 V) appeared to have no effect on beam current over the tested range.
beam current insensitive to filament bias (tests near -90 V)Source quote & editorial note
It appears that filament bias has no effect on the beam current.
Editorial note, tabletop extrapolation: Tuning-order advice, not physics: hold filament bias fixed during initial tuning and spend the effort on dee voltage and pressure - but scan bias if ionization or emission looks current-limiting, since other geometries and regimes do respond to it.
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With an internal fill-gas ion source there is an optimal chamber pressure band - too little gas starves ionization, too much and the ions scatter on gas inside the dee and fall out of resonance; the Houghton machine ran about 1e-5 to 3e-5 Torr.
Houghton's band ~1-3e-5 Torr; their highest raw current appeared near ~1e-4 Torr but with badly broadened resonances - raw current at high pressure is not useful resonant beamSource quote & editorial note
If there is too little gas, less ionization will occur... Too high a pressure and the ionized particles will likely interact with gas inside the dee and fall out of resonance.
Editorial note, tabletop extrapolation: Map current vs pressure on your own machine, recording resonance width and source stability along with current - expect an apparatus-dependent optimum and a non-monotonic curve, and use Houghton's window as calibration context, not a target.
Cited in: The Vacuum Budget of a Cyclotron
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Add deliberate clearance between the filament and the chamber lid - Houghton milled a 0.3 cm deep circular depression into the lid specifically to prevent a repeat filament-to-lid discharge.
0.3 cm milled recessSource quote & editorial note
To make room for a filament and to avoid another electrical discharge from the filament to the lid, a 0.3 cm deep circular depression was milled out of the bottom of the upper lid.
Editorial note, tabletop extrapolation: In the reference machine's tight pole-gap geometry, check every HV-to-ground clearance near the median plane; milling relief pockets is cheaper than chasing sparks later.
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Run the chamber in the source's stated window, 1e-6 to 1e-4 Torr: below it there is too little gas to ionize; above it neutral collisions shorten the ion mean free path and the resonance peaks become broad and shift; the largest recorded beam current was about 0.1 uA.
operating window 1e-6 to 1e-4 Torr (cited machine); best recorded current ~0.1 uASource quote & editorial note
The pressure in the chamber has a large effect on the beam current obtained, and typically needs to be in the range from 1e-6 to 1e-4 Torr for the cyclotron to operate. ... [higher pressures] reduce the mean free path of the ions, and cause the resonance peaks to become broad and shift. The largest beam current recorded, shown in Figure 6, was about 0.1 uA
Editorial note, tabletop extrapolation: Directly sets the gas-handling operating window for the reference machine and explains a common 'no beam' failure at too-good vacuum - throttle up before concluding the source is dead.
Cited in: The Vacuum Budget of a Cyclotron
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Support and connect a floating PIG anode with two 0.5 mm stainless wires fed through alumina tubes sealed with ceramic epoxy (Ceramabond) into the cathode body; a third stainless tube serves as gas inlet.
Source quote & editorial note
Three holes are machined in the cathode body; two are used to support the anode and the third is used as a gas inlet. Alumina tubes are inserted into the two holes used for anode support, and a stainless steel tube is inserted into the gas inlet hole. Ceramic epoxy (Ceramabond) is used to mate the alumina and stainless tubes to the back of the cathode body. Stainless steel wire with 0.5 mm diameter was spot welded to the anode, and the wires were threaded through the alumina tubes in the cathode body. ... Essentially the anode floats inside the cathode body, being supported only by the two stainless steel wires that protrude through the alumina tubes and out the back of the cathode body.
Editorial note, tabletop extrapolation: An amateur-grade insulated support for a modest-voltage, low-current internal electrode - an ion-source anode and the like. Not unchanged for filament leads (0.5 mm stainless is a poor conductor for filament current) or for chamber-wall HV or current feedthroughs: use current-rated conductors and qualified vacuum/HV feedthroughs there, and test the ceramic-epoxy joint for bakeout, leakage and voltage standoff before trusting it. [Note revised 2026-08-23: earlier note extended the scheme to filament leads.]
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A cold-cathode PIG the paper builds from an iron cathode body, a ~3 kG SmCo permanent magnet, a folded 0.13 mm stainless-sheet anode and an iron faceplate with a 6.4 mm axial aperture delivered a continuous 1 mA beam of positive hydrogen ions at 1 mTorr, on 5.4 kV and 32.4 W.
3 kG SmCo; 5.1 cm iron cathode body; 6.4 mm faceplate hole; 1 mA H+ at 1 mTorr, 5.4 kV, 32.4 WSource quote & editorial note
generate a plasma discharge that yields a continuous 1 mA beam of positively charged hydrogen ions at 1 mTorr of pressure. This operating condition requires 5.4 kV and 32.4 W
Editorial note, tabletop extrapolation: A directly copyable permanent-magnet source recipe at hobby machining tolerances - copy from the paper's drawings, and treat the output as mixed hydrogen species (H+, H2+, H3+) until a bend or velocity filter resolves it (dg-001).
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Current-limit a PIG discharge with a series resistor (here 100 kOhm, 100 W) and always report/log the actual anode-to-cathode voltage, not the power-supply setpoint, since the resistor drops significant voltage during operation.
V_source = V_supply - I_discharge * R_ballast; R = 100 kOhm, 100 WSource quote & editorial note
The ion source anode is powered by a 6 kV 200 mA Hipotronics dc power supply and a 100 kOhm, 100 W resistor is connected in-line with the power supply to current limit the discharge. ... Because the 100 kOhm current-limiting resistor develops a voltage drop during source operation, the ion source voltage (anode-to-cathode voltage) is reported instead of the power supply voltage.
Editorial note, tabletop extrapolation: Directly applicable to the reference machine's DISCHARGE/ARC supply metering (the ballast correction belongs to the electrode circuit, not the filament heater): logging supply volts instead of electrode volts corrupts any operating-point map. Check ballast power, working-voltage and transient ratings for the actual supply.
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In the cited compact source-in-chamber setup the pressure inside the ion source was only about 2x the chamber pressure, and source operation was also achieved by simply backfilling the chamber.
P_internal ~ 2 x P_chamber (small chamber, direct injection)Source quote & editorial note
the pressure internal to the ion source is only approximately a factor of 2 larger than the chamber pressure... source operation has also been achieved by simply backfilling the chamber.
Editorial note, tabletop extrapolation: Worth testing on the reference machine: in a small chamber the injection-vs-backfill distinction may shrink - but the source-to-chamber pressure ratio is set by aperture conductance, flow and pump placement, so measure it (or model the conductances) rather than assuming 2x transfers.
Cited in: The Vacuum Budget of a Cyclotron
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A PIG discharge ignites easily at 1 kV or less and delivers continuous positive hydrogen-ion current: at 1 mTorr H2, 580 V gave 0.3 mA discharge / 20.8 uA target, rising to 6.0 mA / 1.5 mA at 5.4 kV.
H2, 1 mTorr: 580 V -> 0.3 mA discharge / 20.8 uA target; 5.4 kV -> 6.0 mA / 1.5 mA (positive hydrogen ions; species mix unanalyzed)Source quote & editorial note
the plasma discharge ignites easily at 1 kV or less for all cases and produces a continuous positively charged ion beam. ... For the 1 mTorr case, at 580 V, the discharge current and target current are 0.3 mA and 20.8 uA, respectively. As the ion source voltage increases to 5.4 kV, the discharge current and target current increase to 6.0 and 1.5 mA, respectively.
Editorial note, tabletop extrapolation: Tens of microamps of positive hydrogen ions at under 1 kV anode drive is ample raw current next to the reference machine's nA-scale accelerated beams - but it is aggregate H+/H2+/H3+ at the target: species fraction and RF capture are separate measurements before any of it is credited as proton beam.
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At its design operating point this PIG source collected 25% of the discharge current on the target (21% for helium) for 32.4 W of source power; beam is scaled by raising pressure or discharge voltage, both of which raise discharge current.
I_target/I_discharge ~ 0.25 (H2), 0.21 (He); 1.5 mA target at 6.0 mA discharge, 5.4 kVSource quote & editorial note
the source has a current utilization efficiency (ratio of target to discharge current) of 25% and requires 32.4 W of power.
Editorial note, tabletop extrapolation: A test-stand collection ratio, not a cyclotron benchmark: the reference machine's beam-to-arc ratio folds RF capture, centering and transmission on top of extraction, so a much lower ratio there does not by itself convict the extraction geometry. Use 25% as the source-side sanity scale only.
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For DC post-acceleration on the source's test stand: a suppressor electrode 2.5 cm downstream of the cathode faceplate and a target 7.6 cm beyond it, both biased negative with respect to the grounded source cathode; a continuous 1 mA positive hydrogen-ion beam was focused onto the target at 0.4 mTorr and 10.5 W, with acceleration voltages up to -30 kV investigated.
suppressor at 2.5 cm, target +7.6 cm, both negative w.r.t. grounded cathode; 1 mA positive hydrogen ions at 0.4 mTorr, 10.5 W; up to -30 kV investigatedSource quote & editorial note
The electrode closest to the source was the suppressor and was located 2.5 cm from the cathode faceplate. A target electrode was placed 7.6 cm from the suppressor. During high-voltage operation, the suppressor and target were biased negative with respect to the ion source cathode (i.e., ground). ... at a pressure of 0.4 mTorr and 10.5 W PIG source power, a continuous 1 mA positive hydrogen ion beam has been focused onto the target and accelerator voltages up to -30 kV have been investigated.
Editorial note, tabletop extrapolation: Template for a bench extraction test stand to characterize the next machine's source before it goes into the magnet.
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An internal cold-cathode PIG source is a low-maintenance choice: the Rutgers source runs more than 40 hours between servicings.
>40 h service intervalSource quote & editorial note
The ion source is an internal cold cathode Penning Ion Gauge (PIG) source that operates in excess of 40 hours before requiring service.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: Benchmarks source maintenance for a next machine: one documented internal cold-cathode PIG ran 40+ hours between servicings. Filament sources trade shorter cathode life for simpler supplies (dg-704's census practice) - lifetimes vary with design and duty on both sides of that trade.
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Separate the source's gas-fed discharge region from the main vacuum with a tight-fitting boron nitride insulator (isolating an on-the-order-1e-5 Torr region); Forringer's test stand held the main chamber near 4e-5 Torr at 2.5 cc/min H2 against a base pressure of 8e-7 Torr.
2.5 sccm H2 -> 4e-5 Torr chamber (base 8e-7 Torr); BN insulator isolates ~1e-5 Torr regionSource quote & editorial note
The boron-nitride insulator, which is a tight fit, separates the high vacuum region behind the insulator (on the order of 10-5 Torr), from the lower vacuum region in the chimney and between the anodes and cathodes. ... The best vacuum achieved in the ion source test stand (with source gas supply turned off) was 8 x 10-7 Torr. With a gas flow rate of 2.5 cc/min of hydrogen, the pressure in the main vacuum chamber is around 4e-5 Torr.
Editorial note, tabletop extrapolation: A single calibration point (about 1.6e-5 Torr per cc/min at that stand's pumping speed), not a slope: characterize the reference machine's own MFC-vs-chamber-pressure curve with its calibrated flow and gauges before reading deviations as leaks or conductance faults.
Cited in: The Vacuum Budget of a Cyclotron
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Forringer's cold-cathode PIG ran from a ~3 kV current-limited supply - after striking, arc voltage drops to whatever sustains the set current - and the 1.9-3.8 mm cathode-anode gap was 'not a critical parameter for the source's operation'.
strike supply 3 kV / 1 A current-limited; running arc voltage < 3 kV; gap 0.075-0.150 in non-criticalSource quote & editorial note
The cathode anode gap was between 0.075 (1.9 mm) and 0.150 (3.8 mm), and is not a critical parameter for the source's operation.
Editorial note, tabletop extrapolation: Relaxes the machining tolerance on a next machine's source gap and anchors the supply class: a ~3 kV current-limited unit ran this source. Strike voltage moves with pressure, gas, field and surface condition, so provide voltage headroom (or an ignition boost) rather than assuming the same number transfers.
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Water-cool the cathode rod and anode base of an internal PIG - copper parts melted when the source was run without cooling - and prepare cathode faces by sanding with 100-grit paper to a uniformly rough surface for reliable arc striking.
Source quote & editorial note
Water cooling for the cathode rod and the anode base are essential (some copper parts were melted when the ion source was run without proper cooling).
Editorial note, tabletop extrapolation: The source's warning stands as written: they melted copper running without cooling. A reference-machine-class source at much lower arc power may not need water - but that is a claim to establish by thermal estimate and a supervised first run with temperature monitoring, not by assumption. The sanded-cathode arc-striking preparation transfers directly.
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For calibration, hot-filament internal sources have run far above tabletop scale: Livingston and Jones heated a U-shaped tantalum filament with ~400 A, ran 2-6 A of arc, and extracted 150 mA through a 129 mm2 slit with a 12 kV puller across a 3.3 mm gap.
Ta filament ~400 A heater; arc 2-6 A; 150 mA extracted at 12 kV, 3.3 mm source-puller gap, 129 mm2 slitSource quote & editorial note
Their cathode was a U-shaped tantalum filament, heated with about 400 amps ... the arc current (the total current measured between the anode and cathode of the ion source) was between 2 and 6 amps. As seen in figure 1.2 a 0.2 in2 (129 mm2) area vertical slit provided the path for ions to exit the source. With this source Livingston and Jones were able to extract 150 mA using a puller voltage of 12kV and a source-puller gap of about 0.13 (3.3 mm).
Editorial note, tabletop extrapolation: Brackets the design space above the reference machine's filament source as an existence proof, not a scaling law: determine the arc a nA beam actually needs by measuring extracted and captured current against arc current on the real geometry.
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In Forringer's tested source, doubling the chimney slit from 0.25 mm to 0.51 mm (both 5.0 mm tall, 10 degree chamfer) raised beam current ~4.4x (52 to 230 uA at 50 mA arc) while radial emittance grew only ~1.7x (27 to 47 mm-mrad) - the larger slit gives more current at larger emittance.
0.010 in slit: 52 uA, 27 mm-mrad radial; 0.020 in slit: 230 uA, 47 mm-mrad (50 mA arc, 3.0 sccm, ~40 kV puller)Source quote & editorial note
The chimney with the larger slit produces a beam with a larger emittance. However, the beam is also of higher intensity.
Editorial note, tabletop extrapolation: Suggests slit width is a powerful knob worth sweeping on a next machine: expect more current and more emittance from a wider slit, and stop widening when the machine acceptance is filled - but the 4.4x/1.7x ratios are that source's numbers; do your own aperture sweep and acceptance analysis before extrapolating.
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A DC extraction test stand characterizes an internal source before installation: a puller with 12.7 mm radius of curvature held 50 kV across a 5.0 mm minimum source-puller gap on that stand, and a 2.9 mm gap held about 25 kV.
R_puller = 12.7 mm: gap 5.0 mm -> 50 kV; gap 2.9 mm -> ~25 kV (that stand's measured holdoff)Source quote & editorial note
This puller was designed for the ion source test stand to hold 50 kV... The minimum source to puller gap is 0.196 (5.0 mm).
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 68, 75
Editorial note, tabletop extrapolation: Two measured holdoff points from one clean DC stand - anchors for a dee-tip/puller voltage budget, not a kV-per-mm allowable: vacuum holdoff is nonlinear in gap and hostage to finish, conditioning, and RF-vs-DC differences. Do what the source did: measure the actual geometry on a test stand rather than applying a scaling law.
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In the tested chimneys, prefer the slit over the hole for beam quality: the slit gave a flat plasma boundary and converging beam, while the hole (1.19 mm, 60-degree chamfer) gave a concave boundary, a diverging beam, ~50% larger normalized radial emittance, and half the luminosity at equal arc current.
hole chimney: 0.66 mm-mrad normalized radial vs 0.44 for slit; normalized luminosity 129 vs 264 A/(mm^2-sr) at 50 mA arcSource quote & editorial note
an approximately flat plasma boundary provides the best match to the experimental beams emerging from the 'slit' style chimneys... while a concave plasma boundary... for the 'hole' style chimney ... The size of the hole in the chimney is 0.047 (1.19 mm) with a sixty degree chamfer. At 50 mA of arc current, the normalized luminosity of the beam which made it to the wire probe was 129 A/(mm2-sr), about half of that for the slit chimney with the same arc current (264 A/(mm2-sr)).
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 73-76, 91-107
Editorial note, tabletop extrapolation: Decides a next machine's chimney aperture style within the tested regime: cut a tall narrow slit rather than drilling a hole if beam brightness and predictable optics matter - and re-verify on the actual source, since the ranking comes from these apertures and operating points.
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Raising PIG arc current raised beam current sub-linearly in the cited scan: for the 0.25 mm slit, 50 to 450 mA of arc gave 52 to 227 uA of beam while beam/arc efficiency fell from 1.0e-3 to 0.5e-3; measured emittance stayed flat over the scan and luminosity climbed 1.7 to 7.1 A/(cm2-sr).
I_beam/I_arc drops 1.0e-3 -> 0.5e-3 over 50-450 mA arc; luminosity 1.7 -> 7.1 A/cm2-sr; emittance ~constantSource quote & editorial note
the general trend of increasing arc current producing increased beam current as expected... there was no noticeable change in the emittance of the beam for different currents
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 77-78, 81
Editorial note, tabletop extrapolation: Cranking arc power buys current with diminishing returns, and in this scan it did not spoil measured emittance. Do not read that as space charge being negligible in general: generalized perveance rises steeply at low velocity, so keep space charge in extraction and first-turn models until a sensitivity check shows it is negligible at your energy and current.
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Keep hydrogen flow comfortably above the arc-mode transition: at this source's normal flows (2-6 sccm, arc 50-350 mA, arc voltage under 3 kV current-limited) no H2+ was observed in the beam, while at 0.5 sccm the arc jumped to voltage-limited mode and molecular ions appeared.
flow > 2.0 sccm -> no detectable H2+ (this source); 0.5 sccm -> mode shift (3.5 kV limit, arc drops to 90 mA) with H2+ observedSource quote & editorial note
hydrogen gas flow rates greater than 2.0 cc/min) no H2+ ions were observed. We were able to observe H2+ ions by lowering the gas supply to 0.5 cc/min.
Editorial note, tabletop extrapolation: Directly actionable on the reference machine's MFC: starving the source of gas silently changes beam species, so locate the actual arc-mode transition for the machine and keep the setpoint above it - and remember 'no H2+ detected' is not 'pure protons': H3+ and below-detection species need their own check.
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Forringer's orbit simulations reproduced measured emittance for both slit and hole chimneys by starting ions on the plasma boundary with an effective plasma temperature of ~35,000 K (central starting energy ~4.5 eV, i.e. 3kT/2).
T_plasma ~ 35,000 K fitted; E_start ~ 4.5 eV = 3kT/2 at that temperature; flat boundary (slit) / concave boundary (hole)Source quote & editorial note
the plasma temperature that provides the best match for experimental beams is approximately 35,000 K (resulting in a central starting energy of 4.5 eV).
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 91-107
Editorial note, tabletop extrapolation: A starting calibration for any first-turn simulation of a next machine's central region: begin near 35,000 K / 4.5 eV, then sweep the initial temperature and meniscus shape and validate against measured emittance or beam profiles - the value is a fitted effective parameter, not a universal plasma property.
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Use a fine-taper metering valve with a vernier handle for gas admission - Series 20: Cv 0.029, 3-degree stem taper, 9 +/-1 turns to open - so flow settings are repeatable (datasheet's 0.055-in orifice and Series 30 figures sighted at extraction; table re-read queued).
Series 20: Cv=0.029, orifice 0.055 in, taper 3 deg, 9+/-1 turns; Series 30: Cv=0.16, orifice 0.125 in, taper 9 deg, 10+/-1 turnsSource quote & editorial note
Vernier knob for repeatable flow settings ... Flow Coefficient (Cv): 0.029 (Series 20) ... Stem Taper: 3 deg ... Turns to Open: 9 (+/-1)
Parker Hannifin, Series 20 & 30 Metering Valves (datasheet) — p. 1-2
Editorial note, tabletop extrapolation: The 3-degree taper spread over 9 turns gives the fine, repeatable hydrogen admission an ion source needs. Log turns-open as the VALVE-POSITION setpoint - repeatable flow additionally needs regulated upstream pressure and a calibration of flow (or chamber pressure) against turns under operating conditions; the vernier repeats position, not sccm.
-
Never use a non-shutoff metering valve as the shut-off: Parker's sheet says the cited series is 'not recommended for positive shut-off' and points to its Series HR metering valve where bubble-tight shut-off is required; the cited series is also pressure-limited (1000 psig upstream, 500 downstream).
max 1000 psig operating (downstream limited to 500 psig); elastomer limits: Buna-N -10 to 250 FSource quote & editorial note
Not recommended for positive shut-off. If bubble-tight shut-off required, the use of a Series HR Metering Valve is suggested.
Parker Hannifin, Series 20 & 30 Metering Valves (datasheet) — p. 2
Editorial note, tabletop extrapolation: Practical form for the gas panel: give the metering valve an isolation valve between it and the bottle - or specify a metering valve designed for shut-off duty, the HR-class option the sheet names. Forcing a plain tapered stem closed to seal ruins the calibrated taper and still leaks into the vacuum system.
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Run the hot-cathode source arc chamber in graphite (86-inch: 0.563-in OD graphite tube), feed 2-3 cc/min of hydrogen, and expect arc conditions of 0.5-1.5 A at 100-300 V with a 0.062 x 2.5 inch exit slit.
H2 flow 2-3 cc/min; arc 0.5-1.5 A @ 100-300 V; slit 0.062 in x 2.5 inSource quote & editorial note
The rate of flow required during operation is from 2 to 3 cc/min ... Electrons are accelerated from the filament into the arc chamber by a 100 to 300 volt potential, the normal arc current being 0.5 to 1.5 amperes.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 62, 64
Editorial note, tabletop extrapolation: Documented arc conditions for a hot-cathode chimney source. Scaling to a much smaller chimney shifts gas flow and arc balance with geometry and pumping, so treat 0.5-1.5 A / 100-300 V / a few cc/min as the class of numbers to expect and tune on the machine. The robust transfer is the material lesson: graphite chimney and slit parts resist sputtering far better than copper or steel.
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Treat alignment of the ion source with the magnetic field and the accelerating slits as the critical tune - the quote; the report's specific geometry (filament fully covering the defining slot, slot edge tangent to the arc-slit plane) is its own practice (scan re-read queued).
Source quote & editorial note
The alignment of the ion source with the magnetic field and with the accelerating slits is critical and is carefully adjusted to obtain best performance.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 64
Editorial note, tabletop extrapolation: Directly applicable: build a next machine's source mount with repeatable rotation/translation adjustment from outside vacuum; source-to-puller alignment is worth more beam than any power knob.
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Regulate arc voltage and arc current independently, as the ORNL source did: hold arc voltage constant via the arc supply and hold arc current constant by trimming filament heating.
loop 1: V_arc = const (arc supply); loop 2: I_arc = const (filament temperature)Source quote & editorial note
Arc voltage and arc current can each be varied independently ... This regulates the filament temperature and thus the arc current, which is then held constant regardless of arc voltage.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 66
Editorial note, tabletop extrapolation: A control philosophy readily implemented with two small feedback supplies; a constant-current arc removes one major drift term from shot-to-shot beam current - stable gas flow and extraction conditions are still needed for real reproducibility.
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Machine face-seal grooves for vacuum to the Parker chart: for a 1/8-in (0.139) cross-section ring, gland depth 0.101-0.107, squeeze 20-30%, vacuum groove width 0.158-0.164, groove radius 0.010-0.025; the chart's other rows (0.210, 0.275 sections) carry their own dimensions - read the row for the ring in hand.
W=.139+/-.004: L=.101-.107, squeeze .028-.042 (20-30%), G(vacuum)=.158-.164, R=.010-.025; W=.210: L=.152-.162, G=.239-.244; W=.275: L=.201-.211, G=.309-.314Source quote & editorial note
201 through 284 / 1/8 / .139 +/-.004 / .101 to .107 / .028 to .042 / 20 to 30 / .177 to .187 / .158 to .164 / .010 to .025
Parker Hannifin, O-Ring Handbook — Design Chart 4-3: O-Ring Face Seal Glands — p. 1
Editorial note, tabletop extrapolation: Hands the mill the numbers for the chamber's lids and ports - per ring size and per geometry: these are STATIC AXIAL FACE seals; a port using a different cross-section or seal configuration gets its own chart row or chart. Note the vacuum groove width column is narrower than liquid service.
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Finish O-ring sealing faces per the chart: 16 RMS for vacuum and gas service, 32 RMS for liquids (the sidewall finish, taper and corner-break values are the chart's further annotations - re-read queued).
sealing face 16 RMS (vacuum/gas), 32 RMS (liquid); groove walls 63 RMS; sidewall taper 0-5 deg; break corners approx .005 radSource quote & editorial note
Surface finish X: 32 for liquids, 16 for vacuum and gases. Finishes are RMS values.
Parker Hannifin, O-Ring Handbook — Design Chart 4-3: O-Ring Face Seal Glands — p. 1
Editorial note, tabletop extrapolation: Specify and check the chamber lid seat to 16 RMS (fly-cut or turned); a rough or cross-scratched sealing face can contribute to leakage and belongs on the leak-diagnosis checklist - as one suspect among several, not a signature of any particular pressure plateau.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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Locate a face-seal groove by the diameter the pressure pushes the ring toward: for internal (outward) pressure dimension groove OD = mean O-ring OD; for external pressure (vacuum chambers) dimension groove ID = mean O-ring ID, tolerance +1% of ID but not more than +0.060.
external pressure (vacuum): H_i = mean O-ring ID, tol +1% ID (max +0.060); internal pressure: H_o = mean O-ring OD, tol -1% OD (max -0.060)Source quote & editorial note
For Internal Pressure (outward pressure direction) dimension the groove by its outside diameter (HO) and width: (HO) = Mean O.D. of O-ring ... Tolerance = Minus 1% of Mean O.D., but not more than -.060 ... For External Pressure (inward pressure direction) dimension the groove by its inside diameter (Hi) and width: (H)i = Mean I.D. of O-ring ... Tolerance = Plus 1% of Mean I.D., but not more than +.060
Parker Hannifin, O-Ring Handbook — Design Chart 4-3: O-Ring Face Seal Glands — p. 1
Editorial note, tabletop extrapolation: For an evacuated chamber atmospheric pressure pushes the ring inward, so the groove ID (not OD) is the controlled dimension when laying out the lid groove.
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Provide pumping speed of at least 1 liter/sec (at 1e-5 mm Hg) per liter of chamber volume, and size the roughing pump to reach diffusion-pump backing pressure in 15-20 minutes.
S >= 1 (l/s)/liter of volume at 1e-5 torr; roughing time to backing pressure 15-20 minSource quote & editorial note
A good rule of thumb is to provide a pumping speed of at least 1 liter/sec at 10-5 mm Hg per liter of volume ... 15 to 20 min is considered a good design figure.
Livingston & Blewett, Particle Accelerators (1962) — p. 197-198
Editorial note, tabletop extrapolation: For a ~30-50 liter tabletop chamber the rule asks for 30-50 l/s DELIVERED at the chamber; the SI100's 100+ l/s class inlet rating leaves margin that the plumbing then spends - baffle, elbows and port conductance cut delivered speed (1/S_eff = 1/S + 1/C, dg-906) - so compute the delivered figure before crediting the margin. On a gas-fed machine the source load dominates either way.
Cited in: The Vacuum Budget of a Cyclotron
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Use a double-gasket seal with a pump-out connection between gaskets on large or troublesome flanges: the interspace lets you test the seal for tightness quickly and with certainty, and - when designed as a continuously pumped guard vacuum - intercepts outer-seal leakage before it reaches the chamber.
Source quote & editorial note
A double-gasket seal is frequently used with a pump-out connection to the space between gaskets. This arrangement makes it possible to test the seal for vacuum-tightness quickly and with certainty.
Livingston & Blewett, Particle Accelerators (1962) — p. 200
Editorial note, tabletop extrapolation: Worth adopting on a next machine's main lid: a guard-vacuum groove turns the worst leak hunt into a valve twist for TESTING; riding out a leak in service additionally needs the interspace continuously pumped with adequate speed, and only helps for leaks through the outer seal.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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For static vacuum seals the source recommends dovetail or face grooves with vacuum grease AND a heavy squeeze: in its butyl face-seal test, raising squeeze through 15%, 30% and 50% cut the helium leak rate dramatically, and the grease's benefit shrank as squeeze rose - undetectable at 50%.
squeeze 15% -> 30% -> 50% gives steeply decreasing He leak rate; grease benefit large at 15%, small at 30%, undetectable at 50%Source quote & editorial note
One butyl compound has been tested in face-type O-ring seals, using grooves that provide 15%, 30%, and 50% squeeze. It will be seen from the results plotted in Figure I that increasing the squeeze reduced the leak rate dramatically... at 50% squeeze the beneficial effect of the grease was not detectable. ... It is therefore recommended that dovetail or face type O-ring grooves be used whenever possible for static vacuum seals, employing a suitable vacuum grease as a sealing lubricant and surface coating in addition to a heavy squeeze on the O-ring.
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 3-4
Editorial note, tabletop extrapolation: Cut a next machine's grooves toward the heavy end per the source's recommendation, but set the nominal from the ring manufacturer's static-vacuum gland tables under worst-case tolerances - 50% was a test point, not a design target; gland fill, compression set and assembly damage cap real designs. Grease is a crutch for light squeeze.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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Estimate O-ring permeation leak rate with the source's mixed-unit formula L = 0.7*F*D*P*Q*(1-S)^2 - L in std cc/s, F the elastomer's permeability in std cc-cm/(cm^2 s bar), D ring ID in inches, P differential in psi, Q the squeeze/lubrication factor from the source's Figure II (~1.35 read off the dry-ring curve at 20 percent squeeze), S fractional squeeze - a rough order-of-magnitude approximation by the source's own statement.
L(std cc/s) = 0.7 F D P Q (1-S)^2; F in std cc-cm/(cm^2 s bar), D in inches, P in psiSource quote & editorial note
L = .7FDPQ(1-S)2 where: L = Approximate leak rate of the seal, std. cc/sec. F = Permeability rate of the gas through the elastomer at the anticipated operating temperature. Std cc cm/cm2 sec bar ... D = Inside diameter of the O-ring, inches. P = Pressure differential across the seal, lb/in2. Q = Factor depending on the percent squeeze and whether the O-ring is lubricated or dry. (From Figure II) S = Percent squeeze on the O-ring cross section expressed as a decimal. ... This formula provides only a rough order of magnitude approximation ... For convenience, the formula contains mixed units. ... The .7 factor provides dimensional homogeneity.
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 5
Editorial note, tabletop extrapolation: Computes the permeation floor of the 10-inch Viton lid seal - then convert to pressure via P = Q_gas/S_eff with the actual effective pumping speed, and remember outgassing and real leaks usually dominate above the permeation floor.
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Avoid tool marks perpendicular to the O-ring sealing line; the ideal vacuum-flange finish has a circular lay (concentric with the ring), since a radial scratch is a built-in leak path.
Source quote & editorial note
care being taken to insure that there are no machine or tool marks perpendicular to the seal... The ideal surface finish for any vacuum seal flange has a circular lay
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 5
Editorial note, tabletop extrapolation: Face the lid seat on a lathe (concentric lay) rather than fly-cutting or hand-sanding radially; never sand a groove crosswise to remove a blemish.
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Vacuum weight loss at ~1e-6 Torr (the chart's gravimetric test): butyl 0.18%, neoprene 0.13%, fluorocarbon 0.07%, against nitrile at 1.06-3.45% - an order of magnitude between the good and bad compounds.
% weight loss, 336 h @ ~1e-6 Torr, 21 C: butyl 0.18, neoprene 0.13, fluorocarbon 0.07-0.09, silicone 0.03-0.31, EPDM 0.39-0.92, nitrile 1.06-3.45, polyurethane 1.29Source quote & editorial note
Vacuum Level: Approximately 1 x 10-6 torr ... Butyl .18 ... Nitrile 1.06 ... Nitrile 3.45 ... Fluorocarbon .07
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 6
Editorial note, tabletop extrapolation: At exactly the reference machine's operating pressure, nitrile's high weight loss marks it a potential outgassing concern near feedthrough insulators, optics and RF surfaces - where the lost mass actually lands was not measured, so treat the ranking as a screening result and prefer the low-loss compounds (Viton's 0.1%-class loss is the cheap insurance) rather than claiming proven film deposition.
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Pick low-permeability elastomers for vacuum by the helium table (77 F, x1e-8 std cc-cm/cm2-s-bar): butyl and neoprene 6.5, nitrile 8.0, fluorocarbon 12.7, EPDM 19.7, fluorosilicone 143, silicone 238 - a ~37x spread from best to worst.
He permeability x1e-8 std cc-cm/cm2-s-bar @77F: butyl 6.5, neoprene 6.5, nitrile 8.0, fluorocarbon 12.7, EPDM 19.7, fluorosilicone 143, silicone 238Source quote & editorial note
Butyl 6.5 @ 77F ... Fluorocarbon 12.7 @ 77F ... Silicone 238.0 @ 77F
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 7
Editorial note, tabletop extrapolation: Viton's placement plus its other properties is why it is the default; silicone's high permeability matters most when helium leak checking (He walks through silicone and fluorosilicone seals, confusing the sniffer) and in permeation-limited systems - compute the actual permeation gas load for the seal geometry before ruling a compound in or out, since at 1e-6 Torr with decent pumping the load is often ignorable either way.
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Make alpha spectroscopy measurements with source-to-detector spacing of 1.5-2 times the detector diameter and vacuum better than 100 microns Hg (13.3 Pa; the datasheet's '10 Pa' is a rounded, slightly stricter figure).
spacing = 1.5-2 x detector dia; P < 100 um Hg = 13.3 Pa (10 Pa as conservative target)Source quote & editorial note
Alpha resolution measurements should be made with a detector source spacing equal to 1.5 to 2 times the detector diameter and under good vacuum (< 100 microns HG or 10 Pa).
Canberra, PIPS Detector Instruction Sheet (2012) — p. 1
Editorial note, tabletop extrapolation: For his ~8 mm active-diameter PIPS, that is 12-16 mm standoff; closer spacing degrades resolution through wide-angle entrance-window losses.
Cited in: Experiments by Energy Band
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Never exceed a diffusion pump's critical forepressure (25-75 Pa, i.e. 0.2-0.6 Torr, design-dependent); above it the jets collapse and inlet pressure rises uncontrollably, and at maximum throughput the tolerable forepressure drops to ~3/4 of its normal value.
critical forepressure 25-75 Pa; at max throughput reduce limit to ~0.75x; boiler pressure ~200 PaSource quote & editorial note
This maximum value called the 'critical forepressure,' ranges from 25-75 Pa (0.2-0.6 Torr)... The critical forepressure should never be exceeded.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 232-233
Editorial note, tabletop extrapolation: Size and maintain the backing pump so the foreline stays well under the pump's critical forepressure during beam-gas loads - for the SI100, take the manufacturer's figure; the quoted 0.2-0.6 Torr is the generic design range. A tired rotary pump silently pushes the foreline over the cliff and dumps oil vapor into the chamber.
Cited in: The Vacuum Budget of a Cyclotron
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Budget unbaked, uncleaned stainless steel at ~1e-5 Pa-m/s (~7.5e-9 Torr-L/s-cm2) after 10 h of pumping, reduced 10-100x for high-vacuum suitability - the quoted figures; the book's bake schedules (mild vs 150 C) and UHV reduction factors are its adjacent material (scan re-read queued).
q(304 SS, unbaked, 10 h) ~ 1e-5 Pa-m/s; HV needs 10-100x reduction; UHV needs 1e4-1e5x; unbaked systems ~1e-6 Pa base, UHV bake ~150 CSource quote & editorial note
The outgassing rate of unbaked, uncleaned stainless steel is of order 10-5 Pa-m/s after 10 h of pumping... reduced by a factor of 10-100... to be suitable for high vacuum
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 308
Editorial note, tabletop extrapolation: Multiply the next machine's internal area by 1e-5 Pa-m/s and divide by delivered pumping speed to predict the 10-hour base pressure before drilling a single hole.
Cited in: The Vacuum Budget of a Cyclotron
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Compress Viton O-rings 15-20% of chord diameter (Kalrez max 12%); aim for initial contact pressure of at least 13 kg/cm2 for 60-75 Shore gaskets - a 3.2 mm ring at 75 Shore develops about 2.7 kg per cm of ring length.
compression 15-20% (Viton), <=12% (Kalrez); min contact pressure ~13 kg/cm2; seal force ~2.7 kg/cm for 0.318 cm ring @75 ShoreSource quote & editorial note
O-rings are typically compressed 15-20% of their diameter... the general criterion for high vacuum sealing to be a minimum initial contact pressure of 13 kg/cm2
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 337-338
Editorial note, tabletop extrapolation: The 2.7 kg/cm figure sizes the lid bolting: a 10-inch-circumference seal (25.4 cm) needs about 69 kg of clamping just for the ring - a 10-inch-diameter ring (79.8 cm around) needs about 216 kg - before atmospheric load helps. Size bolts and flange stiffness from the complete load and allowable-stress calculation.
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An unbaked Viton O-ring outgasses ~1e-3 Pa-m/s initially; a 4-h 150 C bake plus 12 h of pumping drops it to 4e-7 Pa-m/s (2500x). Re-exposure to air reloads the elastomer with water, and solvent washing is ineffective.
Viton: 1e-3 Pa-m/s unbaked -> 4e-7 Pa-m/s after 4 h @150C + 12 h pumping; solvent washing is ineffectiveSource quote & editorial note
An unbaked Viton O-ring will have an initial outgassing rate of 10-3 Pa-m/s... After a 4-h bake at 150C and 12 h of pumping, this value is reduced to 4x10-7 Pa-m/s.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 340
Editorial note, tabletop extrapolation: Argues for baking the assembled system under vacuum where the components allow it. An ex-situ pre-bake in a small vacuum oven helps only to the extent air exposure before assembly is minimized, and the payoff in chamber pressure depends on whether the rings dominate the gas load - budget the gas loads before promising an order of magnitude.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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Do not grease static elastomer seals: grease is not needed for a static elastomer-metal seal and traps gas pockets that release as pressure bursts; if a damaged flange forces it, use the thinnest possible film - and wear gloves, since fingerprints contaminate vacuum surfaces.
Source quote & editorial note
Grease is not needed to make a static seal between an elastomer and a metal surface. It will cause pressure bursts as trapped gas pockets are released.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 340
Editorial note, tabletop extrapolation: Counters the amateur habit of greasing everything: on a clean, undamaged seat with proper squeeze, a dry Viton ring seals without grease's gas burden. A scratched flange is a repair item first; grease is the temporary expedient, not the standard practice.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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For a small diffusion-pumped system, cross over from an oil-sealed roughing pump to the high-vacuum pump at the '100-mTorr rule' point - the source cites circa 10-15 Pa, glossed as 100-150 mTorr (note its own conversion is loose: 100-150 mTorr is 13-20 Pa) - because roughing below that backstreams oil into the chamber.
crossover ~ 100 mTorr class (13 Pa) for small chambers with oil-sealed roughing; viscous flow above the boundary flushes oil back toward the pumpSource quote & editorial note
one should not rough a chamber with an oil-sealed mechanical pump below a pressure of circa 10-15 Pa (100-150 mTorr), otherwise oil backstreaming would contaminate the chamber... the '100-mTorr rule' is valid [for small systems]
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 379-381
Editorial note, tabletop extrapolation: For the reference machine: valve over to the SI100 around 100 mTorr rather than letting the rotary pump grind into the 1e-2 Torr range - after checking the SI100's own maximum inlet/crossover and foreline specs, which are the binding numbers for the diffusion-pump side.
Cited in: The Vacuum Budget of a Cyclotron
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Systematic leak hunting, per the source: blank off and verify the rough pump first (a flange with only a thermocouple gauge); if the pump is good, pump foreline/roughing sections sequentially until the leaky section is isolated; helium-spray external checks start at the TOP of the chamber with only a small flow; welds and seals - the most common leak sites - get checked first; alcohol freezes in a small leak, letting adjacent areas be checked without confusion (remove it with a heat gun).
Source quote & editorial note
the mechanical pump should be disconnected and connected to a blank flange containing only a thermocouple gauge. ... If the pump is operating properly, sections of the foreline and roughing line can be pumped sequentially and systematically until the leaky section is isolated. ... External leak checking with helium should begin at the top of the chamber; only a small helium flow rate is necessary. ... Alcohol freezes in a small leak and allows adjacent areas to be checked without confusion. The alcohol can be removed with a heat gun. ... Welds and seals are the most common leak sites
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 467-470
Editorial note, tabletop extrapolation: Helium rises and migrates: working top-down with small flow keeps the migrated-helium background from swamping localization on a chamber with many ports (the source suggests nitrogen-flushed plastic wrap where sites crowd together). Alcohol near energized equipment is a flammability point - sensible precautions.
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Distinguish a leak from outgassing with a rate-of-rise test: valve off the pump and plot pressure vs time - a molecular leak gives a linear rise over the useful test interval, while outgassing rolls over toward a steady-state value set by the vapor pressures of the desorbing species.
Q = V*dP/dt; leak: dP/dt = const; outgassing: dP/dt decreasing to plateauSource quote & editorial note
A molecular leak causes a linear increase in pressure with time. Outgassing causes the pressure to rise to a steady-state value that is determined by the vapor pressures of the desorbing species.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 468-469
Editorial note, tabletop extrapolation: First diagnostic whenever a next machine won't reach base pressure - existing gauge plus stopwatch. A constant slope points toward the helium bottle, a rolling-over curve toward bakeout - as the leading hypothesis, not a verdict: virtual leaks also roll over, water outgassing can mimic a leak on an RGA, and a real leak departs from linearity once the pressure rises far enough.
Cited in: The Vacuum Budget of a Cyclotron
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Helium permeates a typical Viton O-ring in about 20 minutes, so during MSLD leak checking of an elastomer-sealed system the He background creeps up and won't fall until the gaskets degas - take a break rather than chase phantom leaks, and never leak check during bakeout.
He permeation time through Viton gasket ~20 min at room temperature; much faster hotSource quote & editorial note
This pressure rise is due to helium permeation. The permeation time is about 20 min for a typical Viton O-ring. ... First, do not attempt to leak check the system during baking. Second, helium background from a loaded O-ring will not decrease until it has been pumped from the gaskets. A coffee break may be required before proceeding.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 469-470
Editorial note, tabletop extrapolation: On an all-Viton chamber, spray briefly and wait: a slowly rising, broad He signal minutes after spraying is CONSISTENT WITH gasket permeation rather than a leak at the last joint - confirm by letting the baseline recover and re-testing for a prompt, reproducible local response before moving on.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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On an RGA, oxygen at m/z=32 alongside nitrogen at 28 supports an air leak (atmospheric N2:O2 ~3.7:1, modulated by species sensitivity, and 28 also carries CO); a large 18 peak needs the rate-of-rise to separate water outgassing (falling rate) from a water-line leak.
air leak signature: m/z 32 present with 28 (check 14 and 40 too); m/z 18 (17) source: repeated spectra / rate-of-rise decides outgassing vs water-line leakSource quote & editorial note
Air leaks are discerned by the presence of oxygen at m/z = 32... Outgassing and water line leaks each can produce a large peak at m/z = 18, but they can be distinguished by the rate of rise.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 471
Editorial note, tabletop extrapolation: A used RGA head is arguably the single best diagnostic upgrade for a next machine - one spectrum plus a short rate-of-rise watch replaces a day of guessing.
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No structure can beat the aperture limit: molecular-flow conductance of any opening is at most 11.6 L/s per cm2 for room-temperature air, and any real tube delivers only a fraction a (transmission probability) of that.
C(L/s) = 11.6*A(cm2) for a thin aperture; C = 11.6*a*A for a real duct; long round tube a ~ 4d/(3l)Source quote & editorial note
the molecular conductance per unit area of any structure in molecular flow has a maximum value [11.6 L/(s-cm2) for air at 22C]
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 48-50
Editorial note, tabletop extrapolation: Sets the ceiling on what the SI100 can actually pump through the chamber port: a 4-inch (81 cm2) opening passes at most ~940 L/s, and a baffled elbow far less - size the pump port as large and short as possible.
Cited in: The Vacuum Budget of a Cyclotron
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Room-temperature outgassing of water from metals falls off roughly as 1/t for the first ~10 hours of pumping, so published outgassing rates are meaningless without their timestamp (1 h and 10 h values differ ~10x).
q = q_n / (t/t_n)^a, a = 0.7-2, typically 1, valid ~first 10 hSource quote & editorial note
Room temperature outgassing data for most gases sorbed on metals, including water vapor, show the outgassing rate to vary inversely with time, at least for the first 10 h
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 80-81
Editorial note, tabletop extrapolation: Explains why the chamber keeps improving overnight without any leak being fixed, and why comparing pump-down curves is only fair at equal elapsed times.
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One adsorbed monolayer is ~1e15 molecules/cm2 (the slides' rule of thumb); with an impingement-flux model (gas species, temperature and sticking coefficient stated) that converts to monolayer coverage times of seconds at 1e-6 Torr and ~1000x longer at 1e-9 Torr.
monolayer ~1e15/cm2; coverage time from impingement flux phi = p/sqrt(2*pi*m*k*T) with an assumed sticking coefficient - the classic ~2 s at 1e-6 Torr assumes unity sticking at room temperatureSource quote & editorial note
Rule of thumb - one monolayer consists of ~1e15 molecules (atoms) per cm2
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 42-43
Editorial note, tabletop extrapolation: Explains why pump-down history and surface cleanliness dominate at high vacuum: the wall inventory dwarfs the volume inventory for ordinary chamber geometries - by a factor you compute from the actual area, volume and outgassing rate, which is also what sets whether the walls take hours or days to give up their load.
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A rate-of-rise test doubles as a first-pass diagnostic: measure Q = V(P2-P1)/(t2-t1) after isolating the vessel; a straight line suggests a real external leak (constant flow), a decreasing slope suggests outgassing or a virtual leak (internal, decaying source) - then confirm with helium testing.
Q = V*(P2-P1)/(t2-t1) Torr-L/s over the interval (an average, not proof of constancy); real leak: ~constant rise; virtual leak/outgassing: decreasing riseSource quote & editorial note
Real Leaks: external, constant flow, constant pressure rise. Virtual Leaks: internal, decreasing flow, decreasing pressure rise.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 429-433
Editorial note, tabletop extrapolation: The decreasing-vs-constant slope distinction also flags virtual leaks from unvented hardware, which a helium sprayer can never find from outside.
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Elastomer-sealed flange systems (ANSI/ISO/KF) are realistically good to ~1e-6 Torr (rated 1e-8) and limited to ~150 C bakes; if a joint must ever be baked hotter or hold UHV, design in a metal seal (Conflat copper 300+ C) from the start.
elastomer flanges: rated 1e-8 Torr, better suited to 1e-6 Torr, 150 C max; metal seals (CF/VATSEAL) bakeable to 300 CSource quote & editorial note
Vacuum rated to 1 x 10-8 Torr (better suited to 1 x 10-6 Torr). Temperature rating is dependent on which elastomer o-ring is used (usually 150C)
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 443-446
Editorial note, tabletop extrapolation: Matches the reference machine's observed 1e-6-range vacuum with Viton seals - typical of all-elastomer systems, where permeation and outgassing usually hold operation near the recommended regime, though well-designed elastomer systems can run lower. A CF port or two on a next machine (gauge, RGA) buys bake and UHV headroom cheaply.
Cited in: Cyclotron Glossary · Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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When helium leak checking: specify leaks quantitatively and never as 'vacuum tight' (the slides' own instruction); calibrate the detector against a standard leak, use a low-flow tracer probe, keep helium away from elastomers, and bag suspect regions to localize.
typical MSLD sensitivity spec: 2e-10 atm-cc He/s; ASTM E432, E479, E493, E498, E499, F97Source quote & editorial note
Avoid phrases like; leak tight, vacuum tight, good to 10-8 Torr, good for ultrahigh vacuum, etc.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 456-464
Editorial note, tabletop extrapolation: When farming out welds or buying used hardware, write the acceptance spec as a number DERIVED from the machine's gas-load budget: Q_leak,max = S_eff x (allowable pressure contribution), split between total and single-leak allocations, with tracer gas, test pressure and calibrated detection limit stated - detector sensitivity is what the instrument can see, never itself the acceptance criterion.
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Use published outgassing data comparatively, not absolutely (the slides' table, x1e-10 mbar-L/s-cm2, 1 h / 4 h): Al 80/7, mech-polished Cu 47/7, raw OFHC 266/20, unpolished SS 266/20, electropolished SS 66/5, slightly rusty mild steel 58,520/199 - prepared metals improve sharply with pumping time; raw copper and unpolished stainless settle at ~20, not single digits.
1h/4h desorption (1e-10 mbar-L/s-cm2): Al 80/7, Cu mech-polished 47/7, OFHC raw 266/20, SS unpolished 266/20, SS electropolished 66/5, rusty mild steel 58520/199Source quote & editorial note
Stainless Steel (unpolished) 266 [1 hr] 20 [4 hrs]... Mild Steel, slightly rusty 58,520 199 (mBar-l/sec-cm2 x 10-10)
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 49
Editorial note, tabletop extrapolation: The ~200x one-hour penalty (dropping to ~10x by four hours) for rusty mild steel is the argument for keeping exposed in-chamber pole faces from corroding at all - and for qualifying any specific remedy (plating, vacuum-rated coating, stainless cladding) on its own outgassing, adhesion and magnetic-gap costs rather than prescribing one.
Cited in: The Vacuum Budget of a Cyclotron
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Generic cleaning sequence for vacuum components, from the slides' flow charts: mechanical clean, acetone for tape and ink residues, detergent wash, rinses between baths, DI rinse to the stated resistivity minimum, air dry or filtered-nitrogen dry, then protect in lint-free wrap; bakeout is the final step, and a 200 C bakeout is still required after glow-discharge cleaning.
DI rinse (SS flow chart): >= 2e6 ohm min. resistivity @ 65 C final rinse (slides' notation; water resistivity is conventionally ohm-cm); SS acid pickle 50% by vol. HNO3 with HF (HF concentration illegible in scan - re-read queued)Source quote & editorial note
Mechanical Cleaning; Degreasing or Solvent Cleaning; Detergent Cleaning; Chemical Etch; Electrolytic Polishing; High Pressure Spray; Bake-out ... Remove all tape, ink, & other residues with Acetone & a clean cotton rag ... DI rinse (2 x 10^6 Ohm min. resist. @ 65oC) Air dry or dry with filtered compressed nitrogen ... Protect with lint free paper, foil, or plastic bags ... Acid pickle (50% by vol. HNO3 ... @ 25oC) 10 minutes if removing mill scale, 30 seconds to remove trace alkaline ... A 200oC bakeout is still required after glow discharge cleaning.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 497-513
Editorial note, tabletop extrapolation: Scaled down: acetone wipe, hot detergent wash, DI rinse, N2 or oven dry, gloves-only handling afterward gets most of the professional benefit for chamber internals. The acid pickle stays professional - HF work needs formal controls and alloy-specific procedure, and is not part of the amateur-safe subset.
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A virtual leak is trapped atmospheric gas bleeding out through a blind path; its gas load is bounded by Santeler's envelope Q <= Pa*V/(e*t), and the classic culprits are unvented screws in blind tapped holes, double welds enclosing a void, and unvented double O-rings - vent (drill or slot) every trapped volume.
Q_max(t) = Pa*V/(e*t) - the worst case at time t over all connecting conductances; a specific path with conductance C gives Q(t) = C*Pa*exp(-C*t/V) (Santeler, NASA SP-105)Source quote & editorial note
A virtual leak is a volume of trapped atmospheric gas that leaks into the vacuum vessel through holes or cracks that do not go all the way through the vessel wall. [Examples:] Unvented Screw, Two Welds in Series, Unvented Double O-rings
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 59-63
Editorial note, tabletop extrapolation: Every internal socket-head screw in the next machine (dee supports, ion source mounts) needs a vent hole, a slotted thread, or a vented washer; a slot machined in the O-ring groove floor serves the same purpose.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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O-ring seal design for accelerator vacuum: prefer face seals, use as heavy a squeeze as possible, consider lubrication only when heavy squeeze is impossible, expect heavy flange construction to react the squeeze, and use two O-rings with a guard vacuum between them to drastically cut permeation.
guard vacuum example: 760 Torr across 1st ring reduced to 1e-2 Torr across 2nd ring (DARHT-II: 15 mTorr guard, 5e-8 Torr design pressure)Source quote & editorial note
Face-type o-ring seals are recommended. Use as heavy a squeeze as possible... Two o-rings in series can drastically reduce permeation.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 71-74
Editorial note, tabletop extrapolation: To push an elastomer-sealed system's floor lower on a next machine, a double O-ring lid groove with a guard vacuum from the existing roughing pump attacks the permeation term specifically - the dominant elastomer floor once outgassing is conditioned down - for the cost of one groove and a hose barb. The guard reduces pressure-driven permeation through the inner seal (DARHT's numbers are that installation's); the inner ring's own outgassing remains, so the floor drops rather than disappears.
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Set the vacuum requirement so the beam's mean free path is at least an order of magnitude longer than the total spiral flight distance; compute the flight distance as the sum of the spiral's per-turn circumferences (for r proportional to sqrt(E), about two-thirds of turn count times the final circumference). [Corrected 2026-08-23: an earlier version repeated the source's conclusion that ~2e-3 torr is adequate for a fast machine. That figure follows from the thesis reading a 5 km mean free path off its own plot at 2e-3 torr, which implies a cross-section near 3e-20 cm2 - four orders of magnitude below the measured proton electron-capture cross-section in hydrogen (8.7e-16 cm2 at 10 keV, ORNL-6086 p. A-28). With the measured value the capture mean free path at 2e-3 torr is about 0.2 m, shorter than one turn. The criterion stands; the number does not, and the thesis machine reported no beam. Compute the mean free path with the capture cross-section, never the gas-kinetic one; see /learn/vacuum/.]
MFP >= 10 * flight path; lambda = kT/(P*sigma) with sigma the charge-exchange cross-section [the source's '2e-3 torr -> ~5 km' uses a sigma four orders too small; see correction]Source quote & editorial note
An acceptable vacuum would allow for a mean free path an order of magnitude larger than the expected flight distance. For protons accelerated by a 2.7 T magnetic field and a voltage difference of 1000 V between the electrodes, the expected flight distance is approximately 300 meters.
Editorial note, tabletop extrapolation: The quantitative vacuum spec for a next machine: turns = final energy / energy-per-turn, and total path is turns times the average orbit circumference (about two-thirds of the final one for r proportional to sqrt(E)); halving dee voltage doubles the path and tightens the pressure requirement proportionally. Evaluate lambda with sigma(E) from ORNL-6086 along the orbit (the vacuum calculator's orbit mode does this); a 150 keV, 1 kV-per-dee proton machine needs ~1e-5 torr for 10% loss, not 1e-3.
Cited in: Beam Quality: What It Is and What Degrades It · The Vacuum Budget of a Cyclotron
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Vacuum-weld discipline: use single, continuous seam welds arranged so no unvented trapped volume or vacuum-side crevice remains, and stagger-weld internal bracing so it cannot form sealed pockets - Argonne welded its seams on the atmosphere side only and stagger-welded the braces 'to keep virtual leaks at a minimum'. [Corrected 2026-08-23: earlier text made 'weld only on the atmosphere side' a universal rule and said virtual leaks 'cannot form'. Vacuum-side or full-penetration welds are normal where they avoid a vacuum-side crevice; the invariant is no double-sealed unvented pocket, and Argonne's own word is 'minimum', not zero.]
Source quote & editorial note
Seam welds are continuous, with welding only on the atmosphere side. The internal braces are stagger welded to keep virtual leaks at a minimum.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 7
Editorial note, tabletop extrapolation: On any welded chamber or fitting for a next machine the question to ask of every joint is: is there a pocket sealed on both sides, or a crevice open to vacuum? Vent it, or weld it through. Argonne's atmosphere-side seams are one way to satisfy that, not the rule itself.
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Diagnose breakdown sites by their fingerprints: in the cited tests, starburst patterns clustered at contaminant-particle sites, leading the author to conclude particles cause breakdown - so post-mortem electrode inspection locates candidate initiation sites.
Source quote & editorial note
the frequency with which starbursts appeared at particle sites, I have concluded that particles cause breakdown
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 46, 78
Editorial note, tabletop extrapolation: When a next machine sparks, a loupe inspection for starbursts and craters gives the builder candidate locations for the field problem instead of guessing from outside the chamber - corroborate with particle, geometry and field checks before machining anything.
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Electrode material choice was secondary for HV holdoff in these tests: with contaminant particles present they, not the substrate (Nb, Cu, Au, or their oxides - films ~1000 A, oxides hundreds of angstroms), set the breakdown voltage, and clean Nb and Cu cathodes showed no significant breakdown difference.
Source quote & editorial note
if there are contaminant particles, then they, and not the substrate material, determine the breakdown voltage. ... The Cu and Au films were about 1000 A thick; the oxide films were hundreds of angstroms thick. ... there seems to be no significant difference in breakdown voltages on niobium and copper cathodes.
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 84
Editorial note, tabletop extrapolation: The builder can reasonably keep aluminum dees and spend the effort on cleaning and conditioning instead of exotic electrodes - with the caveat that the tests covered Nb, Cu, Au and their oxides, not aluminum's native oxide; let the machine's own conditioning behavior confirm it.
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Temperature changed HV holdoff dramatically in the cited tests: cathode sites held 95 MV/m at 100 C with no field emission, while the same sites at room temperature showed field emission from ~40 MV/m and broke down near 90 MV/m.
at 100 C: no FE at 95 MV/m; at 22 C: FE onset ~40 MV/m, breakdown ~90 MV/mSource quote & editorial note
Both sites reached 95 MV/m at 100 C with no evidence of field emission ... At room temperature (22 C), field emission began near 40 MV/m, and breakdown occurred around 90 MV/m
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 96
Editorial note, tabletop extrapolation: Motivates a controlled experiment on the reference machine, not a guaranteed fix: try a gentle bake of the dee assembly before HV runs and measure field-emission onset and holdoff after cooldown - the cited data compare performance AT temperature and don't establish that the improvement survives cooling, or the mechanism.
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Attain about 1e-5 mm Hg before starting, tolerate no worse than ~1e-3 mm Hg during RF bakeout, and cyclotron operation 'can be attempted' - the source's phrasing - at 1e-4 mm Hg or less.
base ~1e-5 torr; bakeout ceiling ~1e-3 torr; operation <= 1e-4 torrSource quote & editorial note
a preliminary vacuum of about 10^-5 mm hg should be attained; during 'bakeout' pressure should not exceed ~10^-3 mm. Operation as a cyclotron can be attempted with a pressure of 10^-4 mm or less
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 6
Editorial note, tabletop extrapolation: Historically grounded milestones, and the regime the reference machine operates in. What pressure a given machine NEEDS is the charge-exchange survival calculation (dg-460; the vacuum calculator's orbit mode) - at 1e-4 torr a proton spiral loses heavily, which is why this collection's operating rules sit in 1e-5-class territory.
Cited in: The Vacuum Budget of a Cyclotron
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Wash all tank parts before final assembly to remove organic matter (Wouters recommended a preliminary CCl4 wash; use a modern material-compatible degreaser instead).
Source quote & editorial note
preliminary washing of the parts in CCl4 is recommended to remove organic matter
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 9
Editorial note, tabletop extrapolation: Degrease everything on a next machine that sees vacuum - machining oil, fingerprints, rubber residues - with a solvent chosen per material (elastomers, coatings and trapped volumes need their own compatible process); CCl4 itself is excluded on toxicity grounds.
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Run a short, fat (3-inch diameter) pump duct straight down from the chamber to maximize conductance - the paper's design choice, on a machine that holds ~1e-7 Torr base while feeding its ion source.
3 in dia straight vertical duct; base ~1e-7 Torr with gas loadSource quote & editorial note
a 3 inch diameter tube in the corner can extend directly downwards to a vacuum pump underneath. This design choice maximizes vacuum conductance.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2
Editorial note, tabletop extrapolation: Pumping a gas-fed cyclotron is conductance-limited, so place the pump under the chamber with the largest, straightest duct possible - the term you control at layout time. What pressure results is the whole budget's answer: throughput, pump speed and conductance together (the vacuum calculator).
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Make thin vacuum-chamber lids workable inside a tight magnet gap by supporting them with internal steel rods/posts that carry the atmospheric load, instead of thickening the plates - as the cited machine did.
Source quote & editorial note
Steel supporting rods allow thin top and bottom plates to minimize thickness
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 6-7
Editorial note, tabletop extrapolation: Every millimeter of lid steel is a millimeter of magnet gap - but posts are not free: ferromagnetic posts in or near the gap distort or shunt the field, so place them outside the useful-field region (or use nonmagnetic posts) and verify by model or map; and do the plate-stress and buckling arithmetic for full atmospheric load before trusting a thin lid.
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Run new vacuum hardware hot deliberately to degas it: initial operation raises pressure for minutes, and when the power is then turned down or off, pressure plunges to new lower levels once the surfaces have cleaned up.
Source quote & editorial note
You can hasten the process by running the fusor to degas the inner surfaces. This sends the pressure upward, but after a few minutes it starts to drop ... Turning the fusor power down or off after a few minutes of on time will have the pressure plunge to new lower levels.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 5-6
Editorial note, tabletop extrapolation: The same logic applies to the reference machine's chimney and dee surfaces - but translate it as controlled RF or discharge conditioning with pressure and arc interlocks, not an open-ended beam-on bake-in: beam operation adds sputtering, beam loss, and (at higher energies) activation questions a conditioning plan should assess first.
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For fusion-grade cleanliness, pump to ~1e-6 Torr base pressure first, then backfill with deuterium through fully evacuated lines to 1-10 microns operating pressure.
base ~1e-6 Torr; operate at 1-10 micron D2 backfillSource quote & editorial note
To fully clean the system of residual gases, an initial base pressure of around 1e-6 Torr is necessary. A leak valve is then used to backfill the chamber with deuterium to a pressure in the range of 1 to 10 microns.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 6
Editorial note, tabletop extrapolation: The base-pressure-then-backfill discipline is exactly the reference machine's MFC workflow; at the quoted fusor numbers the operating-to-base ratio is 1,000-10,000:1, which is what keeps the feed gas dominant - but composition is earned by measurement (RGA or gas-load accounting), not by a pressure ratio alone.
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A 1e-6 torr operating vacuum via diffusion pump plus liquid-nitrogen cold trap (roughing to 1e-3 torr mechanically) is the proven recipe at the 15 cm, few-hundred-keV scale; monitor with thermocouple gauges above 1e-3 torr and an ion gauge below.
rough to ~1e-3 torr, diffusion+trap to ~1e-6 torr; TC gauge >=1e-3, ion gauge to 1e-8Source quote & editorial note
an Innovac R220 diffusion pump and Kurt J Lesker TNR6XA150QF cold trap are used, which can lower the pressure to about 1e-4 Pa (1e-6 torr)
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 41-43
Editorial note, tabletop extrapolation: Matches the reference machine's scale exactly: 1e-6 torr base, bled up with source hydrogen, is the working point of the documented machines in this peer group (Houghton, the Rutgers 12-inch, the reference machine - the census's compare rows carry the values). The recipe is the proven one at 15 cm scale; the pressure a machine actually needs remains the survival calculation's answer (dg-460).
Cited in: The Vacuum Budget of a Cyclotron
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Match the chamber to the magnet - the paper's build: a 2.54 cm thick aluminium ring of 9.9 cm outer / 8.5 cm inner radius, ten KF-16 ports secured with vacuum epoxy, with 0.65 cm lids carrying a Viton O-ring groove, reaching 2e-6 Torr.
wall ring 2.54 cm thick, r_out 9.9 cm, r_in 8.5 cm; lids 0.65 cm; 10 x KF-16; Viton O-ring; base 2e-6 TorrSource quote & editorial note
A 2.54 cm thick ring with an outer radius of 9.9 cm and an inner radius of 8.5 cm was milled from 6061 T6 aluminium ... Ports were made in the chamber wall using ten KF-16 flanges, which were secured using Hysol Loctite 1C vacuum epoxy
Editorial note, tabletop extrapolation: A complete documented chamber design for an 8-inch-pole machine, including the epoxied-flange trick that avoids welding. Copy from the paper - then qualify your own copy: epoxy joints and lid stiffness are workmanship-dependent, so leak-check the flanges and run the lids through the lid-deflection calculator rather than inheriting the paper's result.
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Seal large flanges the ORNL way: a continuous square-section rubber gasket in a groove of sufficient cross-section to accommodate the entire gasket under pressure, so the metal faces land metal-to-metal - which the report calls very satisfactory.
groove volume >= gasket volume; metal-to-metal closureSource quote & editorial note
continuous square rubber gaskets located in grooves in the faceplates of sufficient cross section to accommodate the entire gasket under pressure. The resulting metal-to-metal contact ... has proved very satisfactory.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 41
Editorial note, tabletop extrapolation: A strong pattern for a next machine's chamber lids: the metal stop limits further squeeze after closure and makes reassembly repeatable - still check gland fill and squeeze for the actual compound (groove depth sets the squeeze; a too-shallow groove over-crushes even with a metal stop), including tolerance, swell and thermal growth.
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In the cited pump system, a steady stream of dry air injected at the mechanical pump outlet could eliminate the refrigerated vapor trap, and the tank was vented only with dry air to minimize admitted moisture.
Source quote & editorial note
a steady stream of dry air injected into the outlet side of the pump cylinder could eliminate the need for a refrigerated vapor trap ... dry air is used in the tank in order to minimize the amount of moisture
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 44
Editorial note, tabletop extrapolation: Two separable methods: vent the next machine's chamber with dry nitrogen or desiccated air rather than room air (admitted water vapor drops and pumpdown shortens), and treat exhaust-side purging as pump-specific - follow the pump manual, keep any inlet trap the pump needs for vapor handling or oil backstreaming, and mind oxygen deficiency when nitrogen-venting in a small space.
Cited in: The Vacuum Budget of a Cyclotron
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Do not switch on a hot-filament ionization gauge until pressure is below ~0.5 micron (the cited system's rule; check the modern gauge's own limit), mount it where the conductances from the pumps to gauge and to tank are comparable - the cited machine estimated them approximately equal - and give its filament some magnetic shielding, as the manifold wall provided there.
ion gauge on only below ~5e-4 torrSource quote & editorial note
the ion gauge is not turned on until the tank pressure is less than 0.5 microns ... In this position the conductance from the diffusion pumps around the gate valves to the ion gauge has been estimated to be approximately the same as the conductance from the diffusion pumps to the tank proper. ... the wall of the manifold provides the tube filament with some protection from the magnetic field
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 45
Editorial note, tabletop extrapolation: Directly applicable gauge practice near a stray-field-rich H-frame magnet: place the gauge to read the pressure you care about (conductance gradients bias a badly placed gauge under gas flow), and verify the shielding by comparing readings with the field on and off.
Cited in: The Vacuum Budget of a Cyclotron
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Add a Penning (Philips) gauge alongside the ion gauge: far more rugged and sensitive to small pressure changes, though probably not as accurate in absolute pressure.
Source quote & editorial note
far more rugged than the triode ion gauge and sensitive to small changes in pressure; but it is probably not as accurate in reading absolute pressure.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 46
Editorial note, tabletop extrapolation: A cheap Penning head earns its keep as a trend and gas-flow indicator, with the ion gauge kept for absolute readings. For protection interlocks use fail-safe, manufacturer-approved instrumentation - Penning cells can ignite late and drift with contamination - and commercial heads carry their own magnet: mount and shield per the head's specification rather than borrowing the cyclotron's field.
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Benchmark chamber gas load by rate-of-rise: the 280 ft^3 ORNL system held 0.00015 micron/sec with pumps valved off - a total gas load Q = V*dP/dt of ~1.2e-3 torr-L/s. Compare machines by Q, not by pressure rate.
rate-of-rise spec ~ 1.5e-7 torr/s on 280 ft^3 (leak load ~ 1.2e-3 torr-L/s)Source quote & editorial note
Rate of rise on tank assembly 0.00015 microns/sec
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 46
Editorial note, tabletop extrapolation: Measure rate-of-rise after every re-seal as the standard leak-health metric, and state the benchmark as a gas load, not a pressure rate: the ORNL figure corresponds to Q = V*dP/dt ~ 1.2e-3 torr-L/s. A ~30 L chamber would rise at ~4e-5 torr/s only if it carried that same total load - rate-of-rise includes real leaks, virtual leaks and outgassing, so 'equally tight' means equal Q, not equal construction scaled by volume. [Note revised 2026-08-23: earlier note scaled the expectation by volume alone.]
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For vacuum service pick elastomers on the source's three axes - low gas permeability (butyl outstanding), low weight loss under vacuum, and good compression-set resistance - and use up to 40% squeeze with a correspondingly wider groove.
vacuum squeeze up to 40% with increased groove width; choose compound on permeability / vacuum weight loss / compression setSource quote & editorial note
For vacuum seals, O-rings must be comprised of elastomeric materials featuring low gas permeability, low weight loss under vacuum, and good compression set characteristics. ... With outstanding low permeability to gases, Butyl is especially effective in vacuum sealing applications. ... Employing a seal squeeze of up to 40% inhibits media flow through the seal... because of the decreased groove depth, increased groove width is essential.
Apple Rubber Products, Seal Design Guide — p. 84
Editorial note, tabletop extrapolation: Endorses heavier-than-usual squeeze on critical static vacuum joints when the groove is widened to take the displaced volume - within the compound's own application limits. A pre-bake ('post cure' in vendor language) to drive off volatiles before service is cheap insurance on silicone and fluorocarbon compounds.
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In a group of bolts, earlier-tightened bolts relax as later ones compress the joint (elastic interaction), which the source says can virtually eliminate their tension - tighten flange bolt circles in a cross pattern and in multiple passes, re-checking the first bolts.
Source quote & editorial note
As we tighten the rest of the bolts the joint is further compressed, and the previously tightened bolts tend to relax and lose some of their preload. In some cases, this can virtually eliminate our bolt tension.
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 26
Editorial note, tabletop extrapolation: On the next machine's lid, single-pass tightening leaves the first-torqued sector under-clamped - a plausible contributor to O-ring leaks that seem to move with each reassembly; the multi-pass cross-pattern with recheck is the fix either way.
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When machining an extra-shallow gland to get heavy squeeze, widen the groove enough to accommodate the full O-ring volume, or the ring will be crushed instead of sealed.
Source quote & editorial note
when an extra-shallow gland is desired in order to increase the squeeze, it must be made wide enough to accomodate the full O-ring volume.
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 1-2
Editorial note, tabletop extrapolation: If a next machine's grooves are cut for 30% squeeze, groove cross-section area must still exceed ring cross-section area - check fill before cutting.
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Use dovetail grooves where the ring must be retained during assembly and maintenance (vertical faces, lids that open) - the guide's own purpose for them; take the dimensions from its Design Charts II & III, and hold the sharp-corner radius R closely: too small damages the ring on installation, too large invites extrusion.
Dovetail per the source's Design Charts II & III (66 deg walls; W=.139 -> L=.111-.113, G=.113-.117, ~20% squeeze, R=.010 - chart values, scan re-read queued); radius R is criticalSource quote & editorial note
It is often necessary to provide some means for retaining an O-ring in a face seal groove during assembly and maintenance. An undercut or 'dovetail' groove has proven effective in many applications to keep the O-ring in place ... Design Charts II & III (see pp 7-8) provide dimensional recommendations for full and half-dovetail vacuum seal O-ring grooves. ... Radius R is CRITICAL. Insufficient radius will potentially cause damage to the O-ring during installation, while excessive radius may contribute to extrusion.
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 10
Editorial note, tabletop extrapolation: Worth it for a hinged or frequently-removed lid where the ring falls out during assembly; otherwise plain rectangular face grooves are cheaper and more tolerant.
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Avoid welding lids onto a thin flat vacuum chamber: weld shrinkage warped the whole frame; grinding off the weld and sealing with a flat Viton gasket fixed it - prefer demountable elastomer seals for flat chambers.
Source quote & editorial note
after the welding, the bottom plate contracted so much that it bent the whole frame out of shape... seal the bottom plate against the frame using a flat Viton ring.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2-3
Editorial note, tabletop extrapolation: A fabrication trap the builder can sidestep: demountable elastomer seals on both lids avoid weld distortion entirely on a thin flat chamber - the route the source machine retreated to after its frame warped. Where welding is preferred, controlled sequence and post-weld machining are the professional counters; for a garage build, not welding thin flat plates is the cheap answer.
-
Stretch a groove-mounted O-ring 1-5% on its ID (2% ideal); more than 5% is not recommended - the resulting stress causes accelerated aging and cross-section reduction.
O-ring ID = groove diameter / (1 + stretch), stretch 0.01-0.05, ideal 0.02; CS reduction ~ f(% stretch)Source quote & editorial note
This stretch should be between 1%-5% with 2% as the ideal in most applications. A stretch greater than 5% is not recommended. The resulting stress on the O-ring will cause accelerated aging and cross section reduction.
Apple Rubber Products, Seal Design Guide — p. 11
Editorial note, tabletop extrapolation: When picking the AS-568 size for a non-standard groove (dee-stem feedthrough, viewport), size so the ring sits at ~2% stretch rather than swimming or straining.
-
Never let the O-ring volume exceed the gland volume (crush seals excepted, where fill should still stay under 95% of the gland void) - thermal expansion or swell with a 100% -filled gland destroys the seal or the hardware.
V_oring(max, incl. tolerances) < V_gland(min); crush seals: V_oring <= 0.95 * V_glandSource quote & editorial note
The maximum volume of the O-ring should never surpass the minimum volume of the gland... For a static crush seal application, it is recommended that the O-ring volume does not exceed 95% of the gland void.
Apple Rubber Products, Seal Design Guide — p. 14-16
Editorial note, tabletop extrapolation: Check fill arithmetic including worst-case ring tolerance before machining. Viton heated by RF or magnet proximity needs that free volume: elastomer linear expansion is around 1.6e-4/C, so use the volumetric coefficient (roughly three times the linear value) in the fill calculation.
-
Static gland sealing faces tolerate finishes as rough as 64-128 micro-inches RMS but 32 RMS is preferred - and the guide's static gland detail specifies 16 RMS for vacuum and gases; compress static seal cross-sections 10-40% and dynamic seals only 10-30%.
static faces: 32 RMS preferred (64-128 tolerable), 16 RMS vacuum/gas; static squeeze 10-40%, dynamic 10-30%Source quote & editorial note
Surface finishes as rough as 64 to 128 micro-inches RMS can be tolerated. However, a finish of 32 micro-inches RMS is preferred ... Static Gland Detail Surface finish: 32 for liquids, 16 for vacuum and gases ... Static seal cross sections are generally compressed from 10% to 40%, whereas dynamic seals are from 10% to only 30%.
Apple Rubber Products, Seal Design Guide — p. 19, 61
Editorial note, tabletop extrapolation: For a rotating or sliding shaft feedthrough (target manipulator), back off to <=30% squeeze and finish the shaft to the guide's dynamic-service figures (16 RMS; 10-20 micro-inches called most desirable for dynamic seals) - a rough shaft raises friction, wear and leakage quickly.
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Handle O-rings like precision parts: clean the gland of all debris, lightly coat the ring with a compatible lubricant (never a lubricant of the same chemistry as the ring - like dissolves like), cover threads/sharp edges with tape during installation, and remove twists.
Source quote & editorial note
Do not use a lubricant composed of the same material as the O-ring because 'like' will dissolve 'like.' For example, a silicone lubricant should not be used with a silicone O-ring.
Apple Rubber Products, Seal Design Guide — p. 20, 109
Editorial note, tabletop extrapolation: Check the actual lubricant and elastomer grades against a manufacturer compatibility chart. Silicone grease on Viton is commonly compatible but must still clear vacuum-outgassing requirements; petroleum grease on Buna-N is usually acceptable (NBR is built for mineral oils) though additives vary - the firm rule is the quoted one: never lubricate a ring with its own chemistry.
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To run a standard round O-ring in a rectangular face-seal groove, keep every inside corner radius at least 3x the O-ring cross-section diameter, make the O-ring centerline length equal the groove centerline length, and size the ring with the source's equation: O-ring ID = (groove CL length / 3.14) - O-ring CS.
inside corner radius >= 3 * O-ring CS diameter; O-ring ID = (groove CL length / 3.14) - O-ring CSSource quote & editorial note
In order to use a standard round O-ring, the inside corner radius of the groove should not be less than three times (3X) the O-ring cross-section diameter. ... The length of the O-ring centerline should be equal to the length of the groove centerline. Following is an equation to assist in determining the O-ring inside diameter. O-ring ID = (Groove CL length / 3.14) - O-ring CS
Apple Rubber Products, Seal Design Guide — p. 84
Editorial note, tabletop extrapolation: Directly applicable to a racetrack or rectangular lid/port on a next machine: a 1/8 in. cord ring needs >=3/8 in. corner radii or it will bunch and leak at the corners. Note the source's rectangular sizing implies zero nominal stretch while its circular-groove guidance ideals 2% - follow the section matching your groove shape.
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Size the deflector with septum radius increment dR ~ 0.15R - MIT's typical figure, with the formula showing voltage cost growing with dR - and taper the channel gap, the quoted 1/8 in at entry opening to 1/2 in or greater at exit, to accommodate divergence.
V_d ~ (2T/e)*d*(1/R - 1/(R+dR)); MIT 16 MeV, d=0.3 in: dR=0.1R -> 47 kV, dR=0.2R -> 87 kV; typical dR=0.15RSource quote & editorial note
A typical figure, used in the MIT cyclotron, is a dR of 0.15R. The deflector gap is usually tapered ... Spacings as small as 1/8 in. can be used at the entry slit, opening to 1/2 in. or greater at the exit.
Livingston & Blewett, Particle Accelerators (1962) — p. 180-181
Editorial note, tabletop extrapolation: Scaled to ~150 keV the same normalized geometry needs only ~500-900 V on the deflector - an easy supply. Entry-slit width is set against the local turn separation and beam width together (dg-495), not by a fixed prescription.
-
Choose 304L (not 304) stainless for welded vacuum chambers - the low-carbon grade is the standard vacuum choice for weld integrity - and remember TIG/MIG joint design, cleanliness, and (for aluminum) high weld speed control distortion and leaks.
Source quote & editorial note
304L SS, most commonly used in vacuum, a little more expensive... Joint design is critical from vacuum, metallurgical and distortion standpoints. Cleanliness is essential.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 355-360
Editorial note, tabletop extrapolation: For a next machine's chamber welds, specify 304L filler and stock where practical: the low-carbon grade resists weld sensitization (carbide precipitation and intergranular attack near welds). Plain 304, welded cleanly, also serves - the lecture's 'most commonly used' is a preference with reasons, not an exclusion - and leak-tightness comes from joint design and cleanliness either way.
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Verify chamber lid thickness with the fixed-edge circular-plate deflection formula (Roark): the thesis's example - a 10 cm radius aluminum lid only 3.5 mm thick deflects under 1 mm at full vacuum. Deflection is set by elastic modulus and thickness (D ~ E*t^3), which alloy choice barely moves; a higher-yield alloy like 7075-T6 raises the stress margin, not the stiffness.
delta_center = -q*a^4/(2D)*(L14-L11), D = E*t^3/(12(1-v^2)); alloy trades yield margin (7075-T6 505 MPa vs 6061-T6 275 MPa), not deflection - E is nearly identicalSource quote & editorial note
a lid with radius 10 centimeters and thickness of 3.5 millimeters would undergo less than 1 mm of deflection when covering a chamber with internal pressure of 1e-3 Torr
Editorial note, tabletop extrapolation: The actual formula for trading a next machine's lid thickness against magnet gap: a few mm of plate suffices at 8-12 inch chamber diameter IF the edge support is real (the lid-deflection calculator covers both edge conditions). Alloy choice buys yield margin at the price of 7075's poorer weldability and corrosion behavior - it stiffens nothing.
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Everything inside a strong cyclotron field must be magnetically transparent - aluminum, copper, brass - since ferromagnetic parts distort the field and disrupt measurements.
Source quote & editorial note
all cyclotron components must be made of magnetically transparent materials such as aluminum, copper, or brass
Editorial note, tabletop extrapolation: Standard but easily violated rule: screws, feedthrough bodies, and detector hardware inside the reference machine's gap should be checked with a hand magnet before installation.
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Design for maintenance access from day one: ANL mounted the dee assembly on a motor-driven rail carriage so the entire dee system rolls out of the chamber for service - the quote; the mobile diffusion-pump provision is the report's neighboring detail (scan re-read queued).
Source quote & editorial note
the VTO box and obround are mounted on a motor-driven carriage which operates on a rail system. This permits the removal of the dee heads... to facilitate maintenance.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 6-7
Editorial note, tabletop extrapolation: At tabletop scale this means: chamber slides out of the gap, dee removable through a lid, pump cart disconnectable - the difference between a research tool and a sealed monument.
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p-B11 disintegration alphas were observed from ~60-70 kV proton energy in the 1933 experiment - an observed onset under their target and detector arrangement, not a reaction threshold - with yield rising steeply toward 200 kV and a maximum alpha range of 4.7 cm in air; thick-target Li appeared from ~30 kV for comparison.
B threshold(observed) ~60-70 kV at ~50 uA and 0.7 sr; max alpha range 4.7 +/- 0.15 cm airSource quote & editorial note
It is seen that particles are detected at about 70 kv. and the numbers increase more rapidly with increase of bombarding energy than with the lithium film.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 266-270
Editorial note, tabletop extrapolation: Proof that p-B11 alphas are observable far below the 675 keV resonance: the 1933 apparatus saw them at 60-70 kV using tens of microamps and large solid angle, so a lower-current machine compensates with integration time and geometry. Their alphas stopped in under 5 cm of air, hence the vacuum path to a PIPS detector.
Cited in: Experiments by Energy Band
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Check that beam probes/collectors are thinner than the local turn spacing: at 10 kV Vp-p and 1.0 T the turn spacing near r = 4 in is only 0.04 in, so a 0.06-in-thick RF shield on the collector tip masks real beam.
dr = V_gain/(2E_total) * r; Rutgers: dr = 0.04 in at r = 4 in for 10 kVp-p, 1.0 TSource quote & editorial note
the ion revolution turn spacing near r = 4 inches, in a B-field of 1.0T will be just 0.04 inches, which is smaller than the 0.06 inch RF shield of the tip
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 1
Editorial note, tabletop extrapolation: At the reference machine's ~1.3 kV the turn spacing is smaller still, so geometry matters doubly: a thick tip costs single-turn radial resolution first, and a shield mounted AHEAD of the collector can shadow it into reading zero while beam exists - the quoted case. A bare, grooved copper collector is the safe default until turn-resolved measurements are wanted.
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Entry-slit width is set by the turn separation dr = (r/2)*(dT_turn/T) - energy gain per turn over total energy, halved (nonrelativistic); make the septum and deflector radially adjustable because calculated positions are only approximate. [2026-08-28: 'nonrelativistic' scoping adopted from the upstream erratum of 2026-08-26 - the turn-separation form drops the relativistic factor.]
dr/r per turn = (1/2)*dT_turn/T (nonrelativistic); MIT: dr ~ 0.1 in at extractionSource quote & editorial note
The limit at the entry is set by the dr between successive turns at this radius ... it is desirable to have adjustable controls on deflector spacing and location which can be trimmed empirically.
Livingston & Blewett, Particle Accelerators (1962) — p. 181-183
Editorial note, tabletop extrapolation: With ~2.6 keV total gain per turn at ~150 keV, the reference machine's turn spacing at extraction is ~0.9% of r - about 0.7 mm at r = 3.2 in - so build the septum mount with millimetre-scale radial adjustment.
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Expect extraction well below circulating current: MIT obtained up to ~25% of the resonant beam under optimum conditions (150 uA of ~600 uA circulating), with practical operation at 80-100 uA.
extraction efficiency <= ~25% (MIT: 150 uA extracted of ~600 uA circulating; routine 80-100 uA)Source quote & editorial note
Emergent beam intensities up to 25 per cent of the resonant beam intensity have been obtained under optimum conditions ... practical operating intensities would in this case be limited to 80 or 100 ua.
Livingston & Blewett, Particle Accelerators (1962) — p. 182
Editorial note, tabletop extrapolation: Judge a next machine first on internal-probe current at full radius: documented machines commonly ran internal currents several times their extracted beam (MIT's optimum was 4:1), so a gap of that order is precedented rather than failure. The rung-by-rung extraction picture is dg-595's; the census cross-checks are dg-260's.
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Protect the septum from beam power with an open construction: MIT's septum is two 0.020-in tungsten strips, edges 1/8 in apart, each silver-soldered to a curved copper bar with cooling tubing soldered on - a geometry that lets most of the resonant beam pass into the deflector channel without striking metal; others distribute the heat with a long V-slot tungsten septum.
septum: 0.020-in W strips, edges 1/8 in apart, on a cooled copper bar (MIT); alternative: long V slot spreading heatSource quote & editorial note
allows most of the resonant beam to pass into the deflector channel without striking the channel walls. In the MIT cyclotron the septum is formed of two strips of tungsten, 0.020 in. thick and 12 in. long and with the edges spaced 1/8 in. apart. Each strip is silver-soldered to a copper bar bent to the correct curvature, with copper tubing also soldered to the bar for cooling. Other designers use a long V slot in a tungsten-strip septum, so the heat is distributed over an extended surface
Livingston & Blewett, Particle Accelerators (1962) — p. 184
Editorial note, tabletop extrapolation: At the reference machine's beam power the thermal load is small but not zero - intercepted power is loss current times energy per charge (1 uA of 500 keV beam is 0.5 W into a very small spot) - so compute it, and keep the slotted geometry: it maximizes transmitted current into the channel either way.
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Relativistic detuning budget: a 10 MeV proton is only ~1% heavier, but that 1% frequency shift accumulated over hundreds of turns is what caps fixed-frequency cyclotrons near 20 MeV - a small per-turn effect below ~1 MeV, though it still accumulates with turn count.
dm/m ~ T/(938 MeV); cyclotron limit ~20 MeVSource quote & editorial note
once the particle has been accelerated to 10 MeV the mass has been changed by about 1%, which has a frequency shift of 1%.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 12, 21
Editorial note, tabletop extrapolation: At the reference machine's 100 keV-1 MeV scale the instantaneous shift is ~0.01-0.1%. Whether it can be ignored is a turn-count question: with hundreds of volts to kilovolts per turn a sub-MeV machine has phase budget to spare, but the check is the accumulated slip against the +/-90 deg window (dg-273), not the per-turn number.
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Turn-to-turn orbit separation is dR = (R/2)*(2*q*V0*sin(phi_s)/T) - it shrinks as energy grows (100 kV dee, R=1 m, 20 MeV gives only 4.4 mm), which is what makes septum extraction hard late and easy never.
dR = (R/2)*(2*q*V0*sin(phi_s)/T)Source quote & editorial note
The separation for non-relativistic ions is dR = (R/2) (2qVo sin phi_s/T)... Eq. (15.3) implies that dR = 0.44 cm.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 527
Editorial note, tabletop extrapolation: Lets the builder compute whether a probe or future septum can distinguish final turns: at ~150 keV, r ~ 9.6 cm and the reference machine's 2.6 keV total gain per turn, dR = (r/2)*(2.6/150) ~ 0.8 mm - tight for a probe, and doubling volts-per-turn doubles it.
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Design the p-B11 experiment around the 675 keV resonance: the fitted alpha yield coefficient A0 rises from 0.91 mb/sr at Ep=0.15 MeV to 218 mb/sr at 0.65 MeV - a factor of ~240 - so every keV of proton energy toward 650-675 keV multiplies count rate.
A0(0.15 MeV)=0.91 mb/sr; A0(0.30)=20.8; A0(0.49)=114; A0(0.65)=218 mb/srSource quote & editorial note
0.15 0.91 +/- 0.015... 0.65 218.42 +/- 0.55
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 360
Editorial note, tabletop extrapolation: The master rate table for the reference machine's PIPS window (150-675 keV) - as fitted A0 coefficients: a count-rate prediction folds in the angular terms, solid angle, target thickness and integration time (the experiments-by-energy arithmetic). What the table quantifies exactly is what reaching the resonance is worth: ~240x in A0 from 150 to 650 keV.
Cited in: Experiments by Energy Band
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Size an electrostatic deflector from Vd/d = (2T/e) * dR/(R(R+dR)): peeling a 0.472 MeV proton beam from R = 4 in to 4.5 in with a 0.291-in channel requires ~32.5 kV on the electrode.
Vd/d = (2T/e)*dR/(R*(R+dR)); the slide states Vd = 32.531 kV for B = 0.976 T, T = 0.472 MeV, d = 0.291 in - which this formula with these inputs does not reproduce (~7.6 kV); discrepancy flagged for scan re-read [2026-08-25] - use the formula with your own geometry and verify on the benchSource quote & editorial note
Vd = 32.531 kV
Editorial note, tabletop extrapolation: Gives the builder the extraction-voltage scale for a next machine: deflector voltage scales linearly with beam energy at fixed geometry, so a ~100 keV beam needs about a fifth of a 472 keV machine's figure in the same channel. Given the source's formula/number discrepancy (see formula field), size from the formula and confirm by measurement.
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In fixed-frequency magnet scans expect harmonic beam peaks at fields near B/n for odd n (f_RF = n*f_c; the ion completes one turn in n RF periods) - Houghton labelled peaks H+/3, H+/5, H+/7, H2+/9 - so label every peak with a species-and-harmonic hypothesis before claiming fundamental beam.
resonance at B/n, n odd for the two-gap geometry; f_RF = n*f_cSource quote & editorial note
H2+/9 H+/7 H+/5 H+/3 H+ H2+
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 15-18
Editorial note, tabletop extrapolation: Prevents misidentifying beam in the reference machine's B-field sweeps: a peak at one-third the expected field is a CANDIDATE for the same ion on the 3rd harmonic - confirm by species diagnostics or scaling tests, since another species/harmonic combination can land at the same field.
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Fusion rate climbed steeply with grid voltage in the thesis's runs - their sweep: 10 cpm at -16 kV rising through 60 cpm at -25 kV (the quoted point) to 130 cpm at -31 kV, at 13-18 mTorr and ~10 mA - roughly 13x for a 2x voltage increase.
BF3 moderated counter: 16 kV -> 10 cpm; 25 kV -> 60-100 cpm; 31 kV -> 130 cpmSource quote & editorial note
At -25 kV, 8 mA, and 16 mtorr, neutron levels were 60 cpm. This measurement confirmed that nuclear fusion was achieved.
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 45-46
Editorial note, tabletop extrapolation: The same lesson as the p-B11 cross-section curves: sub-barrier yield rises steeply with particle energy, so extra beam energy buys far more counts than the same fractional increase in current. The specific sweep numbers are one fusor's; the steepness is the physics.
Cited in: Experiments by Energy Band
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Neutron yield in Hull's fusor line climbed steeply with drive voltage: the 22 kV supply gave 1e3 n/s, 33 kV gave 1e5 n/s - a hundredfold - and his current machine, on a larger supply, exceeds 6e5 n/s; his investment order is voltage, vacuum cleanliness, and gas handling first.
22 kV -> 1e3 n/s; 33 kV -> 1e5 n/s; current machine > 6e5 n/s (that machine's supply voltage: scan re-read queued)Source quote & editorial note
It was limited to low level output by its 22kv internal supply. 103 n/sec... a 33 kilovolt supply. 105 n/sec... currently produces in excess of 600,000 neutrons per second
Hull, Fusor: An Easy to Construct Fusion Reactor Based on Inertial Electrostatic Confinement (2009) — p. 36-39
Editorial note, tabletop extrapolation: Reinforces energy-over-current for the builder: sub-Coulomb-barrier reaction rates reward every extra keV steeply - though not by a fixed orders-per-10-kV law; Hull's own steps differ between jumps.
Cited in: Experiments by Energy Band
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Recognize the phase-slip failure signature: once the accumulated phase difference passes pi/2 (in the standard convention) an ion stops gaining at the gap, then loses energy and spirals inward - so a beam that slips out of phase before full radius shows current dropping suddenly to near zero beyond whatever radius the ions reach.
phase difference > pi/2 -> deceleration; beam current collapses beyond that radiusSource quote & editorial note
If many ions in the beam fall out of phase before reaching maximum Dee radius, the beam current will drop suddenly to near zero beyond whatever radius the ions tend to reach
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 28, 57
Editorial note, tabletop extrapolation: Diagnostic direction, not verdict: a sharp cutoff in the radial current profile is CONSISTENT with phase slip - and also with aperture interception, wall collisions or vertical-envelope loss - so discriminate by what moves it: RF frequency and dee-voltage changes shift a phase-slip radius, mechanical interception does not, and field trim tells its own story.
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Identify beam species candidates by sweeping magnet current at fixed RF: resonances appear at the fundamental and at odd RF harmonics (B, B/3, B/5 for a given species), so H+, H2+ and He+ each show up several times in a magnet scan - a cheap first-pass mass spectrometer for the internal beam.
f_RF = h*q*B/(2*pi*m), h odd for a two-dee geometry -> resonant fields B_h = 2*pi*m*f_RF/(h*q); e.g. He+ at h=3, 3.68 MHz -> ~0.32 TSource quote & editorial note
for a fixed frequency f, resonances will occur for lower magnetic fields, e.g. B/3 and B/5, corresponding to an odd multiple of a lower frequency
Editorial note, tabletop extrapolation: Practical commissioning technique: a magnet-current sweep plus an electrometer assigns candidate species/harmonic pairs to each peak. Confirming that a peak is really protons (and clean) still needs field calibration and, where purity matters, an independent species check.
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The circulating beam is not continuous: frame-by-frame analysis on this machine showed ions populating about 40 degrees of the 360-degree RF cycle - implying peak current roughly ninefold above average IF the bunch is near-uniform (the rectangular estimate).
bunch width ~40 deg of RF cycleSource quote & editorial note
Frame-by-frame analysis... revealed that ions nominally populate 40 degrees of the 360 degree RF cycle in our cyclotron.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 9
Editorial note, tabletop extrapolation: Sets expectations for fast diagnostics and duty-factor arithmetic on any machine: measure your own bunch width (capacitive pickup, gated counting) and use it - 40 degrees is one measured machine's figure, not a constant.
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In the cited apparatus, the stray magnetic field over the target effectively prevented secondary-electron escape, so the (ebonite-insulated) target's microammeter read the true ion current - magnetic suppression plus insulation is the pattern.
Source quote & editorial note
The stray magnetic field over T effectively prevents the escape of secondary electrons, so that the current measured is the true ion current.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 262
Editorial note, tabletop extrapolation: The reference machine's internal Faraday cup may get partial secondary suppression free from the fringe field - VERIFY it: sweep a suppressor bias and look for a current plateau, or compare with/without a suppressor electrode; outside the field an explicit suppressor is mandatory. Insulation isolates the signal but does not suppress emission.
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For alpha counting close to a target, the source used a thin mica window 1 cm in DIAMETER on a minimal-shadow grid, achieving a solid angle of approximately 0.7 - and calibrated absorber stack and dead space against a known polonium alpha source (range 3.80 cm air at 15 C, 760 mm).
window 1 cm diameter, solid angle ~0.7 sr in the reported geometry (a ~1 cm-class standoff is a derived estimate, not the quoted dimension); Po alpha range reference 3.80 cmSource quote & editorial note
a mica window W, 1 cm in diameter and supported on a grid which subtends the smallest possible area... The solid angle obtained in this way is approximately 0.7.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 262-265
Editorial note, tabletop extrapolation: The close-geometry, calibrate-with-a-known-alpha-source method is how the builder should commission the PIPS geometry before hunting p-B11 alphas - an analogous procedure, with a traceable sealed source, the PIPS dead layer in the accounting, and the solid angle computed for the actual geometry.
Cited in: Experiments by Energy Band
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Measure the beam's vertical envelope with insertable probes: the historical technique measured the width of the region of induced radioactivity on the leading edge of probes inserted to different radial locations.
Source quote & editorial note
One technique has been to measure the width of the region of induced radioactivity on the leading edge of probes inserted to different radial locations.
Livingston & Blewett, Particle Accelerators (1962) — p. 174-167
Editorial note, tabletop extrapolation: A radial probe (the reference machine's shielded Faraday cup on a linear feedthrough) is the workhorse diagnostic: falling collected current at some radius localizes WHERE the beam is lost - field shape, phase slip, focusing, apertures and probe interception then get tested separately as causes. At sub-activation energies, beam marks or a phosphor coat replace the activation-width trick.
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For absolute field calibration use proton NMR: B(gauss) = (234.82 +/- 0.13) x f(MHz) - the source's measured coefficient; Hall probes of its era were ~1% devices, and search-coil fluxmeters are relative instruments.
B[G] = 234.82*f[MHz]; worked example: 5.9 kG <-> 25.1 MHz proton NMRSource quote & editorial note
The frequency for resonance can be measured and reduced to magnetic field through the relation B = (234.82 +/- 0.13)f where B is in gauss and f is in megacycles per second.
Livingston & Blewett, Particle Accelerators (1962) — p. 286-287
Editorial note, tabletop extrapolation: 5.9 kG sits at 25.1 MHz proton NMR - an accessible DIY measurement. Modern calibrated Hall systems can do far better than the era's 1%, so use each instrument's actual spec; and the machine's own resonant frequency gives an orbit-averaged field cross-check whose accuracy is set by how well f, harmonic and species are pinned - budget it, don't assume half a percent.
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Benchmark resolution with a pulser: pulser line width should be about 5 keV narrower than the alpha resolution (warranted 11 keV FWHM here), and system noise is about 3 times the pulser FWHM.
FWHM_pulser ~ FWHM_alpha - 5 keV; noise ~ 3 * FWHM_pulser; certificates: electronic 5.5-5.6 keV, alpha 10.9-11.0 keV FWHM (241Am 5486 keV, 0.5 us shaping)Source quote & editorial note
Pulser line width should be about 5 keV (FWHM) narrower than Alpha Resolution ... the noise level which is approximately 3 times the pulser line width (FWHM).
Canberra, PIPS Detector Instruction Sheet (2012) — p. 1-3
Editorial note, tabletop extrapolation: A pulser check exercises the whole electronic chain and baseline - including grounding, 9 MHz RF pickup, and detector leakage/capacitance contributions while connected - without risking source contamination; isolating charge-collection or detector-response degradation still needs a real particle peak for comparison.
Cited in: Experiments by Energy Band
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Put a negatively biased retarding grid in front of the Faraday cup - potentiometer-adjustable - to drive secondary electrons back into the cup and read true beam current.
Source quote & editorial note
A retarding grid attached to the front of the Faraday cup will eliminate loss of secondary electrons... The grid will be at some negative potential.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 24
Editorial note, tabletop extrapolation: The better-engineered cousin of the simple cup bias (cf. dg-523's cited 9 V machine result): make the grid voltage adjustable and find the suppression plateau experimentally - the plateau, not any particular voltage, is the evidence - while checking what the grid itself intercepts.
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Find the beam by rocking either RF frequency or magnet current back and forth until a current peak shows on the target probe, with the probe pushed in closer to the center to facilitate locating the resonance.
Source quote & editorial note
either one rocked back and forth until a current peak is indicated on the target probe. The probe may be pushed in closer to the center to facilitate locating this resonance.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 11
Editorial note, tabletop extrapolation: Directly applicable commissioning move; starting the search at small radius makes the resonance easier to find. Once a peak is found, walking the probe outward while re-optimizing source and RF settings is the natural continuation - standard practice, though beyond this quote.
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Authenticate a beam by the sharpness of the current peak versus RF tuning and magnet current and by its sensitivity to hydrogen pressure.
Source quote & editorial note
the authenticity of the beam should be checked by the sharpness of resonance as a function of r.f. tuning and magnet current, as well as by its sensitivity to hydrogen gas pressure
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 11
Editorial note, tabletop extrapolation: Directly applicable: a 'beam' that stays constant while you detune B or RF is background until proven otherwise - candidates include ion leakage to the probe, RF pickup, dark current and secondary-electron paths - so diagnose it rather than count it.
-
Give the target probe a high resistance to ground and protect its meter with RF chokes and bypasses; for scale, the report's six-inch cyclotron indicated a 7 uA beam at a frequency corresponding to about 800 kv protons.
6-inch machine: ~7 uA internal beamSource quote & editorial note
The six-inch cyclotron has indicated a 7 microampere beam, at a frequency corresponding to about 800 kv protons.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 11
Editorial note, tabletop extrapolation: The choke-protected, well-insulated probe is the right pickup design. Treat the 7 uA as one historical machine's result, not an expectation: beam current rides on source, vacuum, RF voltage and capture, and tabletop machines have commissioned at picoamps.
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For final proof of acceleration use a nuclear signature: fuse LiF onto a stainless probe tip and look for prompt gammas from proton bombardment of Li and F.
LiF target fused on stainless block; p+Li / p+F gamma emissionSource quote & editorial note
a convenient target substance would be LiF which, when bombarded with protons, will emit gammas from Li ... The target may be prepared by simply fusing a small amount of LiF onto a small stainless steel block
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 11
Editorial note, tabletop extrapolation: Partially applicable: 7Li(p,gamma)8Be is exothermic - there is no threshold - but its prominent resonance near Ep = 441 keV is what makes the signal jump, so at the reference machine's ~150 keV the yield is far down the tail. A next machine near 0.5 MeV could use exactly this check; estimate thick-target yield and detector response first, and remember LiF adds fluorine channels (19F(p,alpha-gamma) with its own strong resonances).
Cited in: Experiments by Energy Band
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Sub-resonance p-B11 measurements were made with only 0.5-10 nA of protons on target (with ~60-70 keV beam energy resolution); the paper's setup - small-solid-angle detectors, thin targets - produced usable alpha spectroscopy at that current.
0.5-10 nA on target for Ep = 0.15-0.4 MeV data; 100-200 nA at higher energiesSource quote & editorial note
At these energies beam intensities varied from 0.5 to 10 nA on target and beam resolution varied from approximately 60 to 70 keV.
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 359
Editorial note, tabletop extrapolation: The single most encouraging number in the batch: professional low-energy p-B11 data at exactly the reference machine's nA beam scale. Whether nA suffices for a given measurement follows from the rate arithmetic - cross-section, solid angle, integration time (the experiments-by-energy worked examples) - not from precedent alone.
Cited in: Experiments by Energy Band
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Report p-B11 yields as alphas detected per luminosity (counts/(Nt*Np*dOmega)), not as a cross section: the number of alphas per reaction contributing to the main peak is energy-dependent - the paper's simulation puts ~2.1 in the peak at the 675 keV resonance.
X = Counts/(Nt*Np*dOmega) [cm2/sr]; simulated multiplicity in the dominant peak: ~2.1 at the 0.675 MeV resonance (energy- and window-specific)Source quote & editorial note
simulations show that out of the three emitted a-particles, on average 2.1 a-particles contribute to this peak at the 0.675 MeV resonance
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 359-360
Editorial note, tabletop extrapolation: When the builder converts PIPS counts, publish counts-per-luminosity as this paper does. Extracting a cross section needs more than dividing by ~2: detector efficiency, angular acceptance, the alphas' angular/energy distributions and window effects all enter, and the multiplicity itself changes with beam energy and analysis window.
Cited in: Experiments by Energy Band
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Calibrate each detector's relative solid angle with low-energy Rutherford scattering on gold plus a known Am-241 alpha source, as the cited experiment did.
relative solid-angle calibration: Rutherford on Au + 241Am sourceSource quote & editorial note
The relative solid angles for each detector were measured using low energy Rutherford scattering on gold as well as a known 241Am source.
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 360
Editorial note, tabletop extrapolation: The builder already owns the pieces: an Am-241 check source exercises the PIPS geometry and energy scale in practice, and the Faraday cup/Keithley 617 integrates charge for yield normalization - noting that ABSOLUTE calibration needs certified source activity, controlled geometry and live-time accounting, and a single alpha line is a one-point energy check.
Cited in: Experiments by Energy Band
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Rutgers' deflector-geometry formula predicted a full energy spread dT = 25.46 keV on a ~0.5 MeV beam; the phosphor-screen spot - approximately half the beam - measured 13.3 keV across it, matching the predicted half-spread dT/2 = 12.73 keV.
dT = (V*R^2/d) * (2*eps_r*dR/(R^2 - eps_r^2)) form per source slide; predicted dT = 25.46 keV full, dT/2 = 12.73 keV vs 13.3 keV measured across the visible half-spotSource quote & editorial note
Predicted dT=25.46 kV ... (Approx half beam spot) ... energy at far left: T=.5087 MeV ... energy at far right: T=.4954 MeV ... dT=13.3 keV ... Theory: dT/2=12.73 keV
Editorial note, tabletop extrapolation: A phosphor screen plus this formula gave a student-machine energy-spread estimate without a spectrometer - as an apparatus-specific check: spot width also carries emittance, coherent radial motion and screen resolution, so deconvolve or bound those before quoting a spread from a screen.
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Put the discharge/beam current meter in the grounded return leg of the HV supply (e.g., at a center-tapped transformer case) so the ammeter sits at ground potential; include a 10 megohm bleeder and wait 2 minutes after shutdown.
ammeter in ground return; 10 MOhm bleeder; 100 uA meter movements with shunts/series resistorsSource quote & editorial note
The location of the ammeter in the circuit keeps it essentially at ground potential... CAUTION! This supply is lethal. Allow at least 2 minutes after shutdown before touching any connections. Make sure that the voltmeter reads zero. Do not omit the 10 meg bleeder resistor.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 8
Editorial note, tabletop extrapolation: The ground-leg metering trick lets the builder log arc and extraction currents on the next machine without floating instruments at kilovolts - the meter still needs protection (shunt, series resistance, clamping) against fault transients. On shutdown, the source's voltmeter-zero check is the load-bearing step: the 2-minute wait is a floor that depends on the actual RC of supply and bleeder, and zero on the meter - then a shorting stick - is what proves it.
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Bias the beam collector to suppress secondary-electron emission - ion impact ejects electrons whose escape reads as extra current, and in the cited machine a 9 V bias measurably lowered (i.e. corrected) the reading.
cited machine: 9 V collector biasSource quote & editorial note
When ions collide with the current collector, they can cause electrons to be ejected. This results in an additional current to that caused by the ion beam itself. ... The beam current measured was lower with the addition of the voltage bias... the bias reduces the emission of secondary electrons, resulting in a more accurate measurement.
Editorial note, tabletop extrapolation: A one-component fix for honest current numbers on any Faraday-cup measurement the builder makes: apply the bias and sweep its magnitude until the reading plateaus - the plateau, not any particular voltage, is the evidence that suppression is complete.
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Bias the internal target/Faraday collector (Houghton: +9 V from a battery) when measuring beam current to reduce the effect of secondary electrons leaving the target, which are created in significant numbers.
+9 V (battery) bias on target vs grounded target comparisonSource quote & editorial note
A +9 V bias can be applied to the target using a battery to reduce the effect of secondary electrons on beam current measurements ... secondary electrons are created in significant numbers on the target.
Editorial note, tabletop extrapolation: One battery attacks the main systematic in the builder's main diagnostic, and the biased/unbiased comparison sizes the secondary contribution - verify the suppression is sufficient by stepping the bias and looking for a current plateau; energetic secondaries and backscatter can survive +9 V.
Cited in: Experiments by Energy Band
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Accept that the honest headline number for a small machine is small: Houghton's best was ~0.1 uA at a B/3 resonance (the paper's figure), and 3 pA at the highest proton energy reached - 160 keV at 796 mT and 12.1 MHz; the paper names more magnet current, cooling and RF frequency as what higher energy would take.
0.1 uA best (B/3 resonance); 3 pA at 160 keV, 796 mT, 12.1 MHz; 400 keV theoretical needs more magnet current, cooling, and higher RF frequencySource quote & editorial note
The highest proton energy obtained so far is about 160 keV, with a 3 pA peak near the correct magnetic field of 796 mT for 12.1 MHz.
Editorial note, tabletop extrapolation: Calibrates expectations exactly at the reference machine's operating point (~150 keV): currents fall steeply near a machine's energy limit, and the gating items the paper lists are the ordinary ones - magnet current, cooling, RF range.
Cited in: Choosing Your Machine
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Take multi-kW beams on grazing-incidence water-cooled targets so the power spreads over a long footprint: the 86-inch ran 500 uA of 23 MeV protons (11.5 kW) steadily on a 6 x 10 inch aluminum grazing target, and its highest calorimetrically stabilized point was 41.7 kW.
grazing incidence spreads P_beam over ~L/sin(theta) (theta to the target surface); steady 500 uA x 23 MeV = 11.5 kW; highest stabilized calorimetric point 41.7 kWSource quote & editorial note
operating steadily for some time with 500 ua of 23 Mev protons on a 6 by 10 inch water-cooled aluminum target of the grazing-incidence type ... The highest level at which operation was stabilized long enough to permit calorimetric measurement gave a beam power of 41.7 kw.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 24
Editorial note, tabletop extrapolation: Overkill at the reference machine's ~mW beam power, but the geometry trick transfers if a next machine ever puts tens of watts on a probe tip: tilt the target - and still do the cooling and stress arithmetic, since grazing only enlarges the footprint.
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Use a rotating multi-faced target (three faces at 45 degrees, each with a 1.2 cm x 1 mm recess for pressed powder) on a water-cooled stem so faces are shielded from each other's sputtering and targets can be compared without breaking vacuum or alignment.
3 faces at 45 deg; recess 1.2 cm dia x 1 mm deep; water-cooled rotating stemSource quote & editorial note
This is of steel and has three faces at 45 deg to the axis, which form a sort of truncated pyramid with a circular base. Each face bears a recess, 1.2 cm. in diameter and about 1 mm. deep. The metal or powder to be bombarded is pressed or hammered into these spaces and the beam strikes the surface which is uppermost. The target is carried on a water-cooled stem M which rotates in a ground joint and can be set so as to bring any one of the three faces into the beam. By having only three faces any one face is completely shielded from the material sputtered from that which is in the beam, and at the same time it is possible to make very rapid comparisons between various targets
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 262
Editorial note, tabletop extrapolation: A boron target plus a blank plus a calibration face on one rotatable holder would let the builder switch targets and measure background without venting.
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Pump the chamber for 10-15 minutes before applying detector bias to drive off surface moisture, then wait about 30 seconds after biasing for the detector to stabilize.
Source quote & editorial note
it is a good idea to evacuate the chamber for 10 to 15 minutes before applying bias. This will remove excess surface moisture ... It is recommended to wait 30 seconds to stabilise the detector.
Canberra, PIPS Detector Instruction Sheet (2012) — p. 1
Editorial note, tabletop extrapolation: Build the pump-first-then-bias order into the beam-diagnostics routine as a TIMED permissive (vacuum reached plus 10-15 min), not a bare pressure interlock, and keep the 30 s post-bias stabilization; moisture raises initial leakage current, which is reason enough for the discipline.
Cited in: Experiments by Energy Band
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Clean a PIPS face by first blowing dry air or N2 on the surface (to remove particles that could scratch), then swabbing with high-quality isopropyl alcohol - never methyl alcohol - and dry under vacuum 15 minutes or at 50 C for an hour before re-biasing. Cleaning may reduce contamination-related surface leakage but will not reverse bulk radiation damage.
Source quote & editorial note
PIPS detectors have an ion implanted entrance window of about 500 A thickness. ... To clean standard PIPS detectors first blow dry air or N2 gas on the surface to remove particles that might cause scratches ... use a cotton ball dampened with a good quality isopropyl alcohol; Do not use methyl alcohol ... put under vacuum for 15 minutes or heat to 50 C for an hour to remove residual moisture before applying bias.
Canberra, PIPS Detector Instruction Sheet (2012) — p. 1
Editorial note, tabletop extrapolation: The ~500-angstrom implanted window (the manual's figure) scratches easily; in a chamber with pump oil and target debris, stick to the manual's procedure.
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Use leakage current as the detector health metric: compare against the individual detector's certificate value at the same bias, corrected for temperature - leakage doubles for roughly every 5 C rise.
I_leak(T) ~ I_leak(T_ref) * 2^((T-T_ref)/5); reference value and bias from the detector's own certificateSource quote & editorial note
Remember that leakage current doubles for about 5 C rise in temperature and take this into account when you compare your measurement to that of the factory.
Canberra, PIPS Detector Instruction Sheet (2012) — p. 1-3
Editorial note, tabletop extrapolation: A detector near warm cyclotron hardware can legitimately read several times its certificate value. Before blaming radiation damage or contamination, walk the checklist: temperature, bias setting, light leaks, humidity, cabling and connectors, microdischarge - the doubling rule is an approximation, not a diagnosis.
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Operate the BKPD 50-11-500 PIPS at its recommended +130 V bias (full depletion +110 V) and never exceed the +150 V maximum bias.
V_rec = +130 V; V_full_depletion = +110 V; V_max = +150 V; depletion 500 um, chip 501 um, 8000 ohm-cmSource quote & editorial note
Recommended bias voltage +130 Volts ... Full depletion bias voltage +110 Volts ... Maximum bias voltage +150 Volts
Canberra, PIPS Detector Instruction Sheet (2012) — p. 2-3
Editorial note, tabletop extrapolation: The reference machine's two detectors (S/N 98343/98344) have only 20 V of headroom above recommended bias; a supply glitch to 150+ V risks breakdown, so use a current-limited, capped supply.
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Match electronics speed to the detector: thin silicon detectors (10-300 um) deliver their charge in 100 ps to 30 ns per the source table, so microsecond-scale shaping integrates the full charge with negligible ballistic deficit for detectors in that class.
collection time: Si 10-300 um: 100 ps - 30 ns; thick (cm) Si/Ge: 1-10 usSource quote & editorial note
(10 ... 300 um thick): 100ps-30ns. Thick (~cm) Si or Ge detector: 1-10us
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 2
Editorial note, tabletop extrapolation: The reference machine's ~500 um PIPS sits above the quoted 10-300 um range - its collection time should still be tens of ns (verify from the datasheet or a rise-time measurement) - and shaping time is then chosen for noise TOGETHER WITH count rate, pile-up and pulse-height stability, not noise alone.
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Signal-to-noise degrades with total input capacitance (detector + cable + stray), and feedback cannot recover it - keep the preamp physically at the detector and minimize cable before the first amplification stage.
V_signal = Q/C_total; equivalent noise charge grows with C_total; S/N cannot be improved by feedbackSource quote & editorial note
S/N cannot be improved by feedback. This result is generally valid, i.e. it also holds for active integrators (charge-sensitive amplifiers).
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 24
Editorial note, tabletop extrapolation: For the builder: mount the preamp on the vacuum feedthrough, not at the far end of a coax run. Cable capacitance raises the series-noise term, and at alpha-spectroscopy resolutions it competes with detector leakage and shaping-time choices for the noise budget - short cable is the cheapest term to fix.
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Read out silicon detectors with a charge-sensitive (feedback-capacitor) preamplifier so gain is set by Cf and is insensitive to detector capacitance, which varies with bias voltage in a partially depleted diode.
Q_signal integrated on Cf; dVout/dQ = 1/Cf independent of C_detSource quote & editorial note
Detector capacitance may vary within a system or change with bias voltage (partially depleted semiconductor diode)... Amplifier output directly determined by signal charge, insensitive to detector capacitance
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 3-8
Editorial note, tabletop extrapolation: Confirms the standard PIPS chain for the p-B11 experiment: a charge-sensitive preamp at the feedthrough - the spectroscopy-grade choice, since a plain voltage amplifier's gain rides on the diode's bias-dependent capacitance. Voltage readout keeps niche uses (fast timing, very high rate) that energy spectroscopy is not.
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Estimate front-end noise of a CR-RC shaper from Qn^2 = 12*tau*IB + 6e5*tau/RP + 3.6e4*vn^2*C^2/tau (rms electrons; tau in ns, IB in nA, RP in kOhm, vn in nV/rtHz, C in pF); the optimum tau balances the capacitance (series) term against BOTH parallel terms: tau_opt = sqrt(3.6e4*vn^2*C^2 / (12*IB + 6e5/RP)). Converting to energy: 3.6 eV mean energy per electron-hole pair in silicon.
Qn^2 = 12 tau IB + 6e5 tau/RP + 3.6e4 vn^2 C^2/tau [rms e-]; tau_opt = sqrt(3.6e4 vn^2 C^2/(12 IB + 6e5/RP)); sigma_E = 3.6 eV * Qn, FWHM_elec = 2.355 sigma_E (Si)Source quote & editorial note
en2 = 12 tau IB + 6e5 tau/RP + 3.6e4 vn2 C2/tau [rms electrons]
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 42
Editorial note, tabletop extrapolation: Computes the expected electronic FWHM of the PIPS chain from datasheet numbers before buying a shaping amplifier, and says how tau should move if leakage rises - combine electronic, statistical and charge-collection terms in quadrature for the total resolution.
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Any particle that can transfer enough energy to displace a silicon atom (threshold of order 20 eV, direction-dependent) causes displacement damage; the source's characteristic estimate is that a 1 MeV neutron transfers about 60-70 keV to the Si recoil, which displaces roughly 1000 atoms in a ~0.1 um region - so neutron-producing runs age silicon detectors far faster than the machine's X-ray background.
displacement threshold ~20 eV (direction-dependent); 1 MeV n -> ~60-70 keV recoil (source's characteristic value; elastic recoils range 0-133 keV) -> ~1000 displaced atomsSource quote & editorial note
a 1 MeV neutron transfers about 60 to 70 keV to the Si recoil atom, which in turn displaces roughly 1000 additional atoms in a region of about 0.1 um size.
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 49
Editorial note, tabletop extrapolation: The reference machine's PIPS detectors tolerate its X-ray background as far as displacement damage goes (ionizing/surface effects are a separate, slower concern), but shield or retract them during any neutron-producing run - deuterium work above all - and budget by estimated neutron fluence at the detector, not just by whether the reaction label says neutrons.
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Radiation-induced leakage current grows linearly with fluence, dI = alpha*Phi*(A*d), with alpha ~2e-17 A/cm for 1 MeV neutrons (3e-17 for 650 MeV protons) at room temperature.
dI = alpha * Phi * A * d; alpha(1 MeV n) = 2e-17 A/cm, alpha(650 MeV p) = 3e-17 A/cmSource quote & editorial note
For 650 MeV protons alpha = 3e-17 A/cm, 1 MeV neutrons alpha = 2e-17 A/cm.
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 51-52
Editorial note, tabletop extrapolation: Track the PIPS bias current on the Keithley 617 as a damage INDICATOR: an unexplained, temperature-corrected secular rise warrants investigating beam or neutron exposure - after ruling out temperature (leakage roughly doubles per ~7 C), humidity/surface leakage and annealing history; raw current is not a calibrated dosimeter.
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Silicon detector reverse-bias (leakage) current is steeply temperature dependent: cooling from room temperature to 0 C typically cuts it to about one-sixth.
I(0 C) ~ I(20 C)/6; activation energy ~1.2 eV (irradiated), 1.15 eV (unirradiated)Source quote & editorial note
Cooling to 0 C typically reduces the reverse bias current to 1/6 of its value at room temperature.
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 52
Editorial note, tabletop extrapolation: A Peltier or cold-finger on the PIPS mount is a cheap resolution upgrade WHEN leakage-current shot noise dominates the noise budget - verify that first, control condensation and temperature stability, and remember cooling does not repair irradiation-induced charge-trapping losses.
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Near 200 keV bombarding energy, the two main p-B11 alphas emerge 150-180 degrees apart with the third particle taking very little energy - a coincidence pair of back-to-back PIPS detectors is a powerful signature at the reference machine's energies.
alpha-alpha opening angle 150-180 deg at Ep ~200 keVSource quote & editorial note
the common mode of disintegration is into two [alpha] particles which proceed at angles of 150 to 180 relatively to one another, the third particle receiving very little energy
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 357-358
Editorial note, tabletop extrapolation: Two PIPS detectors in near-back-to-back coincidence would give the builder a background-crushing p-B11 signature even at very low count rates.
Cited in: Experiments by Energy Band
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Near the 675 keV resonance of 11B(p,alpha), the measured alpha angular distribution is nearly isotropic (|A1|,|A2| a few percent of A0 in the cited coefficients), while the 2.64 MeV resonance shows visible anisotropy.
at 0.65 MeV: A0=218.4, A1=-3.2, A2=6.3 mb/sr (isotropic to ~3%)Source quote & editorial note
While the resonance at 0.675 MeV exhibits isotropy, anisotropy can be seen for the resonance at 2.64 MeV
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 358-360
Editorial note, tabletop extrapolation: For yield measurements NEAR the 675 keV resonance, detector angle costs only a few percent, so geometry and shielding can drive PIPS placement - at other beam energies get angular-distribution data or carry an anisotropy uncertainty, and remember angle still affects kinematic acceptance and scattered-particle background.
Cited in: Experiments by Energy Band
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Silicon detectors for p-B11 alphas, as fielded in the cited experiment: eight detectors at 30-160 degrees, 16.5 cm from the target, ~2.5e-4 sr each, thick enough to stop the alphas at all energies; their spectra show a large elastically-scattered-proton peak (just below 1 MeV at the cited beam energies) alongside the alpha peaks.
cited setup: 8 detectors at 30-160 deg, r = 16.5 cm, dOmega ~ 2.5e-4 sr each; elastic-proton peak position follows beam energy and angleSource quote & editorial note
The detectors were located 16.5 cm from the target ... 60, 75, 90, 115, 135, and 160 [degrees], with each detector subtending a solid angle of approximately 2.5 x 10-4 sr. ... The large peak just below 1 MeV is produced by elastically scattered protons
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 358-360
Editorial note, tabletop extrapolation: Expect the PIPS spectra to carry a scattered-proton peak wherever two-body kinematics puts it for the actual beam energy and detector angle - compute that first, then set the alpha window or choose an absorber; a proton-stopping foil also costs the alphas energy and straggling, so evaluate it with stopping-power numbers before committing.
Cited in: Experiments by Energy Band
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The cited experiment's p-B11 target: 56 +/- 2 ug/cm2 of isotopically pure 11B on a 9 ug/cm2 carbon backing, thickness measured two independent ways - via the known elastic/Rutherford cross-section ratio for alphas at 4.86 MeV and 165 deg, and via the energy-broadening of the elastic peak - agreeing to a 3.6 percent systematic uncertainty in yields.
target 56 +/- 2 ug/cm2 11B on 9 ug/cm2 C; thickness via elastic alpha scattering at 165 deg, 4.86 MeVSource quote & editorial note
the target, which was composed of 56 +/- 2 ug/cm2 of isotopically pure 11B deposited on a 9 ug/cm2 carbon backing. Target thickness was measured using elastically scattered a-particles at 4.86 MeV, where the ratio of the elastic scattering cross section to the purely electromagnetic Rutherford cross section is known at a scattering angle of 165 deg. This measurement provided two independent measures of the target thickness via the known cross section and via the energy loss as measured by the broadening of the elastic peak. Analyses of both results agree and provide a target thickness of 56 +/- 2 ug/cm2 leading to a 3.6% systematic uncertainty in our yields.
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 360
Editorial note, tabletop extrapolation: Defines 'thin' for the reference machine's boron target (tens of ug/cm2) and gives two thickness checks performable with their own detectors - reproducing the alpha-scattering one requires the stated alpha energy and angle where the ratio to Rutherford is known, plus calibrated fluence and solid angle.
Cited in: Experiments by Energy Band
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In the thesis's IEC context D-D fusion technically begins near 10 kV, but detectable fusion 'generally does not occur' below about 15 kV - their first clean counts came at -25 kV.
detectable onset (their setup): >= ~15 kV; first clean counts at -25 kVSource quote & editorial note
D-D fusion can occur in an IEC device at voltages as little as 10 kV or less, but detectable fusion generally does not occur until voltages are at least 15 kV
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 18
Editorial note, tabletop extrapolation: Calibrates expectations for any sub-threshold nuclear signal at home: being physically above a reaction threshold is not enough - the detectable onset sits well above it, and where it sits depends on geometry, gas pressure and loading, current, and the counting setup.
Cited in: Experiments by Energy Band · Shielding a Small Cyclotron
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For thermal-neutron activation or moderated counting in the cited setup, a 3.89 cm (~1.5 inch) HDPE layer gave the peak capture rate with the moderator as close to the source as possible; their activation chamber backed the silver target with a second HDPE layer.
HDPE moderator thickness ~3.89 cm for peak capture; Ag-108 t1/2 2.37 min activation targetSource quote & editorial note
a peak capture rate is obtained with a 3.89 cm layer of HDPE. This detection method involves positioning the HDPE as close to the neutron source as possible ... A piece of silver ... and its subsequent radioactive decay can be measured. An activation chamber was made HDPE with another layer behind the silver
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 23-24
Editorial note, tabletop extrapolation: If the builder cross-checks PIPS counting with activation or a moderated tube (e.g., for D-D work), start from the cited thickness but optimize for the actual geometry - a thickness scan or transport estimate - since the optimum moves with source spectrum and arrangement. Ag-108 (t1/2 2.37 min) remains the classic activation target.
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For amateur fusion work the source recommends D-D fuel, branching about 50:50 to T+p and 3He+n; in their account D-T brings licensing and tritium handling, and 3He is prohibitively expensive.
D+D -> T + p (~50%); D+D -> 3He + n (~50%)Source quote & editorial note
The amateur is limited to the middle or D-D reaction which yields a split 50:50 reaction D+D to T + Proton, D+D to He3 + neutron
Hull, Fusor: An Easy to Construct Fusion Reactor Based on Inertial Electrostatic Confinement (2009) — p. 19-20
Editorial note, tabletop extrapolation: The reference machine's p-B11 choice sidesteps this entirely. If deuterium ever runs in the cyclotron, D-D is the accessible fusion fuel in the source's US hobbyist-era framing - but licensing attaches by jurisdiction and by what the device produces (see /legal/), so verify locally rather than treating any fuel as license-free. The safety fact is the neutron branch: half of D-D reactions emit a 2.45 MeV neutron.
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Back up electronic neutron detection with a passive fast-neutron bubble detector; an independent, electronics-free integrating detector guards against RF/HV-induced false counts.
Source quote & editorial note
Fast neutron bubble detector acts as backup to electronic detection
Hull, Fusor: An Easy to Construct Fusion Reactor Based on Inertial Electrostatic Confinement (2009) — p. 43
Editorial note, tabletop extrapolation: Same philosophy for p-B11: pair the PIPS/electronics chain with a passive detector (e.g., CR-39 track plastic) immune to the cyclotron's RF pickup.
Cited in: Experiments by Energy Band
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Prevent stainless-on-stainless thread galling: lubricate the threads (anti-seize), tighten slowly (heat drives galling), avoid prevailing-torque locknuts, and pair materials of different hardness; once galling starts, continued tightening cold-welds the joint.
Source quote & editorial note
in severe cases, galling can completely weld the nut and bolt together and prevent removal of the fastener ... Thread lubrication is one of the most effective measures to lessen the potential for galling... Heat contributes significantly to thread galling. Installing a fastener generates heat and high-speed installation generates significantly more heat. ... Avoid prevailing torque locknuts. ... Mating parts of the same alloy have a greater tendency to gall than parts of dissimilar alloys having different degrees of hardness.
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 8
Editorial note, tabletop extrapolation: Every stainless-on-stainless bolt into the chamber flange gets anti-seize OUTSIDE the vacuum boundary; inside, any coating or lubricant must be separately qualified for vacuum service (silver plating is a common accelerator practice, but qualify it - Fastenal doesn't cover vacuum). One galled lid bolt can strand the whole chamber.
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Read arc damage patterns as diagnostics: pitting concentrated in the outline of the electrode (not underneath or on top) fingers edge-field breakdown at the electrode perimeter as the failure mode.
Source quote & editorial note
Pitting primarily in the outline of the electrode - not directly underneath or on top.
Editorial note, tabletop extrapolation: When the builder opens the chamber after sparking, pit geography is the first CLUE: perimeter concentration is consistent with edge-field enhancement (fix radii - dg-353), scattered pits with contamination or particulates (clean and re-condition). A lead to follow, confirmed by whether the fix actually moves the breakdown voltage.
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The Rutgers team coated their HV electrode with Aerodag G dry lubricant - conductive, with a low secondary-electron-emission coefficient - as part of their arc-fighting campaign, which also widened gaps by machining away nearby ground planes.
Source quote & editorial note
We coated the HV electrode with Aerodag G dry lubricant, which is also conductive and has low secondary electron emission coefficient.
Editorial note, tabletop extrapolation: A cheap surface treatment to try if a deflector or dee edge hits breakdown limits near the top of its range - one element of the Rutgers fixes, and their own account credits the cable-energy fix (dg-285) and staged resistance (dg-286) with the decisive difference, so treat the coating as a contributor, not a cure.
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The fusor doc's grid rule: make it from tantalum or tungsten wire, fusion- or resistance-welded - their experience: a silver-soldered joint fails fast under a discharge that keeps the electrode incandescent (their 0.024-in Ta grid replaced a 0.030-in stainless one that glowed red at ~120 W).
0.024 in Ta wire replaced 0.030 in SS; grid glowed red at 2 kV x 60 mA (120 W) at 40 micronsSource quote & editorial note
The grid should be made from tantalum or tungsten wire and be fusion or resistance welded.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 5-8
Editorial note, tabletop extrapolation: Applies in spirit to a next machine's chimney slits, puller edges and beam stops: anything the beam or arc dwells on gets a material-and-joint choice made against its actual power density. Refractory metal with welded joints is the robust default where cooling is absent; cooled copper or graphite are engineered alternatives (dg-426, dg-939).
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Provide thread engagement of about one nominal bolt diameter in conventional steel, and more when tapping soft materials; pair nuts and bolts by matching grade so the joint develops the bolt's strength.
length of engagement ~ 1.0*d in steel; longer in soft metals (calculate against thread stripping for the actual materials)Source quote & editorial note
With conventional steel nut and bolt materials, a length of engagement of about one nominal diameter of the bolt is typical. A longer thread length engagement will be needed when dealing with tapped holes in soft material.
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 14
Editorial note, tabletop extrapolation: Tapped holes in aluminum lids or pole pieces need substantially more engagement than steel - size them against thread-shear stripping for the actual alloy, or use inserts; a stripped hole in the finished chamber is far costlier than a longer bolt.
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Estimate tightening torque with T = K*d*F, F = 75% of proof load for standard joints, using the guide's K factors - 0.20-0.30 non-plated black, 0.17-0.22 zinc, 0.12-0.16 lubricated, 0.11-0.15 cadmium - and expect even a perfect torque wrench to scatter preload by 25-30%.
T = K*d*F; F = 0.75*proof load (standard); K per the guide's table: 0.20-0.30 non-plated, 0.17-0.22 zinc, 0.12-0.16 lubricated, 0.11-0.15 cadmium; preload scatter 25-30%Source quote & editorial note
Torque = K x d x F... F = 75% of bolt material proofload for standard bolts... even perfect input torque can give a variation of preload by as much as 25 - 30 %. ... K Factors: Bolt Condition - Non-plated, black finish: K 0.20 - 0.30; Zinc-plated: 0.17 - 0.22; Lubricated: 0.12 - 0.16; Cadmium-plated: 0.11 - 0.15
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 25-26
Editorial note, tabletop extrapolation: Gives defensible torque numbers for lid and magnet-clamp bolts once F is set from the joint design (gasket stress, flange stiffness, thread strength). The lubrication trap is the K ratio: a bolt lubricated to K~0.14 but torqued to a dry-table value assuming K~0.25 sees ~1.8x the intended preload - enough to yield or snap small fasteners.
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Do not trust torque values on reused fasteners: in the guide's test, a Grade 5 pair that needed 70 ft-lb for 9000 lb of clamp needed 145 ft-lb by the fourth installation - same torque table, half the clamp (the intermediate value and thread-load shares are the guide's further data - re-read queued).
thread load share: 1st ~35%, 2nd ~25%, 3rd ~18%; same-clamp-load torque drift example: 70 -> 95 -> 145 ft-lb over 4 installationsSource quote & editorial note
we used an installation torque of 70 ft-lbs to obtain a clamp load of 9000 lbs... By the fourth installation, we required 145 ft-lbs to reach a clamp load of 9000 lbs.
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 30
Editorial note, tabletop extrapolation: Lid bolts cycled dozens of times a year walk away from any torque table - in either direction, since reuse changes the friction coefficient unpredictably. For repeatable magnet-gap or flange clamping: set inspection/replacement criteria for the hardware, and validate preload by a joint-specific method (measured load, bolt elongation, or a calibrated procedure proven on THAT joint - turn-of-nut included only once shown repeatable on its compliance).
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Expect a serious commitment: Iowa State's project was 'long and laborious' and got first beam three years after starting, in spring 1957 (the start-year and team details are the article's: scan re-read queued).
3 years from start to first beamSource quote & editorial note
The project was a long and laborious one, but the efforts were well-rewarded when the first beam was obtained three years later, in the spring of 1957.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 3
Editorial note, tabletop extrapolation: Schedule reality check consistent with the census: documented start-to-first-beam gaps run one to six years (the builds page's computed spread), and Iowa State's three sits mid-pack.
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Budget realistically before scrounging: a modest small accelerator bought new costs ~$128k (vacuum ~$20k, RF ~$17k, instrumentation ~$41k, magnet ~$15.5k, chamber ~$14k, detectors ~$20k) - which is why surplus procurement is the core amateur skill.
new-price line items total ~$127.5k (the article's rounded '$128,500' headline; 2010 dollars)Source quote & editorial note
TOTAL: $128500. Who has >$125k to blow on a very modest strawman small particle accelerator?
Niell, Effective Scientific Equipment Procurement Strategies: Building on a Budget (2010) — p. 2-3
Editorial note, tabletop extrapolation: Calibrates a next machine's budget: every subsystem not scrounged or fabricated costs thousands new (the article's line items), which is why surplus procurement dominates documented amateur practice - the census's cost trail says the same.
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Buy surplus using a three-line envelope - hard cost cap, minimum performance spec, and required function/condition: the quoted example ($400 cap; measure 40 MHz sine waves; in calibration and nearly bombproof); the article's tour of vendor tiers is its own commentary (scan re-read queued).
Source quote & editorial note
Cost: Can spend no more than $400. Performance: Want to measure 40MHz sinewaves... Function: Must be in calibration, and nearly bombproof
Niell, Effective Scientific Equipment Procurement Strategies: Building on a Budget (2010) — p. 7-10
Editorial note, tabletop extrapolation: A disciplined method for the next machine's shopping list: define the B-field, vacuum and RF numbers first, then match each purchase to the cheapest vendor tier whose reliability that subsystem can tolerate - judged per purchase, not by a permanent vendor ranking.
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Meter homebuilt HV with a ~10,000:1 high-resistance divider string feeding a low-voltage panel meter - the quoted arrangement; the thesis's companion practices (high-resistance ballast against surges, oil-immersed transformer and diodes) are its own build (scan re-read queued).
divider ratio ~1:10,000; X-ray transformer + autotransformer, oil-immersed diodes and cap filterSource quote & editorial note
The voltage divider allowed use of a low voltage meter by tapping the divider string at a 10,000 part fraction of the total voltage drop.
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 18-19
Editorial note, tabletop extrapolation: Reusable for the reference machine's DC monitoring - extraction or supply voltage - with a divider rated for the voltage and power, in a fail-safe enclosure, and calibrated. NOT for the dee: a high-resistance DC divider on an RF resonator capacitively loads and detunes it, reads wrongly, can overheat, and can put RF onto the meter. Measure dee voltage with a calibrated capacitive pickup or an RF-rated probe. [Note revised 2026-08-23: earlier note offered the DC divider for 'dee/extraction HV monitoring' without distinguishing the two.]
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The source's scrounger supply: a current-limited neon-sign transformer (12 kV, 60 mA) with case center tap, rectified by microwave-oven diodes into a positive-ground supply; never apply full voltage immediately - bring it up slowly at a few mA.
NST 12 kV / 60 mA + 2x 12 kV MOT diodes, full-wave; positive terminal groundedSource quote & editorial note
One might choose a 12 kV, 60 mA neon sign transformer and use 2 - 12 kV microwave oven diodes... Never apply full voltage immediately to the fusor!
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 5-8
Editorial note, tabletop extrapolation: A scrounger-grade current-limited architecture for source-conditioning and glow-cleaning supplies. Current limiting makes faults survivable for the hardware, not the operator - 12 kV at 60 mA is far beyond lethal, so the full HV practice set applies (grounded case, bleeder, voltmeter-zero, shorting stick; dg-522). Check diode ratings against the topology: in a center-tapped full-wave circuit each diode blocks about twice the half-winding peak - around 17 kV here - so single 12 kV parts are marginal; stack diodes in series per leg.
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Expect and monitor for X-rays once electrode voltages exceed about 20 kV - the source's hazard line for fusor/accelerator work, whose own chamber surveys detected X-rays from 18 kV - with a zero-personnel-exposure goal.
X-ray hazard line ~20 kV on electrodes (source's figure; bremsstrahlung exists below it)Source quote & editorial note
At voltages greater than 20 kV, the resulting x-rays can be hazardous. ... Radiation surveys of the chamber showed the presence of x-ray radiation at voltages exceeding 18 kV.
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 14, 25, 45
Editorial note, tabletop extrapolation: The reference machine's dee/extraction voltages sit below this line today, but HV conditioning or a higher-voltage upgrade crosses it. Monitor with an instrument that actually responds at 15-25 keV - a thin-window GM or scintillation survey meter; a standard thick-walled GM tube under-reads soft X-rays - and remember the viewport is one weak point among several (feedthroughs and thin walls count too).
Cited in: Choosing Your Machine · Shielding a Small Cyclotron
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Hull's fusor line: at his machine's level - in excess of 600,000 D-D neutrons per second - both light neutron shielding and X-ray shielding become needed for further increases; his planned next machine incorporates them.
Hull's shielding line: ~6e5 n/s (D-D, 2.45 MeV) on his machine and occupancySource quote & editorial note
currently produces in excess of 600,000 neutrons per second which allows some low level neutron activation work of short lived isotopes. Both light neutron and x-ray shielding are needed beyond this level and the planned fusor V will incorporate these upgrades.
Hull, Fusor: An Easy to Construct Fusion Reactor Based on Inertial Electrostatic Confinement (2009) — p. 39
Editorial note, tabletop extrapolation: One experienced builder's numeric line for when a home device graduates from monitored to shielded - specific to his output, geometry and occupancy, not a universal threshold: dose scales with distance, time and moderation, so a measured survey decides the actual case. p-B11 alpha work produces no comparable neutron source term.
Cited in: Shielding a Small Cyclotron
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In a classical (azimuthally symmetric) cyclotron, keep the field-decay index n between 0 and 1 at all working radii; only then are both radial and axial motion stable, with tunes Qr = sqrt(1-n) and Qz = sqrt(n).
0 < n < 1; n = -(dB/dr)(r/B); Qr = sqrt(1-n), Qz = sqrt(n)Source quote & editorial note
The axial focusing, as shown above, takes place for any positive values of the field decay exponent. Therefore, orbital stability in both directions takes place only for 0 < n < 1.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 18-20
Editorial note, tabletop extrapolation: The governing stability rule for the weak-focusing reference machine: check the FEMM-derived B(r) for 0 < n < 1 over the working radii. Two refinements: n tends to zero at the machine center by symmetry, so the requirement bites from the first working orbits outward; and the value n takes is the designer's shaping choice - weak-focusing machines run it small at inner radii, rising toward extraction.
Cited in: Beam Dynamics: An Interactive Laboratory
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Analyze all betatron resonances of order below 4 (plus any structure resonance whose order equals the sector number); the Qr = 1 resonance near the center is survivable only because it is crossed in 1-3 turns with no large first-harmonic field error.
check |nr|*Qr + |nz|*Qz = k for order |nr|+|nz| < 4; cross Qr = 1 in 1-3 turns with small B1Source quote & editorial note
its passage without noticeable losses of particles becomes possible only due to the fact that the beam crosses it for 1-3 revolutions, and the first harmonic of the magnetic field with a large amplitude is absent
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 37
Editorial note, tabletop extrapolation: In the reference machine Qr = sqrt(1-n) sits just below 1 everywhere, so first-harmonic field symmetry is the load-bearing tolerance: a coherent distortion driven by B1 grows while the resonance condition holds, and the crossing survives when B1 is small (the quote's condition) and the crossing fast. How small is computed for the actual machine - the beam-dynamics laboratory's imperfection tools do it; pole tilt and off-center coils are the usual B1 sources.
Cited in: Beam Dynamics: An Interactive Laboratory
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Avoid running the beam long near the Walkinshaw resonance Qr - 2Qz = 0 (n = 0.2 in a classical machine): mean-field nonlinearity there pumps radial into axial oscillation with the axial amplitude reaching twice the radial amplitude.
Qr - 2Qz = 0; classical cyclotron: sqrt(1-n) = 2*sqrt(n) -> n = 0.2Source quote & editorial note
When transferring the energy of radial betatron oscillations into axial oscillations, the amplitude of the latter turns out to be twice the amplitude of radial oscillations.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 39
Editorial note, tabletop extrapolation: Very concrete for the reference machine: if the edge-field falloff pushes n through 0.2 near the last turns, dwelling ions grow vertically as far as the coupling perturbation drives them - into the dee aperture if allowed. Keep n below ~0.2 out to the extraction radius, or cross the resonance fast (dg-152, dg-694).
Cited in: Beam Dynamics: An Interactive Laboratory
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To hold the field index n roughly constant over radius, profile the pole (shim) axial gap as g(r) = g0*(r/r0)^n.
g(r) = g0*(r/r0)^n (equivalently g0*(r0/r)^-n), eq. 5.9Source quote & editorial note
If the task is to obtain an average field with a value of the field decay index n close to constant for all radii, then the axial gap g can vary in accordance with the expression
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 49
Editorial note, tabletop extrapolation: A one-line pole-taper recipe for the builder tool: pick n (e.g. 0.02-0.2), machine the gap to this power law, verify in FEMM.
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Form the average field close to the ideal isochronous curve: in the cited 30 MeV compact machine, holding the deviation within 5 G at all operating radii holds the beam's RF phase within about 5 degrees.
cited machine: |B_avg - B_iso| <= 5 G -> |RF phase deviation| <= ~5 degSource quote & editorial note
if the field is formed such that the deviation from the isochronous one for all operating radii is no more than 5 G, then this corresponds to a deviation of the RF phase... by no more than 5 degrees
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 50
Editorial note, tabletop extrapolation: The 5 G <-> 5 deg pairing is that machine's arithmetic, not a portable spec: phase slip accumulates with turn number, harmonic and energy gain per turn, so integrate it turn by turn from the measured B(r) and RF parameters, and set the reference machine's shimming tolerance from the resulting phase-acceptance budget.
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When simulating an existing magnet, the cited design practice introduces calibration coefficients on the winding-field contributions - as a rule not large, ~1-2% of the current value.
calibration factor on winding field contribution ~ 1-2%Source quote & editorial note
the so-called calibration coefficients are introduced to the level of the field created by the windings, which, as a rule, are not large and amount to ~1-2% of the current value
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 50
Editorial note, tabletop extrapolation: For the reference machine's FEMM-vs-Hall-probe comparison: compare field SHAPE versus radius and current first - a residual that is genuinely a scale error can be absorbed in a per-coil factor (checked for current-independence, since saturation makes such factors drift), while a shape mismatch means geometry, B-H data or probe calibration, and no scale factor should paper over it. The cited 1-2% is that machine's correction, not a normal-mismatch budget.
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Compensate the missing focusing at the machine center with a field bump: the central field is raised a few tens to a few hundred gauss (so it falls from center outward over the first turns), paired with RF phases chosen so the first gap crossings add axial electric focusing at the first revolutions.
B_center bump = ~30-300 G above isochronous levelSource quote & editorial note
Then the RF phase shifts to the values at which the particles cross the accelerating gaps with the optimal phase. Thus, conditions are created for the additional focusing of particles in the axial direction at the first revolutions by a high-frequency electric field. Depending on the configuration of the central region of the cyclotron, the level of the magnetic field in the center is raised to an amount of a few tens to a few hundred gauss
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 50-51
Editorial note, tabletop extrapolation: Usable on a next machine: shim a small central cone so B falls gently from center outward, and set the central-region phase so the electric focusing helps rather than hurts - then verify the resulting field index and phase history by model; RF electric focusing means n~0 first turns are not wholly unfocused even before the bump.
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Expect orbit separation from energy gain of dR = R*(dW/W)*(gamma/(gamma+1))/Qr^2 per turn; if that is too small for a septum, add a controlled first-harmonic bump (a few gauss suffices at the Qr = 1 crossing) to drive precession and enlarge turn spacing.
dR = R*(dW/W)*(gamma/(gamma+1))/Qr^2 per turn - W kinetic energy, dW the gain per FULL turn, Qr the local radial tune; the source's precession expression x_c = pi*R*(b1/B0)*n_eff uses its own n_eff definition (scan re-read queued for it)Source quote & editorial note
The presence of the resonance makes it possible to use the first harmonic of the field with a small amplitude (usually a few gauss) to obtain a significant increase in radial amplitudes.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 64-65
Editorial note, tabletop extrapolation: The dR formula tells the builder exactly what turn spacing a ~kV energy gain buys at 4-inch radius (fractions of a mm), i.e. whether a septum/foil extraction is geometrically feasible for a next machine.
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Size water-cooled copper main coils around the source's practically achievable engineering current density of ~5 A/mm^2 - defined there as ampere-turns over winding cross-section (superconducting NbTi windings reach 120-150 A/mm^2).
j_eng(Cu, water-cooled) ~ 5 A/mm^2; j_eng(NbTi SC winding) ~ 120-150 A/mm^2Source quote & editorial note
The practically achievable engineering current density (the ratio of the value of the ampere-turns in the winding to the cross section of the conductor) is of the order of 5 A/mm2.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 15-16
Editorial note, tabletop extrapolation: First-cut sizing for a next machine's coil pack: NI / 5 A/mm^2 estimates the winding cross-section with water cooling - a starting point that still owes fill factor, cooling channels and insulation their space, and the thermal calculation is the real gate (magnet-power calculator). Air-cooled magnet wire derates well below this (dg-092).
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For maximum energy gain per turn, make the dee's RF angular size (geometric angle times harmonic h) 180 degrees or an odd multiple - where the |sin| factor peaks; energy gain per turn is dE = 2*N*q*U*|sin(h*dphi/2)|.
dE_turn = 2*N*q*U*|sin(h*dphi/2)|; |sin| = 1 at h*dphi = 180, 540, 900 deg (the sign alternation is a phase convention, absorbed into the synchronous phase); transit-time effects ride on topSource quote & editorial note
the maximum energy gain corresponds to a system in which the RF size of the dee is close to 180 degrees or is a multiple of 180 degrees with a factor of 3, 5, 7
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 11
Editorial note, tabletop extrapolation: The reference machine's single ~180-degree dee on h=1 is already the optimum; the formula lets the builder tool compute turns-to-energy for any future dee angle or harmonic choice.
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A classical cyclotron's final proton energy is limited to 10-15 MeV with one or two dees at practically realizable dee voltages; set the RF generator frequency below the central-field revolution frequency so the phase slides negative and turns around near -90 degrees, maximizing radius before phase loss.
E_max(protons, classical) ~ 10-15 MeV; choose f_rf < f(0) so phase turnaround occurs near -90 degSource quote & editorial note
With a practically realizable energy set today, the final energy is limited to 10-15 MeV for protons when one or two [dees are used] ... By selecting the value of the generator frequency, it is possible to achieve that the point of changing the direction of the phase motion is near -90 degrees.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 22
Editorial note, tabletop extrapolation: At 100 keV-1 MeV the reference machine is far from the ceiling. Setting the oscillator slightly below the central-field frequency is the source's strategy for spending the phase budget symmetrically - the same lever helps a machine whose field profile is imperfect, but the check remains the summed slip (dg-273), not the detuning itself.
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With a single dee at 60-70 kV, protons can reach 9-10 MeV in a decreasing-field classical cyclotron; energy scales with achievable energy gain per turn, so more turns cannot compensate a phase budget already spent.
1 dee, U = 60-70 kV -> E_final ~ 9-10 MeV (protons, decreasing field)Source quote & editorial note
in the presence of one accelerating dee and a voltage of 60-70 kV, protons can be accelerated in a decreasing magnetic field to an energy of 9-10 MeV
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 51
Editorial note, tabletop extrapolation: Sets the scale, not a law: the quoted machine class pairs 60-70 kV with 9-10 MeV, and the reference machine's ~1.3 kV dee at ~150 keV sits consistently below that line. Final energy in a classical machine is phase-budget-limited (the summed slip, dg-273), which dee voltage relieves nonlinearly - compute the budget rather than scaling proportionally.
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The cited design traces its central-region accelerating-gap voltage boundary at 1.3-1.4 times the Kilpatrick criterion f(MHz) = 1.64*E^2*exp(-8.5/E) (E in MV/m) - an empirical benchmark for RF vacuum gaps, not a guarantee.
Kilpatrick: f[MHz] = 1.64*E^2*exp(-8.5/E), E in MV/m; cited machine's adopted boundary: <= 1.3-1.4 x KilpatrickSource quote & editorial note
the common boundary of the maximum voltage in the accelerating gaps in the central region of the accelerator is traced, which is 1.3-1.4 times higher than the Kilpatrick criterion
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 57-58
Editorial note, tabletop extrapolation: The right sizing framework if a next machine pushes dee voltage to tens of kV across small central-region gaps: compute the LOCAL peak surface field from the electrode geometry (not the average gap field), compare against Kilpatrick as a benchmark, and plan on conditioning and breakdown testing - margin is demonstrated, not assumed.
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Optimize the internal-source slit with chamfer angles of 40-60 degrees, and make the slit's axial size several times its radial size; slit shape strongly changes extracted current (calculated spread 90-850 nA between variants).
chamfer angle 40-60 deg; axial/radial slit size ratio ~ several; the source's Fig. 56 slit variants span max I = 90-850 nASource quote & editorial note
The shape of the source slit, when its axial size is several times larger than the radial one, is most frequently used... They are optimized according to the chamfer angle, which is usually 40-60 degrees. ... the angle of the chamfers directly affect the magnitude of the beam current extracted from the source, which is confirmed by numerous calculations [132] and measurement results (Fig. 56).
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 52-53
Editorial note, tabletop extrapolation: Cheap, high-leverage geometry rule for the reference machine's PIG-style source: start from a tall-and-narrow slit with ~45-degree chamfers - the source's most-used geometry - then optimize against measured beam, since the chamfer angle demonstrably moves extracted current by an order of magnitude across variants.
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With external axial injection, choose an injection energy (in eV per charge) below the dee voltage amplitude: the first gap crossings then rapidly enlarge the orbit, minimizing central-structure size and radial losses.
E_inj/q < U_dee (injection energy less than accelerating-voltage amplitude)Source quote & editorial note
the optimal case from the viewpoint of minimizing the radial beam losses is a mode of operation in which the value of the injection energy is less than the amplitude of the accelerating voltage across the dees
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 55-56
Editorial note, tabletop extrapolation: If a next machine ever moves to an external source and axial injection: the cited criterion (injection energy per charge below the dee amplitude) minimizes radial losses by letting the first gap crossings enlarge the orbit fast - set the actual injection energy jointly with inflector acceptance, transport and RF capture, not from the radial-loss criterion alone.
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With an internal ion source and cosine RF, the central region's phase acceptance is roughly the starting-phase window (-90, +20) degrees; phase slits can then select bunches down to a few RF degrees.
phase acceptance ~ (-90 deg, +20 deg) relative to peak-voltage phase = 0Source quote & editorial note
the phase acceptance of the center, as a rule, contains the particles, the initial RF phases of which do not go beyond the range of (-90; 20)
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 56
Editorial note, tabletop extrapolation: Explains why a large fraction of source output never accelerates: only starting phases inside a ~110-degree window of the full 360 are candidates at all - a uniform-emission estimate makes that a ~30% ceiling, before radial and axial acceptance cut further; it is not a measured capture efficiency. The builder tool should launch macroparticles across this window rather than a single reference phase.
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Modern cyclotron facilities practically achieve ~1e-7 Torr, and the vacuum serves two purposes: beam survival against gas loss, and stable operation of electrical components through higher breakdown voltage.
P ~ 1e-7 Torr practically achievable in modern facilities (example, not target)Source quote & editorial note
Its second purpose is to ensure the stability of operation of electrical components of the accelerator... by increasing the breakdown voltage. In modern cyclotron facilities, a pressure of ~1e-7 Torr is practically possible.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 14
Editorial note, tabletop extrapolation: The dual criterion is the transferable part: if the dee sparks before the beam is lost to gas, vacuum improvement should be judged on breakdown margin, not just stripping loss. What pressure the reference machine actually needs comes from its own gas-loss arithmetic and holdoff behavior - not from this figure in either direction.
Cited in: The Vacuum Budget of a Cyclotron
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Estimate residual-gas beam loss step-by-step as dN = sigma*n*N*v*dt with gas density n[m^-3] ~ 3.22e22 * P[Torr] at 300 K; use species- and energy-dependent cross sections for the actual (or an explicitly assumed) gas composition.
dN = sigma*n*N*v*dt; n[m^-3] ~ 3.22e22*P[Torr] at 300 K; integrated: N/N0 = exp(-sum_i INT n_i*sigma_i(E) ds)Source quote & editorial note
The number of lost particles dN at each time step dt can be estimated by the formula dN = sigma nN v dt
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 70
Editorial note, tabletop extrapolation: Lets the builder tool convert a gauge reading and total path length (hundreds of turns) into a survival fraction - with the composition stated, the gauge's gas-sensitivity factor applied, and the cross sections taken at the right energies. An assumed oxygen-like composition is a labeled assumption, not a guaranteed worst case: water and hydrocarbons can exceed it for the processes that matter.
Cited in: The Vacuum Budget of a Cyclotron
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Place phase slits where the beam's radial size is largest, as close to the center as possible, on different turns azimuthally separated by half a magnet period, and away from accelerating gaps (along the centerlines between dees).
Source quote & editorial note
The slit is most functional if it is installed in the place of the largest radial size of the beam... The closer to the center the device is installed, the more efficient it is, and the less radiation losses thereon. ... If there are several slits, then it is advisable to place them at different revolutions and azimuthally with a difference of half the period of the system, e.g., in a hill and a valley. ... Elements should be installed away from accelerating gaps, e.g., along the center lines of the space between the dees
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 56
Editorial note, tabletop extrapolation: Practical placement rules if the builder adds a beam-defining post or slit to clean up phase spread and improve turn separation at extraction radius.
-
In the cited design context, the transition to high-intensity (space-charge-dominated) operation is most often placed at a few hundred microamperes of beam current.
cited rule of thumb: high-intensity boundary ~ few 100 uA; check by comparing the space-charge term against emittance and focusing terms (generalized perveance / tune depression), using PEAK currentSource quote & editorial note
Most often, the boundary of the transition to high intensities is determined at the level of a few hundred microamperes.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 40
Editorial note, tabletop extrapolation: The reference machine's nA-uA beams sit far below the cited boundary, so omitting space-charge solvers is a reasonable default for the builder tool - but earn it with one calculation: peak (bunched) current through the low-energy first turns is where space charge bites first, so run the perveance estimate there before declaring it negligible.
-
For shielding design, fast-neutron production on complex nuclei is roughly one neutron per 10-15 MeV of proton energy (below 50-60 MeV); the source's permissible-flux figure is 30-60 n/cm^2/s (a dated, era-specific limit - modern limits are dose-based), and it gives the neutron relaxation length in ordinary concrete as 16 cm (1-2 m walls typical).
~1 neutron per 10-15 MeV proton energy on target; source's era limit 30-60 n/cm^2/s (dose-based limits govern today); concrete relaxation length 16 cmSource quote & editorial note
mainly fast neutrons are generated, and the permissible flux is 30-60 neutrons/cm2 s
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 16
Editorial note, tabletop extrapolation: At <=1 MeV protons the reference machine is below every (p,n) threshold - not only the common structural metals but the light targets too: 7Li 1.88 MeV, 9Be 2.06 MeV, 11B 3.02 MeV, and even deuterium 3.34 MeV (NNDC QCalc, retrieved 2026-08-23) - so these neutron numbers do not set its shielding scale. They start to as soon as the machine accelerates deuterons, because D-D and Be(d,n) are exoenergetic with no threshold at all (dg-1047), or pushes protons past ~1.9 MeV on lithium; dg-1041 and dg-1047 carry the residual channels that keep a neutron survey honest below that. Read this as a scale for the case that applies, not as a clearance for the case that does not. [Corrected 2026-08-22: previously said neutron shielding is "a non-issue" for the machine; the exception clause was there, but the headline was an absolute.] [Corrected 2026-08-23: the exception clause itself was imprecise - it said the neutron channels "open far lower" for Li, Be, B or a deuterated material, but every one of those (p,n) thresholds is above 1 MeV as well; the genuinely thresholdless route is deuterons, per dg-1047. Raised by an upstream review of the source dataset.]
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Turn separation from acceleration alone is dr = R*(dE/turn)/(2E), so at fixed radius doubling the dee voltage doubles the turn spacing.
dr0/r0 = (1/2)*(dE0/E0); more exactly dR/dn = R*(dE/dn)/E * gamma/(gamma+1) * 1/nu_r^2Source quote & editorial note
the relative radial increase is only half the relative energy increase. However, for a given cyclotron, the turn separation dr0 will double when the dee voltage is doubled.
Kleeven & Zaremba, Cyclotrons: Magnetic Design and Beam Dynamics — CAS 2015, arXiv:1804.08961 (2018) — p. 44
Editorial note, tabletop extrapolation: The reference machine (~150 keV, 2.6 keV/turn, r ~ 9.6 cm) gets ~0.8 mm/turn. A 10 kV dee at the same radius scales it by the ratio of per-turn energy gains - computed from the actual voltage convention and gap count: 10 kV peak with two crossings at good phase is ~20 keV/turn, ~6 mm; one effective crossing or poor phase halves it or worse.
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Professional-scale reality check: 30 MeV with 100 keV/turn at R=0.5 m yields only 0.83 mm turn separation, versus a typical 4 mm radial beam width - acceleration alone rarely separates turns.
dr = R*dT/(2T)Source quote & editorial note
for a final energy of T = 30 MeV, dT = 100 keV, and an extraction radius of 0.5 m, we find dr = 0.83 mm. This is a rather small number, e.g. when compared with a radial beam width of for instance 4 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 6
Editorial note, tabletop extrapolation: Small machines fare better because dr/R scales as dT/T: a 350 keV next machine at 10-20 keV per turn carries a fractional turn separation 9-17x this 30 MeV machine's. Its beam width does not shrink in proportion, though - so the separation-vs-width comparison still needs the machine's own numbers (dg-495).
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Maximum extra turn separation from precession is 2*pi*(1-nu_r)*x; a 3 mm coherent amplitude accelerated to nu_r=0.8 buys 3.8 mm, added on top of the acceleration term.
dr_precession(max) ~ 2*pi*|1 - nu_r|*x near integer tune (the exact sinusoidal maximum is 2*x*|sin(pi*nu_r)| - 3.53 mm for the quoted 3 mm, nu_r = 0.8 case)Source quote & editorial note
when a coherent oscillation amplitude x of 3 mm has been built up ... and acceleration takes place until vr = 0.8, the maximum turn separation due to precession is 3.8 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 7
Editorial note, tabletop extrapolation: A deliberate few-mm coherent amplitude (source off-centering is one way to seed it), plus letting nu_r fall toward 0.8 in the fringe, can multiply turn spacing severalfold - IF the precession phase is arranged so the separation appears at the septum azimuth. It is a designed, tracked orbit-dynamics move, not a free effect.
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Size the coherent oscillation to roughly equal the incoherent (emittance) amplitude: larger radial amplitude risks vertical blow-up when passing the nu_r = 2*nu_z coupling resonance in the fringe field and invites strong nonlinear effects; smaller wastes separation.
Source quote & editorial note
Accelerating the beam far into the fringe field often means passing the vr = 2 vz coupling resonance. Energy can be exchanged from the radial to the vertical motion, blowing up the beam vertically and leading to beam loss. If the radial oscillation amplitude is not too large, and if the resonance is passed in only a few revolutions, vertical amplitude increase is avoided. In practice, a coherent radial oscillation amplitude of the same size as the incoherent amplitude, is a good criterion for efficient extraction. Another reason for requiring not too large radial oscillation is avoiding strong non linear effects.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 7
Editorial note, tabletop extrapolation: If a next machine's radial beam half-width is ~2-3 mm, start near a ~2-3 mm coherent amplitude and set the acceptable ceiling by tracking through the extraction field - the equality criterion is the source's practical starting point, not a hard limit.
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Keep the deliberately induced radial amplitude from the nu_r = 1 resonance to a few mm, and cross vertical-stability-threatening resonances (nu_r = 2*nu_z at n = 0.2; nu_z = 1/2 at n = 0.25 in smooth weak focusing) quickly.
Source quote & editorial note
one has to limit the radial amplitude, induced from the v = 1 resonance, to a few mm.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 18
Editorial note, tabletop extrapolation: In a weak-focusing field the last turns sweep the field index upward toward these resonances: compute the actual tune curves from the measured field map, and keep energy gain per turn high through any crossing so that tracking predicts acceptable vertical growth - speed of crossing, not a fixed turn count, is the criterion.
Cited in: Beam Dynamics: An Interactive Laboratory
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A first-harmonic field bump displaces the equilibrium orbit by dx = eps1*R/(nu_r^2-1); eps1=1e-4 (about 0.6 G in a 0.59 T field) at R=1 m and nu_r-1=0.01 already gives 5 mm.
dx = eps1*R/(nu_r^2 - 1), eps1 = B1/B0Source quote & editorial note
taking eps1 = 10-4, R = 1 m and vr - 1 = 0.01, one finds an orbit centre shift, i.e. a radial oscillation amplitude, of dx = 5 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 9
Editorial note, tabletop extrapolation: Gauss-level azimuthal asymmetry matters at 0.59-0.89 T NEAR nu_r = 1: the (nu_r^2 - 1) denominator is what turns the quoted 0.6 G into 5 mm, and the sensitivity falls away from the resonance and shrinks with radius. It is both the knob (a deliberate shim or coil bump) and the hazard (uncontrolled bumps de-center the beam) - dg-562's tolerance computation is the same physics from the defensive side.
Cited in: Beam Dynamics: An Interactive Laboratory
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Brute-force first-harmonic extraction needs big bumps: in a 1.7 T conventional cyclotron a 1 G bump introduces only ~0.2 mm of radial gain, and the gain per turn scales with R - favouring large machines.
source Eq. 15 is per unit angle: dR/dtheta = R*b_N/(2*N*B0); per full turn: dR ~ pi*R*b_N/(N*B0) - reproduces the quoted ~0.2 mm for 1 G at 1.7 T with R ~ 1 mSource quote & editorial note
For a typical conventional cyclotron (Bo ~ 1.7 T) a bump of 0.1 mT (1 G) introduces a radial gain of about 0.2 mm. To get a desired turn separation bigger bumps are needed (brute force). ... Since, for a given energy, the magnetic rigidity BR is constant, the radial gain per turn increases with a factor of R favouring larger machines.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 14
Editorial note, tabletop extrapolation: Scaled to 0.6-0.9 T and r ~ 0.1 m the per-turn gain from 1 G is only ~0.04 mm, so mm-scale separation would take tens of gauss of first harmonic - precession is far cheaper than brute force.
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Crossing nu_r=1 with a first harmonic builds coherent amplitude over an effective resonance duration of typically ~10 revolutions; in the cited machines extraction typically takes place near nu_r = 0.8.
x_c = pi*sqrt(2)*(b1/B)*R*n_eff (order of magnitude), n_eff = sqrt(1/(2*pi*dnu_r/dn)) ~ 10 turnsSource quote & editorial note
n_eff is the effective duration of the resonance (typically around ten revolutions). ... Typically the extraction takes place near v = 0.8.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 14
Editorial note, tabletop extrapolation: A smooth azimuthally symmetric weak-focusing machine approaches nu_r=1 from below and never crosses it, so create the amplitude by ion-source off-centering instead (a different mechanism than resonant buildup - verify what it delivers by tracking) and use the fringe region where nu_r has fallen toward the source's typical ~0.8 for precession, with the actual tune taken from the measured field map.
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Electrostatic deflector design point: give the beam a 50-100 mrad kick; septum entrance a few tenths of a mm (0.1 mm in modern IBA practice) thickening to several mm at exit, with a V-slit entrance to spread heat.
theta = E_gap*L/(2T/q) for nonrelativistic protons (pv = 2T)Source quote & editorial note
An angle kick of typically 50 to 100 mrad is provided. The inner electrode, septum, is at earth potential. At the entrance it has a thickness of a few tenths of a mm, increasing to several mm at the exit.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 14
Editorial note, tabletop extrapolation: At 350 keV a 100 mrad kick over 10 cm of arc needs E = theta*(2T/q)/L = 7 kV/cm - about 3.5 kV across a 5 mm gap. At nanoamp beams the septum's heat load is negligible whatever fraction it intercepts: 1 nA of 350 keV beam carries only 0.35 mW in total.
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Deflector discharge limit (Smith-Grunder): keep V*E < 1.5e4 kV^2/cm, and derate the holdable voltage another 20-30% because the deflector sits in a magnetic field.
V[kV] * E[kV/cm] < 1.5e4Source quote & editorial note
a criterion for the product of electric field E and potential V for a cyclotron deflector in order to avoid electric discharges: VE < 1.5 104 (kV)2/cm. The maximum sustainable voltage in a magnetic field is 20-30% lower.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 14
Editorial note, tabletop extrapolation: A 3-5 kV, 5-10 kV/cm tabletop deflector sits orders of magnitude below this bulk-discharge criterion - so at tabletop scale the practical ceiling comes from feedthrough, surface and edge-radius engineering (dg-353, dg-297, dg-295), not from the Smith-Grunder product.
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Round every HV electrode edge: peak field at an edge of radius r facing a gap a is Emax = 0.9*V/(r*ln(a/r)); Rutgers chose 3/16-inch edge radii to keep peaks at 170 kV/inch (67 kV/cm) against aluminum's ~290 kV/inch limit.
Emax = 0.9*V/(r*ln(a/r))Source quote & editorial note
At HV edges, electric field lines become so dense that breakdown becomes a major concern. Aluminum=290 kV/inch ... We settled on a minimum radius of R=.1875 inches ... Emax=170 kV/inch
Editorial note, tabletop extrapolation: Direct amateur precedent: a 1 T / 472 keV university tabletop deflector ran at 28-32 kV. A lower-energy machine needs proportionally less deflector voltage (scaling roughly with beam energy at similar geometry - a 150 keV-class machine perhaps a third, not a tenth), and the edge-field formula stays the design check: generous radii reduce peak field, they do not make sparking impossible - finish and conditioning still rule (dg-295, dg-353).
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Limit stored energy into deflector arcs: a 30 kV supply cable alone stores ~0.1-0.4 J - Rutgers observed arcing at that energy but, in this case, no electrode pitting - so keep the HV cable short and add series resistance at the feedthrough. [Corrected 2026-08-23: earlier text said the stored energy was 'enough to pit electrodes'; the quote says the opposite for this instance. The formula counts cable capacitance only, not the supply's reservoir.]
E_cable = 0.5*C_cable*V^2 (cable only; add the supply's output capacitance for the real arc energy)Source quote & editorial note
~0.1 Joules at 30 kV ... ~0.4 Joules at 30 kV ... The bottom plate and deflector electrode - no pitting on the electrode noticed.
Editorial note, tabletop extrapolation: Rutgers' slide sequence recounts arcing a feedthrough run above its class and rebuilding with the feedthrough inside vacuum plus a corona adapter (the specific ratings are the slides' account - scan re-read queued). The transferable lesson is the margin discipline: choose feedthrough rating from the manufacturer's figure, the vacuum-side geometry and test history, and never run a feedthrough above its rating. [Note revised 2026-08-23: 'rate 2-3x over operating voltage' was an invented margin.]
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Classical-cyclotron deflector sizing (MIT 42-inch practice): peel to DR = 0.1R-0.2R (0.15R typical); for 16 MeV deuterons at R=18.75 in with 0.3 in gap that meant 47-87 kV, with the channel tapered from ~1/8 in at entry to ~1/2 in at exit.
Vd = (2T/q)*d*DR/(R*(R+DR)) (uniform-field estimate)Source quote & editorial note
For DR = 0.1R: Va = 47,000 volts ... A typical figure, used in the MIT cyclotron, is a DR of 0.15R. ... The deflector gap is usually tapered.
Livingston & Blewett, Particle Accelerators (1962) — p. 163-166
Editorial note, tabletop extrapolation: Scaling by 2T: a next machine at 350 keV needs about 1/45 of MIT's voltage at the same normalized geometry - roughly 1-2 kV across a proportionally scaled entry gap - rising if a faster peel (larger DR) or a larger gap is wanted. Compute with the formula for the actual geometry (dg-590's worked example).
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The efficiency ladder for extraction, rung by rung and source by source: ~10% for early synchrocyclotron precessional extraction (Botman), up to 25% of internal beam for a well-tuned classical-cyclotron deflector under optimum conditions (the quoted machine), 75-80% for IBA self-extraction and >90% for modern well-centred precessional methods (Jongen, CYC2004).
Source quote & editorial note
Emergent beam intensities up to 25 per cent of the resonant beam intensity have been obtained under optimum conditions; ... practical operating intensities would in this case be limited to 80 or 100 [micro]a.
Livingston & Blewett, Particle Accelerators (1962) — p. 166
Editorial note, tabletop extrapolation: Plan a next machine's deflector attempt around the classical rungs - tens of percent at best, and that under optimum tuning: with nA internal beam, 0.1-0.25 nA external is still a countable, PIXE-usable beam. The upper rungs belong to machine classes a tabletop deflector does not reach.
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Multi-turn extraction energy spread is of order the per-turn gain, ~2*q*Vdee in the simple picture; single-turn extraction requires RF phase width |phi| < sqrt(2/N) - a few degrees for hundreds of turns - and correspondingly tight field stability.
|phi| < arccos(N/(N+1)) ~ sqrt(2/N)Source quote & editorial note
This results in a phase acceptance of only a few degrees for the typical case of a few hundred turns.
Baartman, Cyclotrons: Why/How Are Their Dynamics Different? — JINST 18 T03005 (2023) — p. 10
Editorial note, tabletop extrapolation: Do not chase single-turn extraction on a small machine: accept multi-turn with spread of order the turn energy gain (~20 keV at a 10 kV dee - the simple-picture floor; turn overlap and precession can widen it), which PIXE tolerates. (Spread and dB/B detail: botman pp.11-14.)
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Extraction purely by acceleration (no deflector) is possible only if turn count Nt <= (R/g)^2/(pi*Nh*gamma*(gamma+1)) - i.e. the pole half-gap g at extraction must be tiny compared to radius R.
Nt <= (1/(pi*Nh*gamma*(gamma+1))) * (R/g)^2Source quote & editorial note
it is mostly the squared ratio of extraction radius and pole gap at extraction which determines the maximal number of turns or the minimal energy gain
Baumgarten, Cyclotron Beam Extraction by Acceleration — arXiv:2205.04124 (2022) — p. 5-6
Editorial note, tabletop extrapolation: A next machine with R ~ 10 cm and half-gap 1.27 cm allows at most ~9 turns by the bound (needing ~18 keV per turn); shrinking the edge half-gap to 6-7 mm allows ~32-44 turns - a few keV per turn, reachable for a 5-10 kV LDMOS dee.
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H- stripping extraction converts nearly all intercepted ions with a simple device - a carbon foil of 50-200 ug/cm2, lifetimes above 2e4 uAh - and makes extracted energy variable by foil radius, at the price of an H- source, stringent vacuum, and the residual losses stripping keeps: interception geometry, scattering, straggling, foil heating and finite life.
dT/T = 2*dr/r sets extracted energy spread from radial beam widthSource quote & editorial note
the negative hydrogen ion beam simply passes a thin carbon foil (e.g. pyrolytic graphite, typically 50 to 200 ug/cm2), which strips off the electrons.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 3-4
Editorial note, tabletop extrapolation: At sub-MeV a 50 ug/cm2 foil costs ~10 keV of energy and some scattering. The septum, HV and turn-separation problems genuinely disappear - replaced by the H- problems: an internal H- source, and the 1e-6 Torr-class vacuum that gas stripping of the fragile H- demands (dg-599).
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H- gas-stripping cross-section is maximal exactly in the 0.1-300 keV range; the compact AMIT design (8.5 MeV, 4 T) loses (14.6 +/- 1.5)% at ~1e-4 hPa central pressure, while a 70 MeV machine at ~1.5e-6 mbar transmits ~87%.
T = exp(-n*sigma*L), n[cm^-3] = 3.3e16 * P[Torr], L = total spiral pathSource quote & editorial note
the cross section of H- interactions with the gas molecules is maximal for the energy range (0.1 - 300) keV of the beam in the central region.
Calvo et al., Beam Stripping Interactions in Compact Cyclotrons — PRAB 24, 090101 (2021) — p. 14
Editorial note, tabletop extrapolation: A next machine's H- variant spends its whole life at the cross-section peak. Run the loss arithmetic explicitly through T = exp(-n*sigma*L) with measured H- detachment cross-sections - the 1e-15 cm2 class near the peak; fetch sigma(E) for the actual gas mix when designing. At that scale ~25 m of spiral at 1e-6 Torr loses of order 5-10%, and 1e-5 Torr costs most of the beam: vacuum, not physics, decides this option. (70 MeV data: cyclotron_vacuum_model p.3.)
Cited in: The Vacuum Budget of a Cyclotron
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Lorentz (magnetic) stripping of H- has rest-frame lifetime tau = (A1/E)*exp(A2/E) with A1=2.714e-6 s*V/m, A2=4.474e9 V/m, E=gamma*beta*c*B - negligible below a few MeV even at 4 T.
tau = (A1/E)*exp(A2/E), E = gamma*beta*c*BSource quote & editorial note
a 4 T magnetic field for the maximum achievable energy of 8.5 MeV in the AMIT cyclotron corresponds to a beam-rest-frame electric field of E = 160 MV/m. This entails a marginal beam fraction loss per unit length of 1.42e-6 m-1
Calvo et al., Beam Stripping Interactions in Compact Cyclotrons — PRAB 24, 090101 (2021) — p. 7-8, 14
Editorial note, tabletop extrapolation: At 0.889 T and 500 keV the rest-frame field is ~9 MV/m, where the exponential makes the lifetime effectively infinite - Lorentz stripping can be ignored entirely for a next machine.
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Precessional extraction preserves beam quality when the turns between amplitude creation and the septum are few, because the HF-phase-dependent spread of orbit centres - 2*pi times the particle-to-particle DIFFERENCE in the integral of (nu_r - 1) dn - stays small for a well-centred beam.
spread of orbit-centre azimuth across the RF-phase distribution: delta_theta = 2*pi * delta[ integral (nu_r - 1) dn ] - the difference of the precession integral between particles, not the integral itselfSource quote & editorial note
the spreading of orbit centres for different HF phases due to HF mixing, is small for an originally well centreed beam, as in general the number of turns from the vr = 1 resonance till extraction is not so large.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 9
Editorial note, tabletop extrapolation: If a next machine uses source off-centering (amplitude created at turn 1, necessarily - it cannot be placed late), evaluate the phase-mixing integral from tracked particles in the actual field map before assuming the coherent centroid survives: individual amplitudes persist while the ensemble centroid can smear. A trim bump near the extraction region, where late placement IS possible, is the cleaner tool.
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Verify turn separation before building the deflector: the cited machine's differential radial probe with 2 mm finger spacing revealed the radial (precessional) oscillation near extraction.
Source quote & editorial note
Figure 11 shows a differential probe measurement for this cyclotron in the extraction region. The separation between the probe fingers is 2 mm. The figure reveals the radial oscillation near extraction.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 11-12
Editorial note, tabletop extrapolation: Adding a two-finger (or shadow-bar) differential head turns the reference machine's existing radial probe into the diagnostic that informs septum placement - choose the finger spacing from the PREDICTED turn separation and beam width (2 mm was that machine's), and combine the measured pattern with orbit tracking and clearance requirements rather than reading placement off the probe alone.
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PIG discharges split into two families: cold-cathode (secondary-emission) arcs run above ~1 kV at 0.5-5 A, hot-cathode (self-heated thermionic) arcs run below ~1 kV at 1-50 A. The cold mode has positive incremental impedance, the hot mode negative — plan the supply accordingly.
cold cathode U_arc > 1 kV, I = 0.5-5 A; hot cathode U_arc < 1 kV, I = 1-50 ASource quote & editorial note
the cold cathode PIG source with arc voltages above 1 kV and currents between 0.5 and 5 A, and the hot cathode PIG source with arc voltages below 1 kV and currents between 1 and 50 A
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82
Editorial note, tabletop extrapolation: The reference machine's source at tens-to-hundreds of mA sits BELOW the handbook's canonical cold-cathode band, which starts at 0.5 A - closer to a glow regime than the tabulated arcs. The design consequence stands regardless: if the discharge crosses into a self-heated, negative-slope mode (AMIT reported a transition near 250 mA on their source), only a stiff current source holds it - so build the arc supply as a current source from the start.
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The arc plasma floats a few volts below anode potential and essentially the full arc voltage drops across the thin cathode sheath; each primary electron yields about 8 ions on average.
V_plasma ~ V_anode - (few V); ions per oscillating electron ~ 8Source quote & editorial note
The arc plasma is a few volts negative in respect to the anode potential and nearly the full arc voltage drops along the narrow cathode sheath ... One electron can produce about eight ions or charges on average.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82
Editorial note, tabletop extrapolation: Ion energy at the cathodes is ~ the full arc voltage (times charge state) before collisional losses - evaluate sputtering from species/material yield data at that energy, not a linear-in-voltage assumption. Grounding the chimney (anode) to the chamber with cathodes negative is ONE workable topology if the source body is meant to sit at chamber potential - check it against the machine's RF/HV design, heater isolation and filtering before wiring it.
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Above a minimum magnetic field of roughly 0.1 T the discharge parameters barely depend on B; ignition is easier at higher field. Ordinary internal PIGs run 0.1-1 T homogeneous.
B_min ~ 0.1 T; typical 0.1-1 T; little d(V,I)/dB above thresholdSource quote & editorial note
There is little influence of the magnetic field on the discharge parameters as long as it reaches a certain minimum of roughly 0.1 T.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82
Editorial note, tabletop extrapolation: The reference machine's 0.59 T and a ~0.9 T successor both clear the handbook's 0.1 T minimum, so field-level effects on the ARC parameters should be small per the quote. Ignition and stable running still ride on pressure, geometry and surfaces (dg-372's ignition margins) - after a large field retune, a quick arc-parameter check beats an assumption.
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Ion current density at the cathodes is 5-10x that at the anode wall; total extracted current is proportional to arc current, roughly 10-100 (mA/cm^2) per ampere of arc for radial extraction through the anode slit.
j_cathode = (5-10) x j_anode; I_extracted/area ~ 10-100 (mA/cm^2)/A_arcSource quote & editorial note
the ion current density at the cathodes is five to ten times the density at the anode surface ... The total extracted current of a PIG ion source is proportional to the arc current (Figure 5.6), and for extraction through the anode, about 10 to 100 (mA/cm2)/A
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82-83
Editorial note, tabletop extrapolation: Sizing arithmetic for the chimney slit: a 0.5 x 5 mm slit (0.025 cm^2) at 100 mA arc predicts ~25-250 uA available at the slit — consistent with Forringer's measured 230-590 uA at 50-150 mA through a 0.5 mm slit.
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Arc voltage rises as gas flow or particle density drops, until the discharge becomes unstable; the practical low-flow boundary of the operating window is set by that instability.
dV_arc/d(gas flow) < 0 at constant I_arc; instability at starvation limitSource quote & editorial note
the arc voltage increases with decreasing gas flow or particle density in the discharge chamber until the discharge becomes unstable
Wolf (ed.), Handbook of Ion Sources (1995) — p. 83
Editorial note, tabletop extrapolation: Run current-regulated and watch arc voltage as a flow/health indicator: creeping arc voltage at fixed current is evidence of falling gas density and approaching instability - cross-check against gas supply and cathode condition before acting, since a worn cathode and other drifts move arc voltage too.
Cited in: The Vacuum Budget of a Cyclotron
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Cold-cathode arc power is limited to about 1 kW per cathode in the source's account, because thermal electron emission sets in beyond that; higher power means pulsing or accepting transition to the hot regime.
P_arc,max(cold, dc) ~ 1 kW per cathodeSource quote & editorial note
The arc power for cold cathode operation is limited to about 1 kW per cathode, because of the start of thermal electron emission
Wolf (ed.), Handbook of Ion Sources (1995) — p. 84
Editorial note, tabletop extrapolation: The reference machine's 50-150 W arc sits well below the cited onset, which makes cold (secondary-emission) operation the expectation - but confirm it: per-cathode heat loading, geometry and cooling set the actual cathode temperature, so check the buttons for signs of running hot rather than assuming the regime from arc power alone.
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Cathodes are worn out when the sputter-erosion crater depth reaches roughly the anode bore radius; beyond that the discharge destabilizes. Titanium is the best cold-cathode compromise; tantalum if the cathodes run hot. Cold mode wears faster than hot because arc voltage (hence sputter yield) is higher.
end-of-life at crater depth ~ r_anode_bore; Ti (cold) / Ta (hot) cathodesSource quote & editorial note
The cold and hot cathodes are worn out when the erosion crater's depth reaches around the anode bore radius. The discharge becomes unstable under these conditions ... Titanium has been selected as the best compromise ... If the cathodes are allowed to run hot, tantalum has been shown to be a good choice.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 84-85
Editorial note, tabletop extrapolation: Cathode buttons are the main consumable: with a ~3 mm diameter anode bore, end-of-life comes near ~1.5 mm of crater depth (the criterion is the bore RADIUS). Stock spare buttons and log arc-hours. Material follows regime, not convenience: titanium for demonstrated cold operation, tantalum where the cathodes verifiably run hot.
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Wolf Table 5.5's cold-cathode column, as extracted (the quote line verifies the gas row against the page image): arc 1-5 kV at 1-5 A, ignition 5 kV, duty <=25%, B >= 0.4 T, source gas pressure 1-10 Pa, gas consumption 0.2 sccm, ion current <=5 mA, anode aperture 1.5 x 25 mm, anode canal 6 mm dia, cathode 9 mm dia, cathode spacing 6.5 cm.
see rule; gas consumption 0.2-0.6 sccm across all PIG types in the tableSource quote & editorial note
Gas consumption (sccm) 0.2 [hot cath.] / 0.2 [cold cath.] / 0.2-0.6 [heated cath.] (Table 5.5; verified against page image)
Wolf (ed.), Handbook of Ion Sources (1995) — p. 101
Editorial note, tabletop extrapolation: The headline for the reference machine is the gas line - full-size accelerator PIGs run on 0.2-0.6 sccm, and its own hydrogen feed is a 1-sccm-full-scale mass-flow controller, so what the chimney buys is not less gas but gas confined where the ionization happens. Dimensions scale down for a 36 mm pole gap (its chimney will be shorter than the 6.5-10 cm cathode spacings listed, which are for big-gap machines).
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Feed the gas into the anode close to the cathode(s) — it eases ignition and minimizes neutral gas flow out through the extraction slit.
gas inlet at cathode end of chimney, not at slit levelSource quote & editorial note
Gas is fed to the discharge usually through the anode close to the cathode(s) to ease ignition of the arc and to keep the neutral gas flow through the extraction slit in the anode low
Wolf (ed.), Handbook of Ion Sources (1995) — p. 81
Editorial note, tabletop extrapolation: Plumb the MFC line to feed near the cathode end of the chimney where the geometry allows (AMIT feeds through the cathode cavity - a variant of, not identical to, the quoted through-anode arrangement): it eases ignition and keeps neutral flow out the slit low. Chamber backfill still works (dg-409) - the injection win is lower chamber pressure for the same source density, to be verified by measurement on the actual machine.
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In a heated-cathode PIG the anticathode is kept cold and collects a net electron current; more than -20 V of bias is needed to suppress it. Anticathode is usually strapped to cathode potential, sometimes left floating for space reasons.
V_suppress(anticathode) < -20 V; usual connection anticathode = cathodeSource quote & editorial note
More than -20 V is necessary to suppress this electron current ... The anticathode is usually connected to the cathode, but sometimes just floating because of space problems in some cyclotrons.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 86
Editorial note, tabletop extrapolation: For the symmetric cold-cathode chimney, strap both cathodes together on one HV feed - that is the intended symmetric topology, not the anticathode case the quote describes. A floating anticathode is a documented space-saving variant in some cyclotrons; if used, verify its self-bias, stability and thermal loading, since floating changes the electron interception the strapped connection sets.
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PIG beam energy spread is tabulated at 10-50 V (read as eV per unit charge), with typical currents in the 5-500 mA class.
dE(PIG) = 10-50 eV per charge state; typical currents 5-500 mA class (source table)Source quote & editorial note
PIG ion source 10-50 [energy spread, V] 5-500 [typical ion current, mA] (Table 2.1)
Wolf (ed.), Handbook of Ion Sources (1995) — p. 51
Editorial note, tabletop extrapolation: Against a few-keV effective first-gap gain a 10-50 eV spread is a ~1 percent perturbation, so source simplicity is worth keeping - confirm with the machine's own capture/acceptance estimate, since capture depends on RF phase and central-region geometry, not the gap voltage alone; the filament-arc comparison needs its own source.
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Cold-start ignition per Clark's account: raise the arc voltage to about 3 kV and increase gas pressure; the struck arc is then stabilized by the supply's current regulator or ballast resistor, with dc arc currents of 1-15 A (the quote). Corroborating machines carry their own figures: AMIT (to -3 kV with a gas boost near 10 sccm, striking in seconds, sustaining under 1 kV) and Forringer's 3 kV current-limited supply (dg-415).
V_ignite ~ 3 kV (Wolf table gives 3-5 kV); V_run = 0.3-2 kV; gas boost then reduceSource quote & editorial note
An arc is struck by raising the arc voltage to about 3 kV and increasing the gas pressure ... is stabilized by the arc supply current regulator or ballast series resistor ... Arc currents are 1-15 amps for dc sources and higher for pulsed sources. Arc voltages are 300-2000 volts.
Clark, Ion Sources for Cyclotrons — Cyclotrons '81, Caen (1981) — p. 3
Editorial note, tabletop extrapolation: Spec the arc supply for ~3 kV compliance even though running voltage is ~0.3-2 kV, and automate the sequence - gas up, strike, gas down, current-regulate - with the boost magnitude and timing tuned on the machine rather than copied.
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Internal-source extraction in Clark's survey: the anode/chimney is grounded and the dee's RF does the extraction via a puller or feeler, at 30-100 kV of RF on the full-size machines; his external sources run 10-30 kV DC with the anode biased positive.
internal PIG anode at ground; extraction field = dee RF via puller; 30-100 kV RF (big machines)Source quote & editorial note
For internal sources, the anode is usually grounded and 30-100 kV of rf voltage is used for extraction with a feeler or puller extending from the dee.
Clark, Ion Sources for Cyclotrons — Cyclotrons '81, Caen (1981) — p. 3
Editorial note, tabletop extrapolation: The reference machine extracts with its few-kV dee - far below the surveyed machines. Compensating with a small source-puller gap follows Child-Langmuir-like scaling (I ~ V^1.5/d^2 in the planar model - a guide in this geometry, not a law): documented small gaps run 2.3-2.9 mm (Siemens, K100 - dg-624), and expect proportionally lower current than published microamp figures until measured.
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PIG cathode maintenance interval in the cited heavy service (1-15 A arcs) is a few hours to a day - cathode replacement plus anode cleaning; a hooded filament source in the same machines delivers a few mA of protons.
cathode service interval ~ hours to 1 day (heavy-ion, 1-15 A arcs)Source quote & editorial note
A disadvantage is the need for cathode replacement and anode cleaning at intervals of a few hours to a day.
Clark, Ion Sources for Cyclotrons — Cyclotrons '81, Caen (1981) — p. 3
Editorial note, tabletop extrapolation: Lower arc power and lighter gas both cut sputter erosion, so a small hydrogen source should do far better than the cited heavy-ion interval - but how much better is a measurement, not a scaling law: run the source and log the wear before promising a lifetime.
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Fully-dimensioned bench PIG (Rovey): cathode body machined from a 5.1-cm iron rod, Sm2Co17 magnet (~3 kG surface flux) in a thin stainless sleeve, spot-welded stainless-sheet anode, and a 3.2-mm iron faceplate with a 6.4-mm hole on centerline - producing a continuous 1 mA positive hydrogen-ion beam at 1 mTorr with 5.4 kV / 32.4 W through a 100 kOhm, 100 W ballast.
1 mA positive hydrogen ions at 5.4 kV, 6.0 mA discharge, 32.4 W, 1 mTorr; 100 kOhm / 100 W ballast; ignition <= 1 kV (paper's ignition result)Source quote & editorial note
The cathode body is a 5.1-cm-diameter iron rod that has been machined to the dimensions and geometry shown in Fig. 1. ... samarium cobalt (Sm2Co17) permanent magnet ... surface flux density of approximately 3 kG ... the cathode faceplate is fabricated using the same iron rod as the cathode body. A 3.2-mm-thick, 5.1-cm-diameter disk is cut from the iron rod and machined with a 6.4-mm-diameter hole on centerline. ... a 100 kOhm, 100 W resistor is connected in-line with the power supply to current limit the discharge. ... generate a plasma discharge that yields a continuous 1 mA beam of positively charged hydrogen ions at 1 mTorr of pressure. This operating condition requires 5.4 kV and 32.4 W of power.
Editorial note, tabletop extrapolation: Existence proof that mA-class hydrogen PIG output needs only tens of watts and modest fabrication (machined rod, spot-welded sheet anode). The axial-extraction geometry differs from a cyclotron chimney, so the discharge economics transfer as encouragement - the chimney's own extraction still needs its own validation, and the 1 mA is aggregate hydrogen ions, not mass-analyzed H+.
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Rovey ballast/ignition data: discharge ignites at <=1 kV at all flows; a 100 kOhm series resistor on a 6 kV/200 mA supply stabilizes it; target/discharge current utilization ~25% for H2 (21% He); his flow-to-pressure points: 1 sccm -> 2e-5, 2 -> 5e-5, 3 -> 1.6e-4, 5 -> 3.5e-4 Torr.
I_beam/I_discharge ~ 0.25 (H2); ballast 100 kOhm at mA scaleSource quote & editorial note
the plasma discharge ignites easily at 1 kV or less for all cases ... a current utilization efficiency (ratio of target to discharge current) of 25%
Editorial note, tabletop extrapolation: Use the right utilization figure for the right geometry when predicting a next machine's beam: Rovey's ~25% is axial extraction; Forringer's radial-slit configurations measured I_beam/I_arc of about 0.0005 to 0.0046 - nearly two orders lower, because the slit samples a small part of the plasma - and neither number transfers to a new source without measurement.
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Forringer chimney/slit trade (measured, 40 kV dc puller, 3 sccm H2): the 0.25 x 5.0 mm slit gives 52-227 uA at 50-450 mA arc (I_beam/I_arc ~ 1.0e-3 falling to 0.5e-3) with radial emittance ~25 mm-mrad independent of current; the 0.51 mm slit gives 230-590 uA at only 50-150 mA (~4.6e-3 x I_arc) but emittance grows with current (47 -> 65 mm-mrad). Wider slit = more current per arc-watt; brighter is narrower.
I_beam ~ (0.5-4.6)e-3 x I_arc for 0.25-0.51 mm slits at 40 kV dc extractionSource quote & editorial note
Table 3.4: Slit 0.010" 40 kV, 450 mA, 3.0 cc/min -> 227 uA; Slit 0.020" 40 kV, 150 mA, 3.0 cc/min -> 590 uA
Editorial note, tabletop extrapolation: Start a next machine with the 0.5 x 5 mm slit - at 50-150 mA arc it made 230-590 uA at 40 kV. A fixed-gap Child-Langmuir scaling to a 4 kV dee (V^1.5) would read ~7-19 uA, but treat that as a blackboard exercise, not available beam: RF extraction changes gap, meniscus and phase acceptance, so model the actual central region before booking any of it against the present 3 nA best.
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Chimney machining details from Forringer: slits chamfered 10 deg, relieved 0.010 in deep in a 0.020 in wall leaving a 0.010 in 'tunnel'; the hole chimney is 0.047 in (1.19 mm) diameter with a 60 deg chamfer. The hole chimney's radial normalized emittance (0.66 mm-mrad) ran about 50 percent larger than the slit's (0.44 mm-mrad); a flat plasma boundary best matched the slit beams, a highly concave one the hole beam.
slit land/tunnel 0.25 mm, chamfer 10 deg (slit) / 60 deg (hole); emittance 0.44 (slit) vs 0.66 mm-mrad (hole)Source quote & editorial note
The radial normalized emittance (0.66 mm-mrad) was about 50% larger than that of the slit chimney (.44 mm-mrad) ... The hole in the chimney is 0.047 in (1.19 mm) with a sixty degree chamfer. ... For the slit chimneys, an approximately flat plasma provided the best match for the radial emittance of the experimental beam while somewhat over estimating the size of the beam in z, and for the chimney with a 0.047 in diameter hole a highly concave plasma was found to provide the best match. ... The chamfer in both of the slit chimneys tested was 10 [deg] ... 0.010 in deep (out of a 0.020 in thick chimney wall) leaving a 0.010 in deep 'tunnel'
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 77, 84, 95-97, 112
Editorial note, tabletop extrapolation: The actual machining callouts for a chimney a home shop can cut. The thin-land/outward-chamfer rationale (don't collimate the beam away; the thesis suggests deeper chamfers may raise current) is engineering reading of the source's optimization remarks. The old ~70 percent-of-slit-height beam figure is dropped pending a scan re-read - not found at the cited pages.
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Cathode-anode gap in the NSCL/ACCEL cold-cathode source was anywhere from 1.9 to 3.8 mm and 'is not a critical parameter'; the thesis's practice pairs that with 100-grit cathode sanding (early screwdriver-scratching proved unnecessary) and the essential water cooling of cathode rod and anode base (dg-416's melted-copper lesson).
cathode-anode gap 1.9-3.8 mm, non-criticalSource quote & editorial note
The cathode anode gap was between 0.075" (1.9 mm) and 0.150" (3.8 mm), and is not a critical parameter for the source's operation.
Editorial note, tabletop extrapolation: Generous tolerance on the AXIAL gap - that part of the chimney stack-up doesn't need precision. Concentricity and slit alignment are separate tolerances with their own tighter demands, and the cooling warning stands at any arc power: provide a conduction path sized for continuous arc wattage, or plumb water.
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In Forringer's cold-cathode PIG source, H2+ was below the analyzer's detection at normal operating points (50-350 mA arc, >=2.0 cc/min H2, arc supply in current limit below 3 kV); starving the gas to 0.5 cc/min flipped the arc into a 3.5 kV voltage-limited mode (current fell to 90 mA) and H2+ appeared. One source, one analyzer, detection limit unstated. [Corrected 2026-08-23: earlier wording turned "no H2+ observed" into a recipe for a clean proton beam; the note below says what a builder can and cannot take from it.]
In the measured source: H2+ below detection for flow >= 2 cc/min with arc current-limited; H2+ appears at starved 0.5 cc/min. Not transferable without the source geometry and pumping speed.Source quote & editorial note
Under normal ion source opperating conditions ... no H2+ ions were observed. We were able to observe H2+ ions by lowering the gas supply to 0.5 cc/min.
Editorial note, tabletop extrapolation: Treat gas flow and arc regime as a species TUNING HYPOTHESIS for the reference machine, not as a purity guarantee: 'below detection' in one analyzer does not exclude H2+ at a lower level, says nothing about H3+, and the cc/min thresholds depend on that source's geometry and pumping. Species misidentification propagates into energy, range, resonance interpretation and any radiation assumption, so verify H+/H2+/H3+ in the actual machine - analyzing magnet, time-of-flight, the f = qB/2*pi*m resonance check, or a reaction diagnostic - before claiming a proton beam. Transfer only the method: scan flow and arc regime while directly measuring species; do not assume the direction or the thresholds reproduce in another source.
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This cold-cathode source family has run at 4.5 T in the Harper Medical Cyclotron and at 0.5 T in NSCL test-stand low-field checks; the thesis's test-stand practice: base vacuum in the 1e-6 Torr range (gas off) for consistent starts, with 2.5 sccm of H2 putting the chamber at 4e-5 Torr under 600-800 L/s of turbo pumping.
B operating range 0.5-4.5 T demonstrated; base vacuum ~1e-6 Torr for reliable startsSource quote & editorial note
have been used in magnetic fields as high as 4.5 Tesla in the Harper Medical Cyclotron (and as low as 0.5 Tesla during low magnetic field tests in the NSCL ion source test stand)
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 27, 39
Editorial note, tabletop extrapolation: The reference machine's 0.59 T sits just inside the demonstrated field range - demonstrated at the endpoints, not characterized as uniform performance across it - and its existing turbo and 1e-6-class base pressure match the thesis's start conditions as-is.
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Puller geometry from the same source family: test-stand puller radius 12.7 mm with 5.0 mm minimum chimney-puller gap at 50 kV design voltage; the K100 medical cyclotron puller runs a 2.9 mm minimum gap (at ~20-40 kV RF), with the puller center deliberately offset 0.5 mm from the chimney center.
gap 5.0 mm at 50 kV; 2.9 mm (K100); offset 0.021" between chimney and puller centerlinesSource quote & editorial note
The chimney is centered at (0.000,0.000) and the puller is centered at (0.021,0.000). The minimum gap between the chimney and the puller is 2.9 mm while the gap at the source opening is 3.0 mm, meaning that the beam does not see the peak electric field. [K100 geometry]
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 78, 85
Editorial note, tabletop extrapolation: Gap sets extraction field at fixed voltage, so at a few kV on the dee the chimney-puller gap must shrink below these machines' values to recover useful gradient - but there is no constant-kV-per-mm law to size it by (dg-419): pick a gap, then verify holdoff on the bench with the actual electrodes, finish and RF. The K100's deliberate 0.5 mm center offset - trading peak field at the beam for extraction optics - is the transferable design idea.
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For orbit-code initial conditions, model ions leaving a slit chimney from an approximately flat plasma boundary and a hole chimney from a concave one, at ~35,000 K plasma temperature (the source's stated 'central starting energy' 4.5 eV, i.e. (3/2)kT under its convention); with these methods the author judged Z3CYCLONE predictions adequate 'such that construction of actual cyclotrons can proceed with reasonably prudent confidence'.
T_plasma ~ 35,000 K; kT ~ 3.0 eV, central starting energy 4.5 eV = (3/2)kT (source convention); flat boundary (slit), concave (hole)Source quote & editorial note
We observe that an approximately flat plasma boundary provides the best match to the experimental beams emerging from the 'slit' style chimneys in our study, while a concave plasma boundary (curving toward the source axis) provides a better match for the beam that emerges from the 'hole' style chimney. In all cases, the plasma temperature that provides the best match for experimental beams is approximately 35,000 K (resulting in a central starting energy of 4.5 eV). Using the methods presented in this dissertation, the orbit tracking code Z3CYCLONE is able to predict the beam produced by a cold cathode PIG ion source with adequate accuracy such that construction of actual cyclotrons can proceed with reasonably prudent confidence that the cyclotron will perform as predicted.
Editorial note, tabletop extrapolation: Drop-in starting condition for the reference machine's central-region orbit models: start protons from a flat sheet across the slit with the source's 4.5 eV central energy, not from rest at a point - and sweep the parameters against measured beams per dg-423.
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Siemens Eclipse RDS111 cold-cathode PIG complete working point at 120 uA on target: arc 0.27 A at 550 V (150 W), ignition up to -3 kV on cathodes, 5.5 sccm H2, 0.7 T field, anode slit 0.7 x 5.2 mm, puller slot 1.1 x 5.3 mm at 2.3 mm anode-puller distance, plasma column 4.0 mm dia set by collimators in a 5.0 mm anode bore, Ta cathodes 4.3 mm dia; 800 uA H- extracted (beam-on-post); rebuild interval 120 h, target 300 h.
150 W arc -> 800 uA extracted H- in 0.7 T; slit 0.7 x 5.2 mm; gap 2.3 mmSource quote & editorial note
Arc Current 0.27 A / Arc Voltage 550 V / Arc Power 150 W / H2 Gas Flow 5.5 sccm / Beam-on-Post (Extraction Current) 800 uA (Table 1)
Potkins et al., Improvements to Siemens Eclipse PET Cyclotron Penning Ion Source (2017) — p. 2-3
Editorial note, tabletop extrapolation: The single most relevant commercial datapoint - 0.7 T (nearly the reference machine's field), 150 W arc, sub-amp arc current, hundreds of uA extracted, 120+ hour consumable life. It makes H-: useful as discharge and lifetime context, but it does not quantitatively predict a positive-ion version's H+ output - species fractions, meniscus and extraction all change with polarity, so measure H+ directly.
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Siemens PET-source upgrades, as measured: grooved molybdenum anodes lowered arc power 7% and raised target beam 20% (material and groove tested together, not separated); a cesium getter pill in the cathode gave +26% beam at -25% arc power; thoriated-tungsten cathodes were a net loss; widening the plasma-to-wall 'cool ring' also gained beam - with the printed dimensions carrying an arithmetic slip: a 5.0 mm bore with the column collimated 4.0 -> 3.8 mm gives 0.50 -> 0.60 mm of ring, not the 0.70 previously stated (re-read queued for the true bore).
plasma-to-wall gap 0.5-0.7 mm (H- volume production); Mo grooved anode +20%; Cs pill +26%Source quote & editorial note
anodes made from molybdenum with circumferential groove features lowered the arc power by 7% and increased the target beam current by 20%
Potkins et al., Improvements to Siemens Eclipse PET Cyclotron Penning Ion Source (2017) — p. 3-6
Editorial note, tabletop extrapolation: The cool-ring and Cs tricks are H(-)-specific; the transferable lessons for a positive-ion source are that geometry near the slit dominates output, molybdenum is a sound anode material, and exotic cathode materials earned nothing - with the grooved-anode gain belonging to the whole tested configuration, not to Mo as such.
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Round apertures vs slits are a transmission-vs-current trade — converting the Eclipse anode/puller slits to equal-area round holes raised cyclotron transmission from 19% to 30% but cut target current from 120 to 40 uA.
round aperture = +57% transmission, -67% net current (equal area)Source quote & editorial note
Post-to-foil transmission increased dramatically (from 19% to 30%) but the total target current decreased from 120 uA to 40 uA
Potkins et al., Improvements to Siemens Eclipse PET Cyclotron Penning Ion Source (2017) — p. 3-4
Editorial note, tabletop extrapolation: For a machine starved of axial acceptance a hole source may waste less injected beam, while total current favored the tall slit in the Eclipse test. The reference machine's 1.42 in physical gap suggests but does not establish generous DYNAMIC acceptance - pick slit vs hole from central-region tracking or a measured acceptance/delivered-current comparison, not the gap dimension.
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Cold-cathode PIG V-I regimes as measured on AMIT: below ~250 mA arc the cathodes supply electrons mainly by secondary emission and the impedance is high; as current rises the cathodes heat up and begin supplying electrons thermionically. The paper also reports arc power vs gas flow passing through a minimum near 4 sccm.
AMIT: secondary-to-thermionic transition ~250 mA (that geometry); arc-power minimum near 4 sccm (that source)Source quote & editorial note
For arc currents below 250 mA the electrons are mainly furnished by secondary emission and the impedance is high. When the current increases, the cathodes heat up and begin to supply electrons by thermionic emission
Editorial note, tabletop extrapolation: Staying below the transition keeps the discharge in its high-impedance regime, which is the friendlier load - but 'stable with a simple regulated supply' is a property of the measured V-I curve plus the ballast, not of a current number: measure the tabletop source's own V-I and dynamic behavior over gas flow, and choose ballast and compensation from the measured differential resistance, ignition included.
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PIG thermal budget (IRANCYC-10, ~500 W total at 1.1 A discharge): cathode heads reach 1992 K from ion bombardment, anode peaks at 472 K adjacent to the exit slit, cathode thermal distortion 0.2 mm; 0.007-0.04 kg/s of 18 C water holds everything. Thermionic contribution at 1992 K is only 0.6% of the discharge current.
hot spots = cathode heads and slit region; ~0.5 kW needs ~0.01-0.04 kg/s waterSource quote & editorial note
the maximum temperature of the cathodes are 1992 K, which is far away from the cathode melting point ... an electron current of 0.00706 A at 500 V which is negligible in comparison to the discharge current of 1.10352 A
Zakerhosseini et al., Heat Transfer Study of PIG Ion Source for 10 MeV Cyclotron — IPAC 2016 (2016) — p. 1-3
Editorial note, tabletop extrapolation: At the reference machine's ~100 W arc the cathode heads may or may not run incandescent - temperature scales with T^4 radiation, bombardment distribution and contact conductance, none linearly with arc power. Mount the heads on refractory stems either way, and size the chimney's heat path (copper stalk to a cooled or finned flange) from a small thermal model or a calorimetric test, including what happens on loss of cooling.
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KIRAMS-13 anode-bore calibration: in simulation a 7 mm ID anode maximized electron density and 8 mm gave the highest beam current density on the real machine; above ~9 mm ID, secondary-electron production falls. Their geometry: 20-mm-long anode, Ta cathode discs screwed into holders, ~2 T field.
KIRAMS-13: anode ID optimum 7-8 mm, falloff above ~9 mm; anode length 20 mm; simulated range 6.16-10.1 mmSource quote & editorial note
the anode with 7 mm in inner diameter is demonstrated to be capable of producing the highest density of electrons while the 8 mm inner diameter anode gives the highest beam current density in KIRAMS-13 ... when the anode with inner diameters higher than 9 mm, the number of electron production will decrease ... The cylinder shape anode with 20 mm in length having different internal diameters of 6.16 mm to 10.1 mm, were used in simulation.
Mu et al., Simulation of Electron Behavior in PIG Ion Source for 9 MeV Cyclotron (2015) — p. 3, 5
Editorial note, tabletop extrapolation: A starting range, not a spec: at 0.59 T the electron column is fatter than at KIRAMS's 2 T, so begin near the top of the 7-8 mm range or make the chimney bore an interchangeable insert and find the optimum at the actual field, pressure and arc voltage.
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Alignment sensitivities: an off-center cathode (relative to anode bore and B axis) produces dramatically fewer secondary electrons with shorter confinement lifetimes; extraction is optimized over a mere -0.2 to -1.5 deg of anode (slit) rotation relative to the puller (>50% extraction inside that window), with the puller 2.2 mm from the anode aperture.
cathode-anode-B coaxiality critical; slit-to-puller rotational alignment ~1 deg classSource quote & editorial note
the properly aligned configuration produces significantly more secondary emission electrons ... with the anode rotation angles from -0.2 to -1.5 degree, more than 50% H- beam can be extracted through pullers
Mu et al., Simulation of Electron Behavior in PIG Ion Source for 9 MeV Cyclotron (2015) — p. 4-6
Editorial note, tabletop extrapolation: Two different tolerance classes: build the chimney concentric (pin the cathode discs to the bore, machine in one setup), and provide an external rotational adjustment of the source stalk with sub-degree feel for slit-to-puller aiming. The KIRAMS optimum spanned about a degree, so an adjustment range of a few degrees around nominal is the class to design for - the actual optimum is found on the machine, not inherited.
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A commercial-class 10 MeV PET-cyclotron power budget (CYC2016 design): 1.5 kW internal PIG ion source against 26 kW magnet coil and 14 kW RF consumption; simulated beam after the third accelerating gap ~197 uA at 190 keV from a 40 kV gap voltage.
P_ion_source ~ 1.5 kW (commercial); ~4% of machine wall powerSource quote & editorial note
Coil Consumption Power [kW] 26 ... RF Consumption Power [kW] 14 ... Ion Source Power [kW] 1.5 (Table 1) ... Cavity loss power was calculated 12.7 kW to generate an electric field with 40 kV gap voltage ... Beam energy and current was checked 190 keV, 197 uA after third accelerating gap
Editorial note, tabletop extrapolation: Context datum, not a scaling law: the reference machine's ~0.1-0.2 kW source budget is a deliberate derating of this class of design, but beam current does not scale with source power - capture, acceptance and extraction losses dominate - so estimate current from measured source output and capture efficiency.
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A chimney over a filament converts an open e-bombardment source into a column source: thermionic electrons travel the full chimney to the median plane, ions form in the whole column, and a small aperture (1/16", 1.6 mm) facing the dee releases them into the gap with field lines naturally matched to the first orbit.
chimney aperture 1/16" (1.6 mm) toward dee (Rutgers 12-inch)Source quote & editorial note
The inclusion of a chimney placed on top of the existing design will permit the thermionic electrons to travel to the median plane, thereby generating ions in the entire column. A small aperture, 1/16 of an inch in diameter, opening towards the DEE permits ions to be drawn into the accelerating field.
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 2-3
Editorial note, tabletop extrapolation: The half-step option: chimney-over-filament keeps the reference machine's existing filament supply and adds gas confinement plus a defined 1.6 mm emission aperture. Injection matching to the first orbit remains its own design question (aperture position, puller, phase - dg-348), not an automatic property; a PIG chimney gets the same geometry benefits and deletes the filament, at the price of a new arc supply (dg-383).
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Before freezing a magnet design, survey parameters on a cheap small-scale model magnet (CIT used 2-inch poles for wide surveys, then 6", 9", and final-geometry models) rather than computing everything.
Source quote & editorial note
A series of studies were made on a model magnet with poles 2 inches in diameter. This could be changed quickly and cheaply to give rough data over a wide range of parameters.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 7
Editorial note, tabletop extrapolation: General magnet practice, transferable with its limits: a small bolt-together model surveys geometry cheaply (CIT's 2-inch scans were 'rough data over a wide range'), while saturation and B-H behavior do not scale - same-steel-same-B is what made scaled prediction land elsewhere (dg-1322). The model surveys shape; full-size verification still happens, or FEMM plays the model's role (dg-1089).
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Optimize coil height (and yoke/pole area ratio) by minimizing combined steel + copper + power cost; the cost minimum is flat, so deviating for mechanical convenience costs little.
minimize cost(steel) + cost(Cu) + cost(power) vs coil height and A_yoke/A_poleSource quote & editorial note
The coil height giving the minimum cost was found for a field of 20,000 gauss. Since the cost curve had a flat minimum this resulted in little increase in cost.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 8
Editorial note, tabletop extrapolation: General magnet economics in FORM: minimize steel + copper + power cost for your own prices and expect a flattish minimum near the optimum - CIT's flatness belonged to a 20-kilogauss design at 1950s prices, so re-run the small optimization with today's numbers before leaning on the flatness for convenience deviations.
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The CIT model poles were shimmed until, with 20,000 gauss at the center, the field fell approximately linearly to 96.7% of the central value at 96.5% of the total radius - the point the source identifies with magnetic index n = 0.2. Note the tension the source leaves unresolved: a strictly linear 3.3% drop gives a local n of only ~0.03 at that radius, so their n = 0.2 must reflect the locally steepening slope at the working edge, not the average decrease.
n = -(r/H)(dH/dr) evaluated from the LOCAL derivative of measured H(r); source's profile: H(0.965R) = 0.967*H(0), 'approximately linear', labeled n = 0.2 at the edgeSource quote & editorial note
with 20,000 gauss at the center, produced a field of 96.7 percent of this value at 96.5 percent of the total radius (corresponding to the magnetic index n = .2), with an approximately linear decrease in field from center to edge.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 9-10
Editorial note, tabletop extrapolation: The transferable practice is the method: measure H(r), compute n(r) from its local slope, and place the working radius where n stays in the focusing band - do not set a shim target from endpoint percentages, and do not adopt n = 0.2 as a goal without orbit, phase-slip and extraction analysis.
Cited in: Beam Dynamics: An Interactive Laboratory
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Do not count on holding the field up beyond about 90% of the pole-face radius: the source's shim studies hit that limit because the pole cross-section was too small just below the face - thickening the pole there is the lever they identify.
Source quote & editorial note
Shim studies showed it would be very difficult to hold up the field out to a radius greater than 90 percent of the pole face radius. This was due to the pole cross-section being too small just below the pole face.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 9
Editorial note, tabletop extrapolation: Directly applicable planning figure: budget usable beam radius near 90% of the 8-inch pole (~3.6 in) - and let the machine's own field map set the real number (dg-098's fringe accounting).
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The cited shim study developed a relative field measurement along a radius good to 0.1 percent and used it for the detailed shim work - build the measuring capability before starting shim studies.
Source quote & editorial note
A method of measuring the relative field in the gap at points along a radius to .1 percent was developed and used on later detailed shim studies on this magnet.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 9
Editorial note, tabletop extrapolation: A 0.1% relative radial map (differential Hall probe or flip coil) was that team's entry ticket; derive the next machine's actual requirement from its field and orbit tolerances, and qualify the probe's calibration, positioning, thermal drift and repeatability as part of building the capability.
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Expect the poles to deflect toward each other under magnetic load - the CIT model magnet averaged 0.002 to 0.004 inch - and measure or budget the gap change between field-off and field-on.
Source quote & editorial note
The deflection of the poles under the magnetic load was found to average .002 to .004 inches for the model.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 9
Editorial note, tabletop extrapolation: Historical calibration context, not a prediction: estimate the next machine's load from magnetic pressure B^2/(2 mu0) over the pole area and its structure's stiffness, distinguish per-pole motion from total gap closure, and always shim and map at operating excitation, not cold.
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Verify dimensional stability before committing to high-saturation alloy shims: CIT repeated its Hiperco edge-shim tests and dropped the material after finding it dimensionally unstable.
Source quote & editorial note
The Hiperco tests were repeated but dropped when this material was found to be dimensionally unstable.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 9
Editorial note, tabletop extrapolation: Any exotic Co-Fe edge ring for the next machine's pole edge needs dimensional and magnetic checks after machining, heat treatment, assembly and excitation cycling - modern grades and treatments may behave differently from CIT's stock. Low-carbon steel is the conventional baseline, not a guaranteed adequate answer.
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Before freezing the design, CIT machined a final pair of model poles from the same steel forgings used for the full-scale poles and re-verified the shim performance - repeat the model validation with production-representative pole steel.
Source quote & editorial note
A final pair of model poles was machined out of the steel forgings actually used for the full-scale magnet poles. The results were satisfactory, and the design was frozen.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 10
Editorial note, tabletop extrapolation: Transferable principle: validate on material representative of the production poles - measure coupons from the actual pole stock or the finished poles themselves; same-lot shim stock is a reasonable extra precaution but is beyond what the source demonstrates.
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CIT held the machining of the pole tip to +/-0.0025 inch on almost all dimensions.
tolerance: +/-0.0025 in on pole tipSource quote & editorial note
The machining of the pole tip was held to +/- .0025 inches on almost all dimensions.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 11
Editorial note, tabletop extrapolation: A few-mil pole tolerance is achievable in a good hobby/job shop - derive the next machine's actual requirement from gap sensitivity and the field-uniformity budget, and remember final mapping and shimming absorb what machining leaves.
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When welding cases or fittings around finished coil windings, mask every metal seam (CIT: glass tape) so weld flash cannot reach the insulation.
Source quote & editorial note
Glass tape is inserted along all metal seams to prevent weld-flash from entering the can.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 14
Editorial note, tabletop extrapolation: Directly applicable craft rule for welding on or near a next machine's coil case: glass tape or an equivalent temporary barrier keeps weld flash and spatter out of the can. It does nothing against brazing flux, molten filler or conducted heat - hot work near a wound coil also needs thermal protection and temperature monitoring, or should be finished before winding. [Note revised 2026-08-23: earlier note extended the barrier to 'any welding or brazing'.]
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Design the vacuum chamber to split and withdraw without disturbing the shimmed magnet pole tips, so chamber service never invalidates the field map.
Source quote & editorial note
The chamber parts into two halves in a vertical plane through the center of the magnet, permitting the removal of the chamber without disturbing the magnet pole tips.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 15
Editorial note, tabletop extrapolation: Directly applicable packaging rule: make the next machine's chamber removable or serviceable in place without unbolting pole tips or shims - and still re-verify the field after any reassembly that could have moved iron. Undisturbed tips make the recheck quick, not unnecessary.
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Support the dee on insulating columns 'making it possible to provide a DC bias' - CIT's design summary planned 1000-2000 V (NYO-780 p.75).
dee DC bias 1000-2000 V (NYO-780 summary, p.75)Source quote & editorial note
It is supported on insulating columns, making it possible to provide a DC bias.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 15
Editorial note, tabletop extrapolation: A DC-isolated dee mount costs little at design time and provides the discharge-control knob the era's reports repeatedly reach for (dg-320, dg-680, dg-805). A kilovolt-class bias means the mount and its feed are HV-insulated by design, not as an afterthought.
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Drill numerous holes in pole-tip liners so the volume behind them is pumped instead of trapping gas, as the CIT chamber did.
Source quote & editorial note
Numerous holes are drilled in them to facilitate vacuum pumping.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 19
Editorial note, tabletop extrapolation: Virtual leaks behind liners and skins are a classic small-chamber trap: vent every otherwise-trapped volume on the next machine with holes or slots sized for pumping conductance - checked against RF current paths, structure and field quality - and deburr and clean the openings.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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Helium leak-test every vacuum subassembly individually after manufacture, before installation into the machine.
Source quote & editorial note
Each assembly was leak-tested with a helium mass spectrograph after manufacture.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 20
Editorial note, tabletop extrapolation: Bench-test each next-machine spool, duct, and feedthrough before it disappears into the stack - vacuum-mode helium mass-spectrometer testing is the acceptance method the source used. Rate-of-rise and sniffing are preliminary screens only; keep soap solutions off vacuum-wetted surfaces, and pressurize a vacuum-only part for testing only if it has a documented pressure rating.
Cited in: The Vacuum Budget of a Cyclotron
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In the CIT chamber, only two leaks were detected and both were at gasket seals, attributed to non-uniform gasket thickness - inspect gasketed joints early and control gasket stock uniformity.
Source quote & editorial note
Only two leaks were detected, and these were in the gasket seals. They were believed to be due to non-uniform thickness of gasket material.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 24
Editorial note, tabletop extrapolation: A useful prior for a next machine's leak hunt: check O-ring/gasket joints first - while still testing welds and feedthroughs, since one chamber's tally doesn't make welds innocent; compression, gland condition and damage are additional gasket failure modes beyond thickness.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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Benchmark vacuum health by the pump-down curve from cold: the CIT chamber reached 1e-5 mm in 1 h 45 min and 3e-6 mm in 2 h 30 min from a cold atmospheric start; log your own curve and watch for degradation.
cited system, cold start: 1e-5 mm in 1.75 h; 3e-6 mm in 2.5 hSource quote & editorial note
The vacuum reached was 3 x 10-6 mm of mercury. Starting with cool pumps and the system at atmospheric pressure, the pump-down times were as follows: 1 hour, 45 minutes to reach 10-5 mm mercury; 2 hours, 30 minutes, to reach 3 x 10-6 mm mercury.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 24
Editorial note, tabletop extrapolation: Transferable practice - a recorded reference pump-down curve for the next machine's chamber is the cheapest early-warning leak/contamination diagnostic.
Cited in: The Vacuum Budget of a Cyclotron
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Suppress high-frequency parasitic oscillator modes with resistive (light-bulb) loads inductively coupled to the tube lines, and kill an unwanted low mode with a series-resonant trap from dee to chamber.
Source quote & editorial note
Parasitic modes at higher frequencies than desired for proton acceleration were successfully eliminated with light-bulb loads inductively coupled to the tube lines, and the lower mode ... was avoided by means of a series resonant circuit from dee to vacuum chamber.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 30
Editorial note, tabletop extrapolation: The general methods transfer - coupled lossy loads to damp unwanted modes, and a tuned series trap for a specific mode - but not component values or topology: identify the actual unwanted modes of the LDMOS-driven resonator first, then design the damper/trap for the measured mode, checking its dissipation and its effect on the operating mode.
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Treat sub-scale oscillator models as provisional: CIT's 3/4-scale model indicated six 880 tubes where the full-scale results indicated four would suffice - final RF numbers come from the real geometry.
Source quote & editorial note
results now indicate that four 880's will suffice, while the data from the three-fourths scale model had indicated that six would be necessary.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 29
Editorial note, tabletop extrapolation: Transferable caution - stray capacitance, proportions and device parameters do not scale cleanly; validate a next machine's dee voltage vs drive on the actual resonator, using models as guides.
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Stack removable radiation shielding in two staggered layers so no straight-through cracks remain; where density matters the report's magnetite concrete reached ~200 lb/ft3 with 3000 psi crush strength (its mixture's figures).
magnetite concrete ~200 lb/ft3, 3000 psi at 28 days, ~10% waterSource quote & editorial note
All removable shielding blocks were stacked in two vertical layers so that no straight-through cracks remained.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 43
Editorial note, tabletop extrapolation: Transferable - stagger any shielding blocks on a next machine (concrete, water, borated PE) so seams never line up with the beam plane.
Cited in: Shielding a Small Cyclotron
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Interlock access doors and enclosures so they cannot open without turning off the cyclotron oscillator or moving the magnetic field off its resonance value.
Source quote & editorial note
they cannot be opened without turning off the cyclotron oscillator or reducing the magnetic field from its resonance value.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 44
Editorial note, tabletop extrapolation: Directly applicable: interlocking RF-enable to the enclosure door is the cheap, classic scheme. Prefer the oscillator-off condition as the gate - an off-resonance field reduces acceleration but leaves RF and high voltage energized, so field detuning alone is not a conservative personnel interlock.
Cited in: Shielding a Small Cyclotron
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In a mixed copper/aluminum/steel water loop, add a corrosion inhibitor: CIT found trace dissolved copper provoked attack on the aluminum and steel (their chromate dose is the report's recipe - re-read queued; chromate is restricted today regardless).
1/3 oz sodium chromate per gallon (historic; chromate now restricted)Source quote & editorial note
requires the addition of an inhibitor to reduce attack on the aluminum and steel provoked by the presence of minute quantities of copper in the water.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 53
Editorial note, tabletop extrapolation: Directly applicable chemistry for any next machine's water loop touching Cu plus Al: pick a modern inhibitor for the actual alloy set, water chemistry and temperature - the transferable fact is that trace copper is the aggressor, so the loop needs treatment even when each metal alone would be fine.
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Water-cool high-current terminals and fit them with thermal switches that trip the supply before the terminals overheat.
Source quote & editorial note
All the adapters on the coil terminals are water cooled and supplied with thermal switches to protect the coil terminals from overheating.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 56
Editorial note, tabletop extrapolation: Directly applicable - thermal cutouts on a next machine's coil terminals/lugs (and dee stem cooling) are cheap insurance against a loose-joint meltdown.
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Guard diffusion/high-vacuum pumps with gauge-controlled automatic valves that close when a leak exceeds what the pump can handle - the report's rig used compressed-air actuation.
Source quote & editorial note
The valves are automatically operated by compressed air cylinders and are controlled by vacuum gauges so that they will close when a leak occurs which the pump is not able to handle.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 58
Editorial note, tabletop extrapolation: Directly applicable: an interlocked isolation valve (even a spring-loaded solenoid gate) protects a next machine's diff or turbo pump from a chamber let-up - with closure speed and actuation chosen for the pump being protected.
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Make demountable RF joints with strips of thin soft copper sheet backed by foam-rubber pads under clamp pressure; the strips deform to surface irregularities and multiply the contact area for RF current.
Source quote & editorial note
good contact is established by the use of strips of thin soft copper sheet backed by foam rubber pads.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 10
Editorial note, tabletop extrapolation: The cheap 1948 equivalent of RF finger stock for external, low-temperature joints - removable housing panels and line covers. For vacuum-facing or high-current joints (dee-stem clamps), use vacuum-compatible spring contacts or engineered clamps with verified pressure and RF heating: ordinary foam rubber outgasses and relaxes.
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To minimize RF power losses, the 184-inch design copper-plated all steel surfaces exposed to RF fields.
Source quote & editorial note
To minimize rf power losses, all steel surfaces exposed to rf fields are copper-plated.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 10
Editorial note, tabletop extrapolation: On a next machine keep steel (chamber walls, bolts, pole faces) out of RF current paths or plate/line it with copper - Q and dee voltage per watt are at stake; how much a given steel surface costs is a measurement or model result for that geometry.
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Size dee-to-ground vacuum clearance from RF voltage the way the 184-inch did: a 3-inch minimum at the hot open dee end for 50 kV RF, relaxing to 2 inches at the supported (low-voltage) end - informed by their bench result that a polished 0.080-inch copper gap held 50 kV at 13 Mc and ~5e-6 mm.
184-inch design points: 3 in at 50 kV (open end), 2 in (supported end); bench: 0.080 in polished Cu gap held 50 kV at 13 Mc, ~5e-6 mm - NOT a linear kV/inch lawSource quote & editorial note
the vacuum gap be sufficient to withstand 50 kilovolts rf at the accelerating gap. Consequently, a minimum of 3" spacing was employed in the vicinity of the open front end of the dee; near the rear end (i.e. supported end) a minimum of 2" was allowed. ... [a] 0.080" gap between copper or copper-plated surfaces having a reasonable polish would hold a maximum of 50 kilovolts at 13 mc at a pressure of about 5 x 10-6 mm
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 10
Editorial note, tabletop extrapolation: Do not scale these linearly: vacuum holdoff is nonlinear in gap and dominated by geometry, finish and conditioning (their own bench gap held the same 50 kV across 0.080 inch). Set a next machine's clearance by electrostatic analysis of the actual geometry with conservative peak-field limits, then prove it by conditioning at full voltage.
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Qualify feedthrough/support insulators before installation on a resonant test line that develops full RF voltage from a small driver: the 184-inch group developed over 50 kV at 13 Mc across the insulator with a 5 kW oscillator, and found air-blast cooling necessary under the most severe tests.
Source quote & editorial note
Over 50 kilovolts rf could be developed across the insulator at 13 mc by a 5 kilowatt oscillator. Under the most severe test conditions, air blast cooling of the insulators was found necessary.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 13
Editorial note, tabletop extrapolation: A bench resonator lets the builder soak-test dee-stem insulators at full 5-13 kV RF from modest drive - how modest depends on the fixture's measured loaded Q (constant-Q scaling of the cited point suggests tens of watts at 5 kV but hundreds at 13 kV), so measure Q and compute the drive rather than assuming it.
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Budget vacuum RF gaps from bench data, then derate for surface roughening: an 0.080-inch polished copper gap held 50 kV at 13 Mc and 5e-6 mm on the bench (625 kV/in; 40 kV was the design value), while the discharge-roughened operating unit held ~30 kV over its 0.060-inch gap - 500 kV/in, about 20% lower in average field.
bench: 50 kV / 0.080 in = 625 kV/in (polished Cu, 5e-6 mm, 13 Mc); design ~80% of bench; roughened unit: 30 kV / 0.060 in = 500 kV/in (~20% field derate)Source quote & editorial note
a .080" gap between copper or copper-plated surfaces having a reasonable polish would hold a maximum of 50 kilovolts at 13 mc at a pressure of about 5 x 10-6 mm.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 13
Editorial note, tabletop extrapolation: Directly applicable breakdown data for setting a next machine's dee-to-liner and puller gaps at 5-13 kV - with the derate compared in FIELD, not voltage (the two units had different gaps), and remembering vacuum RF hold-off does not scale as fixed kV-per-gap: bench-verify the actual geometry (dg-419).
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Bring cooling water to electrodes at RF or DC bias potential through several-foot lengths of flexible insulating (polyethylene) tubing carrying treated low-conductivity water.
Source quote & editorial note
The water circuit is completed to ground potential by means of sets of flexible polyethylene tubing, each several feet long. Treated water of low conductivity is used.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 13
Editorial note, tabletop extrapolation: Applicable if the next machine's dee or stem is water-cooled while biased - but hose length plus DI water is the historical arrangement, not a sufficiency proof: calculate the water-column resistance at worst-case conductivity (DI water degrades in service - monitor it), include RF capacitive current through the column, and ground/interlock accordingly.
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Determine transmission-line lengths, effective dee capacitance, and RF power on a scale model of the complete resonant system before construction: quarter scale means frequency x4 and all L and C divided by 4 (the quoted scaling); the 184-inch model program's measured companions - power x2 and Q x 1/2 for equal voltage, and an effective dee capacitance well below static (500 vs 1000 pF) - are the report's results.
1/n scale -> f x n, L and C / n (quarter scale measured: power x2, Q x 1/2)Source quote & editorial note
For reasons of convenience, a quarter scale was chosen. The resonant frequency is then increased fourfold and all inductances and capacitances are reduced by a factor of four.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 14
Editorial note, tabletop extrapolation: Transferable method: prototype a next machine's resonator at reduced scale with a VNA - remembering effective dee capacitance is not the static value, which is exactly what the model run is for.
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Expect small dimensional errors in RF models and layouts to accumulate - the quoted case: about two inches of cumulative model error produced a transmission-line-length discrepancy, with consequences the report details (scan re-read queued); build in adjustment range.
Source quote & editorial note
The evident discrepancy in transmission line length was eventually traced to a cumulative error of about two inches in various small errors in model dimensions.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 22
Editorial note, tabletop extrapolation: Directly applicable: give a next machine's resonant line or tank a deliberate tuning range - trombone section, tuning vane, trimmer capacitor - instead of trusting calculated dimensions to land the frequency.
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Check for a re-entrant cavity resonator mode between the two magnet pole pieces with the vacuum tank walls as the return circuit; the 184-inch found one near its lower frequency limit and suppressed it easily by strapping the pole pieces together.
Source quote & editorial note
disclosed a re-entrant cavity resonator mode between the two pole pieces of the magnet with the vacuum tank walls as the return circuit resonant near the lower frequency limit. This was easily suppressed by strapping the pole pieces together.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 22
Editorial note, tabletop extrapolation: The pole-chamber geometry of an 8-inch machine forms the same class of parasitic cavity - sweep or model the assembled structure, and add a verified pole-to-pole RF bond if a mode lands near the operating band; don't strap preemptively, since added straps can perturb the intended RF structure or form current loops.
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Cure resonant-electron/multipactor discharges in large volumes around the dee by cutting down the free volume with perforated grounded shields, adding a grounded dummy dee, and applying negative DC bias to the dee.
Source quote & editorial note
All discharges were eliminated by cutting down the available volume by means of perforated shields around the sides of the dee, by adding a grounded dummy dee and by applying a negative bias to the dee.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 23
Editorial note, tabletop extrapolation: Directly applicable - the 1948 combination that cleared THAT machine's discharges: reduced free volume (perforated shields preserve pumping speed), a grounded dummy dee, and negative dee bias. On a new machine, apply the elements as diagnosis suggests (dg-1273's discrimination between multipactor and gas discharge) rather than as one obligatory bundle - though all three are cheap to design in from the start.
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In the 184-inch rotary-condenser geometry there was sufficient magnetic field to allow a Philips-gauge (Penning) discharge when positive bias was applied, so negative bias was imperative there - magnetic field threading an RF gap can sustain a Penning discharge with the wrong bias polarity.
Source quote & editorial note
There is sufficient magnetic field at the rotary condenser to allow a Philips gauge discharge when positive bias is applied; a negative bias is therefore imperative.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 23
Editorial note, tabletop extrapolation: The next machine's dee sits in 0.59 T, so if a DC bias is used to kill discharges, start negative on the strength of this precedent - then verify empirically: whether a Penning discharge ignites depends on the E/B geometry and pressure, not the field alone.
-
Mount brittle ceramic insulators so they carry only pure tension or pure compression, never shear: the 184-inch put its upper two dee insulators in pure compression and lower two in pure tension, and after a year of service with no trouble whatever - despite fragility in shear evident at assembly - judged the care 'thus well justified'.
Source quote & editorial note
the upper two insulators are under pure compression, the lower two under pure tension. ... The rf insulators have given no trouble whatever since installation one year ago, though at the time of assembly, their fragility was evidenced insofar as shear forces were concerned. The care taken in insuring that only pure tension and compression forces would be applied was thus well justified.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 24
Editorial note, tabletop extrapolation: Directly applicable to a next machine's dee-stem standoffs and feedthroughs: arrange the support geometry (threaded rods, spherical seats) so ceramics never see bending or shear - prefer compression where practicable, avoid point loading, and respect the manufacturer's tensile rating, which is far below the compressive one.
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Magnetically shield the RF power stage near the magnet: a 1/4-1/2 inch steel enclosure cut a 140-gauss fringe field to under 20 gauss (plus a 1/2-inch sleeve at the tube), verified on a 1/16-scale replica; budget for the magnetic force on the box (450 lb there).
1/4 in steel walls, 140 G -> <20 G; force on enclosure 450 lbSource quote & editorial note
the inner face, or back, is made of 1/2 in steel ... this house serves as a magnetic shield for the oscillator tube. A crude replica (1/16 size) was tested by the magnetic measurements group ... using the 1/16-scale 184-inch model magnet, and this shielding was found sufficiently effective, the field being cut from 140 Gauss to less than 20 Gauss. This is further reduced at the 9C21 elements by means of a 1/2 in steel sleeve slipped over the cooling jacket. The magnetic force on the oscillator box amounts however to 450 lbs.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 20
Editorial note, tabletop extrapolation: LDMOS amplifiers, fans and ferrite-cored parts near a 0.59 T magnet want a steel housing - and the source's method is the transferable part: they verified the shielding on a scale model before committing, and budgeted the large attractive force on the box. Measure the fringe field at the amplifier location and check the housing's effect; do not assume a thickness.
-
Calibrate dee-voltage-per-watt expectations from this report's machine: its oscillator produced 15 kV peak on the dee at 10 Mc (9 kV at 20 Mc) for 6 kW input at ~70% average efficiency; the report elsewhere identifies the machine and tube complement (scan re-read queued for those details).
15 kV dee at 10 Mc for ~6 kW input, ~70% efficiency (37-inch dee, C ~ 300 pF)Source quote & editorial note
It would produce 15 kv peak volts on the dee at 10 me and 9 kv at 20 me with 6 kw input. It averages around 70%.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 4
Editorial note, tabletop extrapolation: A benchmark near the reference machine's 9 MHz - and transferring it runs through the resonator parameters: scale by the actual dee capacitance and Q via dg-313's formula, not by watts-per-kV alone.
-
Provide a tuning vane - a movable copper sheet with flexible end connections facing the resonant line - to trim the resonant frequency without rebuilding the line; on the source machine the vane's range was about 6%.
vane travel -> ~6% frequency trim of the resonant lineSource quote & editorial note
The upper and lower frequency limits can be varied together about 6% by a tuning vane which varies the impedance of the transmission line. It is a movable copper sheet with flexible end connections.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 5
Editorial note, tabletop extrapolation: Directly applicable to a fixed-frequency machine: a vane gives few-percent trim to land the dee resonance on the magnet's cyclotron frequency. The range you get depends on your line's geometry - size the vane by calculation and keep a fallback adjustment (dg-665's trombone/trimmer).
-
Orient demountable RF-housing joints so current flows parallel to the joint wherever possible - such joints needed no particular contact care in the cited housing - and use rubber-backed copper sheet (the rubber supplies pressure, the copper makes the contact) where current must cross a joint.
Source quote & editorial note
The horizontal joints are also rubber backed, but no particular care is necessary to insure contact as the current flow is parallel to the joint.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 6
Editorial note, tabletop extrapolation: Plan a next machine's panel seams along the RF current direction and spend the contact-strip effort on the seams that cross current - remembering fringing and return currents can cross nominally parallel seams, so verify with a current map or by checking seam temperatures at power.
-
The cited construction ran bare steel in the RF path at 10 Mc but needed copper plating when tried at 20 Mc - at any frequency, estimate conductor loss from surface resistance (~ sqrt(f*mu/sigma), so steel's permeability hurts badly) before leaving steel in a high-current path.
Source quote & editorial note
It was tried this way at 20 megacycles, but it soon became necessary to copper plate most of the surfaces.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 6
Editorial note, tabletop extrapolation: At 9 MHz bare steel may survive, but plating (or copper construction) is cheap insurance for Q and hot spots - decide from an Rs estimate and verify temperatures at full power rather than reading 10-vs-20 Mc as a safe cutoff.
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The 37-inch built low-inductance grid/bypass capacitors as flat metal rings with radiused (1/8 inch) edges over 0.010-inch polystyrene - good in their service for >15 kV DC and ~1500 V RF, but only while the metal parts stayed cool.
0.010 in polystyrene sandwich -> >15 kV DC, ~1500 V RF when coolSource quote & editorial note
Polystyrene of this thickness used in this manner will stand over 15,000 volts DC and approximately 1500 volts r.f. provided the metal parts remain cool.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 8
Editorial note, tabletop extrapolation: A historical construction worth knowing, not a transferable rating: the implied DC stress is ~59 kV/mm, so the numbers belong to that geometry, cooling and test practice. For a next machine's RF chain, prefer certified RF/HV capacitors; if building, take the dielectric's own data (Kapton is often lossier than polystyrene or PTFE at RF), derate heavily, design creepage and corona control, and test thermally and at withstand voltage.
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To prevent intermittent (grid-blocking) oscillation in a self-excited tube oscillator, such oscillations will usually not occur if the resonant system's time constant exceeds ten times the grid-leak RC - keep R_grid*C_grid below about one-tenth of the resonator's amplitude ring-down time.
tau_resonant (amplitude decay ~ 2Q/omega) > 10 x R_grid*C_grid (the source's usually-sufficient heuristic)Source quote & editorial note
Such oscillations will usually not occur if the time constant of the resonant system is more than ten times the time constant of the grid leak grid condenser network.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 8
Editorial note, tabletop extrapolation: The bias-network-vs-resonator time-constant race is the transferable idea for any self-excited driver on a next machine's dee - for transistor circuits the mechanisms are topology-dependent, so do a small-signal/transient stability analysis rather than relying on this RC ratio.
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In loop-coupled oscillators, minimize non-mutual loop inductance (large-diameter tubing, shortest leads). The 37-inch's computed plate-filament phase shift was 21 degrees, corrected by a series capacitor in the filament loop - 140 pF by calculation, ~220 pF as installed (the excess neutralizes the filament-choke inductance) - made adjustable and trimmed for minimum plate current.
series C in filament loop: 140 pF computed, ~220 pF installed incl. choke neutralization; trim for minimum DC plate current at the required dee voltageSource quote & editorial note
The loops are therefore made of large diameter tubing and the length of tubing which is not serving as mutual inductance in the dee stem circuit is kept at a minimum. ... the total shift between plate and filament voltages is 21 [deg]. The correction is made in the filament circuit by inserting a capacitor of 140 uuf (c, in Figure 3) in series with the loop. ... The capacity (c, Figure 3) used in the actual installation is around 220 uuf, part of which serves to neutralize the inductance of the filament chokes. It was made adjustable over a small range and varied until minimum plate current was obtained.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 9
Editorial note, tabletop extrapolation: Minimum-DC-input trimming is a meterable, practical phasing procedure for a feedback-coupled driver - hold the required RF output/dee voltage while trimming, or the 'minimum' you find is just reduced drive; other topologies need their own phase-margin analysis.
-
Survey the RF system for secondary resonances near harmonics of the operating band: the 37-inch's plate-loop mode could not be raised above 38 Mc and coincided with 2x the fundamental at one tuning point - a variation predicted and demonstrated to lose most of the ions at 19 Mc - and was cured by adding about 15 pF, moving the mode to 34 Mc.
keep f_parasitic away from n x f_operating where the mode is coupled; 15 pF moved 38 -> 34 Mc in the cited systemSource quote & editorial note
the frequency of the plate loop could not be made higher than 38 megacycles. At one point this will coincide with the first harmonic. ... It has been predicted theoretically and demonstrated experimentally that most of the ions can be lost by such a variation if the ions reach their final radius at 19 megacycles. ... It was therefore necessary to add about 15 uuf to this circuit, which lowered its frequency to 34 megacycles.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 10
Editorial note, tabletop extrapolation: Even at fixed frequency, sweep the next machine's system for modes near 2x and 3x of 9 MHz; a found mode matters only if it is coupled and excited - measure its effect on dee voltage before detuning it, since an added capacitor perturbs the mode structure too.
-
Put a controllable series element in the oscillator HV supply lead as an emission/current limiter - the 37-inch used an 893 triode with 20 kW plate dissipation - to protect the RF power stage when discharges occur in the tank and condenser.
Source quote & editorial note
Provision was made for arbitrary amplitude modulation by inserting an 893 triode in series with the power supply lead. As yet it has not been used for this purpose, but as it has a 20 kw plate dissipation, it has been used as an emission limiting device to protect the oscillator tubes when discharges occur in the tank and condenser.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: The principle transfers: fast current limiting or foldback in the LDMOS drain supply, plus a VSWR trip, is the modern form. It reduces fault energy; it is not immunity - reflected-power overvoltage and drain transients are separate failure paths needing their own protection (dg-338).
-
Expect an electron-oscillation discharge that lives only below an extinction voltage near 500 V RF and blocks voltage build-up even at 1e-5 mm Hg; the 37-inch eliminated it with a sweeping field - biasing the dee, transmission line and condenser stator a few hundred volts POSITIVE - and the bias, unexplained, roughly doubled their beam.
discharge sustained only below ~500 V RF (the source's extinction neighborhood); any sweeping field kills it - the 37-inch used a few hundred volts positive biasSource quote & editorial note
Above this voltage, which is in the neighborhood of 500 volts, the discharge is rapidly extinguished as electrons can no longer oscillate. However, the discharge is usually intense enough, even at 10-5 mm of Hg to prevent the voltage from building up to this extinction value. Such a discharge can be eliminated by a sweeping field obtained in any manner. The sweeping field was obtained on the 37-inch cyclotron by biasing the dee, transmission line, and condenser stator parts a few hundred volts positive.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: The single most relevant discharge fact for the reference machine: its ~1.3 kV dee lives just above this regime, and the 5-13 kV upgrade must punch through it during every start - plan for a bias supply on the dee from day one, and note the source's polarity (positive on the 37-inch; dg-320's machine used negative - both worked, because any sweeping field defeats the resonance).
-
Keep RF-exposed electrode spacings along the magnetic field short: at 20 Mc an electron gains ~30 eV over a 5 cm path, so paths of ~20 cm sustain ionizing oscillation discharges while the short dee-region paths gave no trouble.
at 20 Mc, ~30 eV in 5 cm; danger paths ~20 cm; safe paths < ~5 cm (worse at lower f)Source quote & editorial note
At 20 megacycles the space between electrodes which will allow an electron to reach an energy around 30 volts in 5 cm. There are very few paths, along the magnetic field, in the neighborhood of the dee that are greater than this, so no trouble has occurred in this region. In the rotary condenser however, most of the paths are of the order of 20 cm. Electrons oscillating in this space can reach efficient ionizing energies long before their amplitude becomes equal to the distance between electrodes.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: Directly applicable geometry rule - at 9 MHz electron oscillation amplitudes are larger still, so keep open RF-exposed volumes and along-field gaps in the next machine's chamber small or shielded.
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If bias alone cannot quench the low-voltage discharge, drive the system through the critical low-voltage region with a small independent 'tickler' oscillator - which, not deriving its excitation from the load, can push the main self-excited oscillator over the critical voltage.
Source quote & editorial note
Since the tickler oscillator does not derive its excitation from the load, it can drive the main oscillator over the critical voltage.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: With an externally driven LDMOS chain the analogue is a controlled fast RF ramp through the low-voltage (multipactor-prone) band - with vacuum, arc and reflected-power monitoring, since driving through a discharge can reflect hard; there is no self-excited handover in a driven architecture.
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A few-hundred-volt positive dee/line bias doubled the 37-inch beam current for reasons then unexplained - worth one experiment, but only where no magnetic-field region can sustain a Penning discharge (the 184-inch later required negative bias).
Source quote & editorial note
For reasons which are not clearly understood this bias usually increases the size of the beam by a factor of two or more.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: Conditionally applicable - and 'try both polarities' is a controlled test, not a knob: use an RF-rated bias network with proper isolation and discharge paths, current and arc monitoring, and vacuum interlocks, and assess Penning-discharge conditions (crossed E and B regions) before applying either polarity. The dee's RF stored energy does not care about the bias supply's current limit.
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Characterize your RF circuit cold: measure dee/anode-to-ground capacitance with an impedance bridge, subtracting measured lead capacitance (29 pF deducted in the cited measurement, quoted +/-2 pF on that bridge and fixture).
Source quote & editorial note
The measurements were made with G-R Impedance Bridge, Type 650-A Serial #1977, and are +/- 2 uuf. Lead capacity of 29 uuf has already been deducted.
Anderson, 184″ Cyclotron: Oscillator Capacitance Measurements — MDDC-964 (1947) — p. 3
Editorial note, tabletop extrapolation: A modern LCR meter with lead-nulling does the same job on the reference machine's dee stem. C-to-ground alone doesn't predict the ~9 MHz resonance - combine it with the stem inductance (or a distributed model), then confirm the assembled resonance with a low-power VNA; a kHz-range LCR reading can differ from the effective RF capacitance.
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Scan a bombarded target assembly past a 1/8-inch slot in lead bricks with a counter behind it to map where beam really struck: Berkeley's scan found 21 mR/hr on the foil holder's top outside edge and 18.5 mR/hr on the foil just above the median plane - the strike geometry, not just the target, shows up.
Source quote & editorial note
a high intensity point (21 mr/hr) on the top outside edge of the copper foil holder, another high intensity point (18.5 mr/hr) on the foil just above the median plane
Reyenga, 184″ Cyclotron: Radiation Measurement of Breech Load Probe Head — MDDC-982 (1947) — p. 3
Editorial note, tabletop extrapolation: At nA currents and sub-MeV energies on ordinary holder metals, residual activation of the hardware is small where it occurs at all (thresholdless capture and deuteron operation excepted - the standard scoping). The lesson transfers regardless: check holder edges and apertures for beam strike with film, phosphor, or discoloration, because a large fraction of the beam can miss the target.
Cited in: Shielding a Small Cyclotron
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If the beam dies short of design radius, check the n = 0.2 radius first: the 184-inch beam spread vertically and vanished at 81.5 in (design 85 in), closely matching where magnetic measurements put n = 0.2 - a machine-specific correlation with the nu_r = 2*nu_z coupling resonance, not a universal loss boundary (linear weak-focusing stability itself runs 0 < n < 1).
n = -(R/H)(dH/dR); at n = 0.2 (smooth approximation) nu_r = 2*nu_z - a resonance worth suspecting, not an automatic wallSource quote & editorial note
The autographs indicate a rapid spreading vertically of the beam at about 81 1/2 inches. This agrees quite closely with the point at which n = 0.2 from magnetic measurements.
Editorial note, tabletop extrapolation: Fully applicable as a diagnostic: map B(r) on the bench, compute n(r) and the tunes, and if the reference machine's beam stalls early, the n = 0.2 crossing is suspect number one - but confirm with tracking and check field-error resonances and aperture before moving the target radius.
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The historical vertical-envelope diagnostic: bombard U-slotted 1/16-in copper targets (slot widths 2.5-4.5 in bracketing the beam) with the deuteron beam for 1-3 minutes, remove them, and radioautograph to see where beam hit - an activation-based method: deuterons on copper make Cu-64/Cu-66, so reproduction needs activation estimates, surveys and handling procedures, not 'zero electronics' innocence.
Source quote & editorial note
bombarded with a large deuteron beam for about 1 to 3 minutes, removed from the tank and radioautographs were taken to determine where the beam was hitting.
Editorial note, tabletop extrapolation: Copy the slotted C-target geometry but read it with a vacuum-compatible phosphor/scintillator viewed through a window (validate its spatial response) instead of activation film; a set of slotted witness targets at different radii still gives the whole vertical envelope in a few runs.
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To test whether multiple 'pips' per beam pulse are precession rather than source noise, the 184-inch group added a second RF-shielded probe 155 degrees away: structure that keeps the orbit-model phase relation between azimuths supports precession, while common-mode structure points to source or RF fluctuation.
Source quote & editorial note
in an effort to determine more definitely that the peaks, or 'pips,' shown in synchroscope photographs of the beam current are caused by precession of the beam. ... [an auxiliary probe] shielded for RF pickup, was introduced into the main vacuum tank through a Wilson seal on the port near the ion source in such a manner as to generate a 155 deg angle with the regular probe.
Yeater, 184″ Cyclotron: Synchroscope Beam Pictures on Two Probes — MDDC-987 (1947) — p. 3
Editorial note, tabletop extrapolation: The two-azimuth comparison transfers to any machine: it is a test, not a verdict - accept the precession reading when the measured inter-probe phase agrees with an orbit model and controls exclude RF pickup and coherent source modulation (which can also arrive with a fixed offset).
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Build beam probes as RF-shielded copper fingers entering through a Wilson seal so radial depth is adjustable under vacuum - Berkeley added a whole second diagnostic probe this way without breaking vacuum architecture.
Source quote & editorial note
An auxiliary copper probe, shielded for RF pickup, was introduced into the main vacuum tank through a Wilson seal on the port near the ion source ... made adjustable as to its radial depth
Yeater, 184″ Cyclotron: Synchroscope Beam Pictures on Two Probes — MDDC-987 (1947) — p. 3
Editorial note, tabletop extrapolation: Exactly the right probe pattern for the reference machine's chamber: an O-ring/Wilson-sealed sliding shaft with grounded coaxial shield tube and a defined exposed collector. Near a 9 MHz dee an unshielded probe's reading is dominated by RF pickup superposed on any beam signal - shield, then verify with beam-off RF-only background runs and filtering before crediting the remainder as beam.
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For first detection of a weak deflected beam, the 184-inch found film on the probe best: compare exposures with deflector on and off - their ion-chamber 'detection' could not be reproduced, but film showed the displacement.
Source quote & editorial note
The best detection of the beam deflection was made by mounting X-ray film on the probe and exposing it to both the undeflected and deflected beam.
Sewell, 184″ Cyclotron: Vertical D.C. Electrostatic Deflector — MDDC-1051 (1947) — p. 2
Editorial note, tabletop extrapolation: Start extraction commissioning with on/off comparison images - film or a scintillator-plus-camera at the channel exit - alongside a shielded Faraday collector: integrating detectors trade time for sensitivity and ignore RF pickup, while a well-guarded electrometer is also capable of picoamps when the noise is managed. Use both; agreement is the commissioning signal.
Cited in: Experiments by Energy Band
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Do not build a deflector septum from 0.002-inch copper foil supported as the 184-inch first tried: sparking between the HV electrode and the foil locally heated and badly warped it in one run - size and support the septum to survive spark heating, not just beam heating.
Source quote & editorial note
There was considerable sparking between the HV electrode and the .002 inch copper foil. The copper foil was warped badly ... The 0.002 inch copper foil supported in this manner is not suitable for this job.
Sewell, 184″ Cyclotron: Vertical D.C. Electrostatic Deflector — MDDC-1051 (1947) — p. 2
Editorial note, tabletop extrapolation: A next machine's septum should be sized against the deflector's stored spark energy and thermal impulse, then tensioned or heat-sunk accordingly - conditioning sparks are part of deflector life, and the septum edge is where they concentrate. Thickness follows from that calculation, not from a fixed minimum.
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An in-tank DC electrostatic deflector electrode held about 60 kV in the operating 184-inch cyclotron - amid magnetic field, RF, and beam - a demonstrated 1947 operating value (fed, per the report, through a current-limiting series resistor; scan re-read queued for its value).
Source quote & editorial note
Approximately 60 kv could be held on the high voltage electrode of this deflector.
Sewell, 184″ Cyclotron: Vertical D.C. Electrostatic Deflector — MDDC-1051 (1947) — p. 2
Editorial note, tabletop extrapolation: Compute the next machine's required deflector field from beam rigidity, channel length and allowed interception - then design insulation, clearances and stored-energy limiting for that voltage in its own right. The series spark-limiting resistor is worth copying; the assumption that deflector HV is low-risk is not.
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Do not fight the n = 0.2 resonance for the last few percent: Berkeley POSTPONED accelerating past that radius because the available ion energy there was already within 5 percent of the system maximum (the specific radii and the n = 1 identification are the report's: scan re-read queued).
E_max at radius where n = 1; usable beam ends near n = 0.2Source quote & editorial note
accelerating particles past the radius where n = 0.2 in the 184-inch cyclotron has been postponed, since the available energy of the ions at this radius is within 5 per cent of the maximum of the system
Editorial note, tabletop extrapolation: Budget a next machine's energy at the n = 0.2 radius, not the pole edge - and where shims can push the n = 0.2 contour outward, that buys usable energy more surely than chasing radius into the fringe (dg-152's taper rule is the design form of the same point).
Cited in: Beam Dynamics: An Interactive Laboratory
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At n = 0.2 the coupling resonance omega_z = omega_r/2 converts radial oscillation energy into vertical oscillation at up to double the amplitude - and machines with low accelerating voltage (many turns per inch) build it up rapidly.
omega_r = sqrt(1-n)*omega_0, omega_z = sqrt(n)*omega_0; at n = 0.2, omega_z = omega_r/2 (the coupling resonance); the amplitude transferred depends on coupling strength and crossing speed - the doubling figure is the report's estimate for its machineSource quote & editorial note
It must be kept in mind for systems having low accelerating voltages similar to the 184-inch cyclotron, that the ions will rapidly increase the amplitude of their vertical oscillations at the point where n = 0.2.
Editorial note, tabletop extrapolation: The reference machine's few-kV dee means many turns near any resonance radius - the slow-crossing regime the quote warns about. Keep n below 0.2 over the whole usable radius (the mapped check, dg-138), and give the dee aperture real margin over the expected radial oscillation amplitude.
Cited in: Beam Dynamics: An Interactive Laboratory
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Localize where beam dies by surveying activation of dee edges and liners: a sharp radioactivity peak on the dee lip at exactly 82 in confirmed the vertical-loss radius independent of target experiments.
Source quote & editorial note
a sharp peak of radioactivity was found on the dee lip at the 82-inch radius, which gave additional evidence that the beam was spreading vertically in this region.
Editorial note, tabletop extrapolation: At tabletop energies activation of ordinary structural metals (copper, steel, aluminium) is small and short-lived where it occurs at all - thresholdless (p,gamma) capture and any deuteron operation are the exceptions - so a survey of the dee lip may well find nothing; a cheap wipe survey costs little and settles it. The localization logic transfers regardless: line the dee aperture with removable witness strips (paper, phosphor, anodized Al) and read burn or discoloration marks to find the loss radius. A bombarded target is a separate question and is surveyed on its own terms (dg-1041). [Corrected 2026-08-22: previously 'No activation at tabletop energies', an absolute the site's own safety pages contradict.]
Cited in: Shielding a Small Cyclotron
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Probe-current fine structure carries orbit-center information: the minor-pulse frequency agreed quite well with the calculated precession frequency of the orbit center about the magnetic center - in the smooth weak-focusing model omega_prec = (1 - sqrt(1-n))*omega_0, so pip counting at a known probe radius estimates n there.
omega_prec = (1 - sqrt(1-n))*omega_0 (smooth weak-focusing model, n the local field index, omega_0 the orbital frequency)Source quote & editorial note
The frequency of the minor pulses in each beam pulse agrees quite well with the calculated frequency of precession of the center of rotation of the ions about the magnetic center of the system
Editorial note, tabletop extrapolation: Transfers with caveats: on a CW fixed-frequency machine you need a pulsed source or fast probe electronics to see the structure, but a pulsed-arc run makes precession directly visible on a scope - treat the inverted n as an approximate effective-tune diagnostic, cross-checked against the field map.
Cited in: Beam Dynamics: An Interactive Laboratory
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Working small classical cyclotrons in the 1958 census ran center fields of 12.5-19 kG (ISSP 16-in: 14-19; BNL 18-in: 13.1; Stanford 27-in: 12.5; ANU 31-in: 12.6; Purdue 37-in: 16.2; Copenhagen 90-cm: 17.5) - none below ~12 kG in the tabulated set; iron near saturation was the cheapest energy.
K_p[MeV] ~ 48.2*(B[T]*r[m])^2; K_d ~ 24.1*(B*r)^2Source quote & editorial note
Mag. field, k-gauss 14 - 19
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Editorial note, tabletop extrapolation: The reference machine's 0.59 T is a factor 2-3 below this tabulated population; pushing a next machine toward 1.2-1.5 T multiplies energy 4-6x at fixed pole radius - the route every tabulated machine took.
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Dee-to-dee voltage in the census tracks energy loosely: ISSP's 16-inch ran 10-18 kV and still held 100 uA internal beam; larger 1-4 MeV machines ran to ~30 kV (Stanford 20, Tokyo 27), and 7-11 MeV machines 40-90 kV.
Source quote & editorial note
Dee-to-dee, kv 10 - 18 ... Internal Beam, Stable, ua 100
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Editorial note, tabletop extrapolation: Proof that low dee voltage works at small radius: ISSP is the existence proof for a sub-MeV goal on a ~10 kV-class dee. Dee voltage buys turn count, phase budget and survival - the energy ceiling stays with B*r (dg-026) - and the field profile must keep the extra turns focused.
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Oscillator budgets for the census's 16-31 inch machines ran 10-50 kW, dominated by self-excited single-tube circuits (ISSP: one 8T11R, 10 kW in / 6 kW out; Stanford: one RCA 899A, 12 kW; BNL: one 5771, 35 kW in / 20 kW out; ANU: 50 kW out).
Source quote & editorial note
Oscillator type self-ex. Oscillator tube 5771 ... Osc. input, max 35 kw. Osc. output, max 20 kw.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 106
Editorial note, tabletop extrapolation: Those kilowatts bought tens-of-kV dees at high Q, not beam power. A few-kV tabletop dee's budget comes from the resonator formula instead (dg-313: tens of watts dissipated, so a 100 W-1 kW amplifier class with margin) - and the census's plain self-excited oscillators show that sophisticated drive chains are not a prerequisite for running a cyclotron.
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Magnet iron grows steeply with pole diameter across the census: 16-in -> 6 tons Fe, 18-in -> 6, 27-in -> 10, 28-in -> 17, 31-in -> 31, Copenhagen 90-cm -> 35, Washington 54-in-core -> 70; copper or aluminum windings add 1-12 tons.
census tonnage vs pole diameter: growth is steep but not a clean power law - gap, yoke geometry and field vary across the setSource quote & editorial note
Weight, Fe 6 ; Cu 4 tons. Winding 3/4 in x 1/16 in strip.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 106
Editorial note, tabletop extrapolation: Extrapolating down the census, an 8-in-pole machine sits in the fraction-of-a-ton class - hobby-crane scale, and the reference machine's 757 lb H-frame agrees - while every inch of added pole diameter on a next machine is bought with steeply growing steel.
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Census geometry ratios - the quoted 31-inch row computes to: pole gap 17.7% of pole diameter, dee aperture 59% of the gap, dee diameter 93.5% of pole diameter, maximum beam radius 81% of pole radius; the census's smaller machines bracket similar ratios (full tabulation: scan re-read queued).
Source quote & editorial note
Pole tip dia. 31 in. Beam radius, max 12.6 in. Field gap, center 5.5 in. ... Dee dia. 29 in. Dee aperture 3 1/4 in.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 26
Editorial note, tabletop extrapolation: Sanity template for a next machine on 8-inch poles: ratios of this class suggest a 1-1.4 in gap, a 0.5-0.8 in dee aperture, and energy planned at a 3.2-3.6 in beam radius rather than the pole edge - starting proportions to check against the machine's own field map and stability analysis, not expected dimensions.
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Shim for a 2-4% total field drop-off from center to maximum beam radius - the census machines cluster tightly there as tabulated (Copenhagen 1.75%, ANU 2%, ISSP 2.5%, BNL 3%, Tokyo 25-in 3%, and the quoted Rochester row's 3-4%).
total dB/B (center to r_max) ~ 0.02-0.04Source quote & editorial note
Field drop-off 3-4 %
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 164
Editorial note, tabletop extrapolation: Directly transferable as a SHAPE target for the reference machine's field: the fixed-frequency population converged on a smooth, monotonic few-percent total drop. The total constrains the average only - the stability check remains the local n(r) map (n > 0 throughout, staying clear of 0.2; dg-003, dg-138), which the same total drop can satisfy or violate depending on where the fall concentrates.
Cited in: Beam Dynamics: An Interactive Laboratory
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Internal beams of 100-3000 uA were routine on the census's small machines (ISSP 16-in: 100 uA deuterons; BNL 18-in: 1-2 mA protons; ANU: 3 mA); external beams ran far lower on most (Copenhagen 2%, ANU 8% of internal), with BNL's tabulated pairing - 800 uA external against 1000-2000 uA internal, nominally 40-80% - the outlier, and the table's values not necessarily simultaneous.
Source quote & editorial note
Internal Beam, Stable, ua 1000-2000 ... External Beam, Stable, 800 ua; 100 ua focused on target 15 ft from machine
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 107
Editorial note, tabletop extrapolation: If the reference machine sees nA, the gap to the historical uA-mA norm lives in source output and center-region transmission, not physics limits - and extraction cost most census machines most of their beam, so budget a next machine's external current pessimistically.
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Hooded low-voltage arc sources with hot filaments dominated the census's small machines as tabulated: ANU hooded arc with tungsten filament, BNL hot cathode in a copper arc house, Stanford hooded arc, ISSP hooded low-voltage.
Source quote & editorial note
Ion source, type hooded arc, tungsten filament
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 26
Editorial note, tabletop extrapolation: Population-level evidence that the hooded filament arc is the proven route to 100 uA-class internal beams at this scale - evidence of practice, not proof a cold-cathode PIG cannot compete (PIGs run cyclotrons too, dg-383): the choice trades filament fragility against arc-supply simplicity and delivered current.
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Center the beam with slits on the first revolutions: ANU used beam-defining slits on turns 1, 2 and 3 (third-turn slit 0.5 mm) and reached 100% extraction efficiency at low current - but only with dee voltage stabilized better than 0.5%.
Source quote & editorial note
Beam defining slits used on 1, 2, and 3rd revolutions to define center of beam rotation; 3rd turn slit is 1/2 mm wide. 100% extraction efficiency with low beams, requires better than 1/2 % stabilization of dee volts.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 27
Editorial note, tabletop extrapolation: A historically successful, mechanically simple extraction aid: slits in the center region plus tight dee-amplitude regulation. Evaluate it for a next machine by comparing its interception losses and centering benefit against the calculated turn separation and deflector tolerances - slits select phase space by throwing beam away, so they complement, not replace, deflector design.
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Vertical focusing on the first few turns can be electrostatic: ANU ran carbon grids across the dee apertures and reported electric focusing successful on the first four revolutions, bridging the region where the magnetic-gradient focusing is still negligible.
Source quote & editorial note
Electric focusing with carbon grids on the dees successful on first four revolutions
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 27
Editorial note, tabletop extrapolation: First-turn loss at low dee voltage is a classic tabletop failure mode, and the ANU carbon-grid result makes grid focusing worth testing - model the electric fields first, note a slit plate is not the same as a transparent grid, and check interception, RF loading, heating and outgassing at low current before adopting it.
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A variable-energy small cyclotron can hold its field profile over a range: ISSP varied 14 to 18 kG by coil current alone, keeping 1-2.5% drop-off at the 16-cm exit radius, with a variable-frequency self-excited oscillator following.
Source quote & editorial note
Magnetic field variable, by only changing the coil current, from 14 to 18 kg with 1 to 2.5% field drop-off at the exit (r = 16 cm).
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Editorial note, tabletop extrapolation: The builder can trim B to match a fixed RF (or vice versa) and expect the shim profile to survive over a modest range - PROVIDED the iron is not driven into locally different saturation, which reshapes the profile. Measure n(r) at both ends of the intended current range before trusting it.
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Air-cooled magnet windings sufficed on documented small machines: the survey lists Stanford's 27-in (12.5 kG, 10 t Fe) and Howard's 16-in (15-16 kG) with air-cooled coils.
Source quote & editorial note
Air-cooled coils. Iron ore blocks for shielding
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 127
Editorial note, tabletop extrapolation: Precedent that air cooling can work at this scale - two real machines did - not proof that a given coil can: adequacy is set by I^2R dissipation, winding geometry, insulation rating, duty cycle and airflow. Do the dissipation arithmetic (magnet-power calculator) and monitor winding temperature (dg-220) instead of citing precedent.
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Whole working cyclotrons were built for $5k-$110k and about two years, per the census: Stanford 27-in cost $5000 plus $5000 in improvements (1940 to first beam July 1941); ISSP 16-in $40k with first beam 26 months after start; BNL 18-in $110k.
Source quote & editorial note
Construction started 1940. Completion date July 1941 ... Total cost $5000 initial, $5000 improvements.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 166
Editorial note, tabletop extrapolation: Scope calibration: small teams on small budgets built working 2-4 MeV, 16-27 inch machines in this era. A next machine at the few-hundred-keV scale on 8-in-class iron - dg-697's K ~ 48*(B*r)^2 gives about 0.35 MeV at 1 T on an 8-in pole's usable radius - is historically a modest, well-precedented project.
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Make PA protection automatic and operator-proof, as the source did with tubes: a linear 'or' gate where the dee-voltage error and per-tube cathode-current limiters compete and the highest signal takes control, so mistuning cannot damage the power tubes.
control = max(dee-voltage error, PA cathode-current limit, driver cathode-current limit)Source quote & editorial note
As a result of these circuits improper tuning cannot damage the power tubes.
Editorial note, tabletop extrapolation: For the LDMOS upgrade, take the architecture (limiters that seize the control loop) but not the sufficiency claim: LDMOS dies fail on single-cycle peak Vds, mismatch load-line excursions and oscillation faster than an averaged ALC responds - so add device-specific SOA protection, fast reflected-power shutdown, thermal sensing and a stability check, with polarities and response times defined and fault-tested.
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Let the current-limit reference track the RF plate (output) voltage so that plate dissipation, not plate current, is what is held constant: the amplifier is then protected when the dee circuit is tuned off resonance, while full power remains available when properly tuned. [Corrected 2026-08-23: the earlier formula implied I_limit proportional to V_rf is itself the protection; it is one input to a dissipation estimate, and the note below says what else an LDMOS stage needs.]
Limit on estimated device dissipation, e.g. P_dc_in - P_rf_out, or Vds*Id averaged over the RF cycle - not a fixed current clamp, and not simply I_limit ~ V_rfSource quote & editorial note
to let the reference voltage vary with the rf plate voltage so that plate dissipation would be limited to a constant value
Editorial note, tabletop extrapolation: The LDMOS analogue (editorial transfer, informed by modern device practice rather than this source): foldback on a calibrated dissipation estimate - DC input minus delivered RF between defined measurement planes (which lumps matching-network loss into the estimate), or cycle-averaged <vds(t)*id(t)> - tightened under mistuning. Dissipation limiting is one protection layer, not sufficient: add drain-voltage clamping, a reflected-power/VSWR trip, device-temperature sensing and fast fault shutdown, since LDMOS also dies of RF-cycle overvoltage, mismatch and fast thermal transients.
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Modulate the machine electronically through the dee-voltage control loop rather than mechanically: a small current injected at the modulation-amplifier input depressed dee voltage about 1% per 10 uA, with recovery time set only by the control-loop bandwidth.
~1% dee-voltage depression per 10 uA injected at the "or"-gate inputSource quote & editorial note
The dee voltage is depressed about 1% for each 10 uA of injected current, and because a balance is maintained at the input of the amplifier, the recovery time is limited only by the bandwidth
Editorial note, tabletop extrapolation: A tabletop ALC loop gets dee-voltage modulation for free by injecting an offset into the amplitude setpoint - but that is voltage modulation, not proven beam gating: measure the transfer to extracted current, energy and extinction ratio (and where the un-extracted beam goes) before using it for activation or timing work; true beam-off needs a validated source-side chopper. The 1%/10 uA constant is their circuit's, not a scaling law.
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Interlock an automatic dee-tuning servo against low amplitude: the cited flip-flop phase detector stuck in one state below 15 kV of dee voltage, where the servo would run in the proper direction only by luck of which side of resonance the circuit sat on.
servo enable at V_dee >= 20 kV on an 80 kV system (i.e. ~25% of full amplitude)Source quote & editorial note
below a dee voltage of 15 kV, the flip-flop will remain in one state and only if the dee circuit happens to be tuned to the low frequency side of resonance will the servo run in the proper direction
Editorial note, tabletop extrapolation: Any auto-tune loop (phase comparison of PA drive vs dee pickup) needs a validity gate: characterize the detector's own signal-threshold, enable the servo only above it, bound the tuner's travel and rate so a confused loop cannot run away, and provide a manual jog mode to walk into range - the low-signal failure mode recurs across detector technologies even though its details differ.
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Set PA neutralization by a beam-independent RF cross-check: adjust the neutralizing capacitor until maximum dee voltage and minimum plate current coincide as the dee is tuned through resonance. [Corrected 2026-08-23: earlier text added a 'first-cut' procedure - full drive with plate and screen supplies off, null RF on the plate - that is not in the source and can exceed grid or screen ratings; removed.]
Source quote & editorial note
adjusting Cn for coincidence of maximum dee voltage and minimum plate current as the dee was tuned through resonance
Editorial note, tabletop extrapolation: Neutralization is a triode/tetrode matter, and the coincidence test belongs to a neutralized tuned-plate PA: on that class of amplifier the dee-voltage peak and plate-current dip should line up through resonance, and a skew flags feedback. On a solid-state or matched-line chain there need be no input-current dip at resonance at all - verify resonance and match there with dee voltage, reflected power and the device's rated currents instead. [Note revised 2026-08-23: the earlier note generalised the test to 'any amplifier-dee chain' and changed the observable to PA input current.]
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Keep DC supply voltage off RF conductors that run through the magnetic field in vacuum: a DC-biased line in the field can sustain a Phillips-ion-gauge-type discharge - the quote's warning; the discharge-to-window damage sequence is the report's incident account (scan re-read queued).
Source quote & editorial note
a Phillips-Ion-Gauge-type discharge can start in the magnetic field inside the vacuum tank near the positive transmission line
Editorial note, tabletop extrapolation: Very relevant at higher dee voltage on the reference machine or a next machine: crossed E and B in vacuum is exactly a PIG geometry - it is how the gauge and the source work - so route DC-carrying feedlines, bias leads and probe wires out of the field region or shield them. This failure mode is designed out at layout time.
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For sliding RF contacts, the cited design used heavy fingers - Eimac grid collet at 0.020 inch, twice their standard finger stock - clamped by water-cooled copper blocks against a silver-plated, water-cooled stem: nearly three years of flawless service with routine operation to 110 A/in and no sign of contact heating.
demonstrated point: 110 A/in routine (that geometry, cooled both sides); 0.020 in fingers vs 0.010 in standardSource quote & editorial note
It was decided to use Eimac grid collet (which is .020" thick in contrast to their regular line of finger stock which is .010" thick) mounted on water cooled copper blocks ... dee stem surface was silver-plated copper which was also water cooled. The shorting plane as originally installed has been in service for nearly three years and has performed flawlessly. There is no discoloration or other indication of heating of the contacts, despite routine operation to 110 A/in and occasional operation to higher current densities
Editorial note, tabletop extrapolation: The recipe transfers - thick fingers, positive clamping, plated surfaces, cooling on both sides of the joint - the number does not: calculate the proposed tuner's actual contact current, then verify temperature rise and contact resistance under representative duty; a demonstrated operating point in one cooled geometry is not a ceiling for another.
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Be wary of vacuum capacitors in the high-power PA plate circuit - in this system every vacuum-capacitor arrangement tried in the final plate circuit failed, and the design settled on fixed capacitive coupling plus a movable-short coaxial resonator.
Source quote & editorial note
vacuum capacitors have been used in various ways in its plate circuit. None has been found to stand up satisfactorily.
Editorial note, tabletop extrapolation: Dated in absolute terms - but 'modern vacuum caps are fine at kW-class' is a ratings question, not a vintage question: they are suitable where the manufacturer's peak-voltage, RF-current, frequency and thermal ratings are met with margin, and fault energy is considered. The placement lesson stands either way: put lumped variable capacitors where RF current is low and do coarse tuning with distributed elements.
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Squaring the dee waveform by adding a 1/3-amplitude third harmonic attacks what the source calls ordinarily a major beam-loss mechanism: it minimizes the axial electric defocusing force and even provides some focusing during the usually defocusing part of the phase excursion, where magnetic focusing is weakest.
V(t) ~ sin(wt) + (1/3)sin(3wt) (first two Fourier terms of a square wave)Source quote & editorial note
It minimizes electric defocusing, which is ordinarily a major cause of beam loss, and actually provides some focusing during the usually defocusing part of the phase excursion.
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 10-11
Editorial note, tabletop extrapolation: Electric defocusing on the first turns is a plausible and testable contributor to the reference machine's losses - not an established attribution; a flat-topped dee is likely too much RF plumbing for a next machine, but the mechanism explains why phase excursion and gap-crossing timing deserve modeling attention in any small machine.
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The source's analysis found the same central-region bunching occurs even with a third harmonic added to square the RF waveform - ions still group to cross the gap near the fundamental's peak - so flat-topping and automatic phase grouping coexisted in that analysis.
dominant term -w*t*sin(wt+theta) unchanged by third harmonic (Appendix I)Source quote & editorial note
the same bunching occurs even if a third harmonic is added to the r-f wave form to square the wave
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 10
Editorial note, tabletop extrapolation: Reassurance that waveform shaping and center-region bunching are separable problems in the source's treatment; any claimed voltage benefit depends on harmonic amplitude/phase and what is held fixed (peak voltage vs RF power), so quantify longitudinal acceptance by calculation before banking on it. The bunching mechanism itself (Cohen) is what sets which ions survive the center region. OCR note - theta prints as (c) in these appendix equations.
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The dee must be a high-Q energy-storage resonator, never a switched load: brute-force reversing a 100 pF dee-to-liner capacitance at 100 kV and 10 Mc/s would demand 20 MW, versus watts-to-kilowatts to sustain the same voltage in a resonant system.
P_switched ~ 2*C*V^2*f for hard +V/-V reversals - each reversal moves the stored charge through 2V, so the source's 20 MW = 2 x 1e-10 F x (1e5 V)^2 x 1e7 Hz checksSource quote & editorial note
If this is done at the rate of 10 megacycles per second, the power requirement would be 20 megawatts!
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 13
Editorial note, tabletop extrapolation: The cleanest back-of-envelope argument in this collection for why dee voltage is bought with Q, not amplifier watts - scale it to a next machine (7-9.5 kV on tens of pF at 6.78 MHz) to show why a few hundred LDMOS watts suffice only through a good resonator.
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To make one dee resonate simultaneously at the fundamental and third harmonic, terminate the dee capacitance in two shorted transmission-line stubs whose electrical lengths satisfy cot(a1 w) + b cot(a2 w) - ac w = 0 with w=1 and w=3 as roots; a coax bench model matched calculated lengths within about 2%.
cot(a1*w) + b*cot(a2*w) - ac*w = 0 with roots at w=1 and w=3; solving both conditions gives b13 = (cot(3*a1) - 3*cot(a1))/(3*cot(a2) - cot(3*a2)); a1 < pi/3 < a2Source quote & editorial note
The extra current element can, however, be a second transmission line
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 18
Editorial note, tabletop extrapolation: A lumped-plus-stub version is buildable at tabletop scale and the design tables (PDF 33-60) are precomputed; even unused, the method shows how to place a resonator's higher modes deliberately instead of discovering them by accident.
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Tune a dual-resonance system iteratively, one frequency at a time (the source's five-step procedure): null the input admittance at the fundamental with one line length; measure the admittance sign at the third harmonic; trade length between the two lines while keeping the fundamental nulled, using the sign and interpolated tables (its Appendix III) to know which way to tune; repeat until both frequencies null.
Source quote & editorial note
The following tuning procedure was found to be easy to follow: 1) Set the oscillator frequency at w0 and set the admittance meter to the correct reading for zero admittance at the junction to the system. 2) Tune the length of one of the lines for a null on the admittance meter. 3) Set the oscillator frequency to 3w and measure the admittance; note whether it is positive or negative. 4) Return to w0 and change a1, compensating with a change in a2 to keep the system tuned to w0. One can determine which way to tune by comparing the position of the resonances with numbers interpolated from Appendix III. 5) Remeasure admittance at 3w, and repeat the procedure until the admittance measures zero at 3w.
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 21
Editorial note, tabletop extrapolation: The written five-step procedure is a model for documenting any coupled-adjustment RF tune-up - a next machine's coupling loop and trimmer interact the same general way; precomputed knowing-which-way-to-tune tables are the transferable trick, though the dual-line tables themselves don't map onto a different topology.
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A single quarter-wave coupling line can feed both the fundamental and third harmonic to the resonator: an (ideally lossless, nondispersive TEM) line that is lambda/4 at the fundamental is 3*lambda/4 at the third harmonic and inverts impedances at both frequencies - if the resonator is tuned resistive at both, the driver sees resistive loads at both.
l = lambda1/4 = 3*lambda3/4; Z_in = Z0^2/Z_load at both frequenciesSource quote & editorial note
if the coupling line is one-quarter of the fundamental wave length it is three-quarters of the third harmonic wave length, and the impedances are simply inverted by the line at both frequencies
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 22
Editorial note, tabletop extrapolation: A handy odd-harmonic identity - and a warning that a quarter-wave feeder presents TRANSFORMED impedances to your amplifier's harmonics even in a plain sine-wave system: evaluate the actual harmonic load with Z0(f) and measured S-parameters (connectors and loading shift the third-harmonic electrical length) before assuming either benefit or instability.
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Multi-frequency drive pushed the source toward separate control: getting the third harmonic's phase and amplitude right was 'somewhat difficult' - and the report notes no serious self-excited driving system was attempted, so the comparison there is undeveloped, not decided.
Source quote & editorial note
It was somewhat difficult to get both the phase and the amplitude of the third harmonic adjusted correctly; however no serious attempt was made to develop a good self-excited driving system.
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 25
Editorial note, tabletop extrapolation: Mirrors the next machine's decision already leaning MOPA: independent control of each degree of freedom is the argument, and a DDS + LDMOS chain is the modern form - while the self-excited literature (dg-1367, dg-254) holds the other seat. This source records a difficulty, not a verdict.
Cited in: Driving the Dee: RF Coupling
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Monitor the dee waveform continuously and provide remote or servo tuning: tuning drifts are always experienced in cyclotron operation, and in a multi-resonance system drift changes the relative amplitude and phase of the harmonics, silently altering the waveform.
Source quote & editorial note
Tuning drifts are always experienced in cyclotron operation. Since a tuning drift would change the relative amplitudes and phases of the first and third harmonics, such a drift would alter the wave form. A visual means of monitoring the wave form and a remote tuning or an automatic servomechanism for tuning should be provided.
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 25
Editorial note, tabletop extrapolation: Even a plain sine system drifts (thermal detuning is logged on the reference machine); a calibrated capacitive pickup on a scope is the minimum instrument, and it is a prerequisite for any auto-tune servo on a next machine.
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Ion bunching by the RF displaces orbit centers by Delta-r = 2D sin(theta) with D = eV/(2*m*omega^2*d); in the ORNL Analogue I example this was equivalent to ~20 turns, ~2 kV, or ~1% energy spread at the exit radius.
Delta-r = 2*D*sin(theta), D = eV/(2*m*omega^2*d) characteristic bunching displacementSource quote & editorial note
the radial displacement amplitude is equivalent to about twenty turns, or to about two kilovolts, or about 1% spread in energy at the exit radius
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 12
Editorial note, tabletop extrapolation: Budget this effect for any future extraction work by evaluating D and Delta-r with the machine's own V, omega, gap and phase distribution and tracking the offsets to extraction - the ORNL equivalences are that machine's numbers, not a floor. Flat-topping reduces the phase-dependent part; neither AVF nor flat-topping removes the displacement wholesale.
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Size a dee tuning servo the source's way: loop gain such that one degree of phase error applies full power to the servo motor, and total trimmer range sufficient to shift the dee resonant frequency 2%.
full drive at 1 deg phase error; trimmer range 2% of f_res (both the source's criteria)Source quote & editorial note
The loop gain should be such that one degree of phase error will apply full power to the servo motor. ... the trimmer should have sufficient range to shift the resonant frequency 2%
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 7
Editorial note, tabletop extrapolation: Good starting criteria for a stepper-driven trimmer on a next machine's resonator - then derive the actual range and slew from measured cavity drift (thermal and mechanical) and actuator dynamics, and verify loop stability margins; the field tolerance and the tuning range are separate constraints.
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Build the tuning-loop phase detector to null exactly at the desired phase with high, KNOWN sensitivity: the cited detector produced 0.76 V per degree of phase error (its null-point phase and sign convention are the report's circuit details - re-read queued).
K_d = 0.76 V/deg at the nullSource quote & editorial note
The phase detector is quite sensitive and produces an output signal of 0.76 volt for a phase error of 1
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 13
Editorial note, tabletop extrapolation: Characterize K_d on the actual detector near the chosen null so loop gain is a number, not a knob - then size downstream amplification from the full loop model (actuator, mechanics, delays). Modern detector options span analog slopes to charge pumps to digital outputs; their gain is a datasheet-plus-measurement fact, not a folklore mV/deg figure.
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Make the control loop's gain independent of machine operating level: the source's heterodyne converter produced an IF whose amplitude equals the local-oscillator level - not the RF level - over its usable range, and an antinoise circuit extracted phase despite arc-source and dee-vibration noise.
Source quote & editorial note
the amplitude of the intermediate frequency is exactly equal to the magnitude of the local oscillator signal and entirely independent of the magnitude of the phase signals
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 12-13
Editorial note, tabletop extrapolation: The principle transfers: servo dynamics should not change with dee-voltage level over the operating range, and the ion arc is a noise source the phase detector must tolerate. Modern equivalents are limiting amplifiers or digital phase detection - but every implementation has a floor: specify and test input dynamic range, limiter behavior, phase noise and loss-of-signal handling, because no detector stays accurate as the signal approaches its noise floor.
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In the cited independently-tuned two-dee system, unneutralized dee-to-dee capacitance coupled the two tuning servos so strongly that stability was, in the source's words, insuperable - power flows dee-to-dee through the high-Q resonator, and shielding skirts and time-constant tweaks did not fix it; transmission-line neutralization between the stems did.
dee-dee neutralizing line load condition Vn = Va*w*CDD*Zo*sin(beta*l)Source quote & editorial note
The most serious objection to the dee-to-dee capacitance is the coupling between servo systems which it provides. The problem of servo stability becomes insuperable.
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 15
Editorial note, tabletop extrapolation: A single-dee next machine dodges the coupled-servo problem entirely - the design lesson. Any two-dee or dee-plus-tuned-dummy variant with separate tuners should measure the coupling matrix and analyze loop stability first: neutralizing lines are one narrowband remedy, and common tuning, coordinated (MIMO) control or reduced bandwidth are others.
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Verify neutralization by exciting one dee stem at a time and measuring the voltage induced on the others; the 20-inch achieved coupling coefficients below 3%. The adjustment was done with the machine vented to air, because at low pressure the low-level test drive multipactors.
N_ij = e_j/e_i; 20-inch achieved < 3% (their result, not a universal pass number)Source quote & editorial note
It was necessary to do this while the machine was down to air, in order to avoid multipactoring. ... The coefficients for the 20-inch cyclotron were below 3%. In order to adjust the coupling loops of the neutralizing lines the dee stems were excited one at a time
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 18
Editorial note, tabletop extrapolation: Two transferable habits: quantify RF isolation as a measured coefficient (set the pass number from your own loop-stability analysis), and remember low-level RF in vacuum can sit in a multipactor window - the reference machine has seen multipactor-like loading. Venting for the test sidesteps multipactor but is not blanket safety: corona, heating and hazardous RF voltage remain, so keep monitoring and interlocks in place.
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A 45-degree (lambda/8) transmission line makes a constant-amplitude phase shifter: for an ideal lossless line with resistive termination, |Z_in| = Z0 independent of the load resistance, so driving from a constant-current source and servo-varying a load pot (250-ohm, ~7 ft of RG-58 at 11.2 Mc in the cited system) shifts phase without changing amplitude.
45-deg (lambda/8) line; |Z_in| = Z0 independent of R_L; phase of V_in depends on R_LSource quote & editorial note
if the line is excited from a constant current source the magnitude of the voltage appearing across the input of the line is constant but the phase of the voltage depends upon the load resistance
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 11
Editorial note, tabletop extrapolation: A DDS sets phase digitally today, but the lambda/8 trick remains a zero-active-parts phase adjuster and a nice classroom transmission-line demonstration - measure the residual amplitude variation of the real cable, pot parasitics and finite source impedance before using it where amplitude flatness matters.
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Reduce cross-coupling before closing control loops: once the three dees were isolated electrically by adjusting the neutralizing loops, the machine behaved like three separate single-phase systems, each controllable with its own small amplifier and servo.
Source quote & editorial note
Once the three dees are isolated electrically by adjusting the neutralizing loops the machine behaves like three separate single-phase systems.
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 18
Editorial note, tabletop extrapolation: The architectural moral - decouple where practical, then control each loop as SISO - applies to a next machine's interacting adjustments (tuner vs coupling vs amplitude); measure the residual interaction after decoupling, and where it stays significant use coordinated control rather than fighting coupled loops one at a time. The programme burned months servoing the coupled system first (ucrl-3187 p.5-6, 11).
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Moving the source off-center and injecting azimuthally into a dee transformed the 20-inch: a central open arc giving 3.2 mA with severe dee-tip heating was replaced by a hooded-arc source at ~1.75-in radius with a 1/8 x 3/4-in exit slot, roughly doubling the beam to 6-7 mA and eliminating the dee-tip heating - though source type and position changed together.
source radius ~1.75 in on a 20-in machine (~0.2 of pole radius); slot 1/8 x 3/4 inSource quote & editorial note
A major improvement was effected when an off-center source was installed which injected azimuthally into one of the dees.
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 12
Editorial note, tabletop extrapolation: For the reference machine's filament source, radial position and slot azimuth are cheap, high-leverage experiment variables (directly relevant to the planned source-species test) - scan them, normalized to the first-orbit geometry. Expect improvement mechanisms to be entangled as they were historically; measure, don't assume a factor of two.
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Cross-check internal-beam probe readings calorimetrically and expect method-dependent discrepancies that grow with current: calorimetry gave 90% of the probe reading at 1-2 mA but only 75% at 6-8 mA; the probe was judged the more reliable.
calorimetric/probe ratio 0.90 at 1-2 mA, 0.75 at 6-8 mASource quote & editorial note
the calorimetric method gave 90% of the probe method, while in the 6- to 8-ma range this ratio dropped to 75%. The probe method was believed to be the more reliable.
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 14
Editorial note, tabletop extrapolation: At the reference machine's nA scale the transferable doctrine is: never trust one beam-current method - independent checks can reveal method-dependent bias, as the mA-scale probe/calorimetry comparison did. Establish the actual uncertainty from calibrated measurements, blank runs and charge integration; the electrometer-background subtraction is a control within one method, not an independent second method. OCR note - the 75% figure was verified on the page image.
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Use a positive probe bias as one purity check on beam-current readings: on the 20-inch, +450 V left the full-radius reading unchanged (consistent with fast-ion current) while inside 6 inches the unshielded-probe current rose steeply and was reduced by bias - flagging low-energy and secondary contamination near the center.
necessary check, not sufficient: accept readings only where dI/dV_bias ~ 0 over a swept range AND source-off/RF-off controls are cleanSource quote & editorial note
at this radius was unaffected by 450-v positive bias on the probe. However, inside 6 inches the probe current rose steeply with decreasing radius and was decreased by positive bias voltage.
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 12
Editorial note, tabletop extrapolation: Directly usable on the reference machine's probe: sweep the bias until the reading plateaus, and back it with controls (RF on/no beam, source off) - bias-flatness alone can miss RF pickup, leakage and photon-induced currents. Set the bias magnitude from collector geometry and secondary-particle energies, not from the beam current.
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Beam loading is a free diagnostic at milliampere scale: turning the source on raised the 20-inch's final-amplifier plate currents two- to threefold over source-off - the beam absorbing real RF power.
I_beam approximately linear in V_dee; plate current 2-3x source-off under full beam loadSource quote & editorial note
The beam load would cause a two- to threefold increase in the amplifier plate currents compared to the source-off condition.
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 14
Editorial note, tabletop extrapolation: The 2-3x signature does NOT transfer to nA beams (P_beam = I*E/q puts a nA beam far below amplifier-meter resolution - compute it for your parameters); what does transfer is the habit of plotting beam current against dee voltage empirically as a run-log staple, WITHOUT imposing linearity - capture and transmission bend that curve, and V_dee itself goes as sqrt(P) at fixed impedance.
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Protect the RF finals in layers - the quoted list: interlocked air cooling, spark gaps at both ends of the transmission lines to the dee stems, and an rf-dc fault circuit; the comparison logic (remove excitation when DC is present but RF fails to build) is the site's reading of that circuit's function, to be verified against the report (scan re-read queued).
fault = (V_dc present) AND (V_rf below threshold) -> remove excitationSource quote & editorial note
protected by an interlocked air-cooling system, spark gaps at both ends of the half-wave transmission lines leading to the dee stems, and by an rf-dc fault circuit
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 11
Editorial note, tabletop extrapolation: The rf-dc comparison is the tube-era ancestor of modern output-detect foldback and ports to the LDMOS upgrade: DC applied but no RF developing means something is wrong - an arc, a detune, or a failed stage - so kill drive and investigate. Spark gaps at the feedthroughs remain cheap insurance.
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When automatic fault recovery (a spark recycler with operator-adjustable delay) is added, also freeze the tuning servos during recovery - during repeated recycling the servos received spurious signals and crept away from tune, turning one fault into a detuned machine.
Source quote & editorial note
during this time the servos received spurious signals and tended to creep away
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 12
Editorial note, tabletop extrapolation: A control-system rule that transfers verbatim to any next machine's auto-tune or ALC firmware - hold integrators and actuator positions during spark recovery/restart, and make both the recycle delay and the servo-hold adjustable; same lesson as coo-535-543's amplitude gate, learned independently.
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Expect thermal detuning plus ion lock after shutting down from high-power running: this machine would not re-excite, and had to be retuned by exciting each dee-stem tank with a grid dip oscillator and adjusting the tuning capacitances for resonance.
Source quote & editorial note
thermal effects detuned the machine sufficiently so that ion lock prevented the rf from being restored ... It was then necessary to retune the machine by exciting each of the dee-stem tanks with a grid dip oscillator and adjusting the tuning capacitances for resonance.
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 12
Editorial note, tabletop extrapolation: The transferable practice is a permanent low-level resonance-check capability - a VNA or dip meter on a pickup loop, with RF-rated isolation or interlocking so it can never see drive power - so resonance can be found cold, plus logging tune position vs temperature. The reference machine already shows warm-up drift.
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Do not use amplifier efficiency as a proxy for electrode phase: on this machine, peak final-amplifier efficiency did not correspond to the required 120-degree dee phase difference, so phase was measured and servoed from dee pickup signals directly, with separate efficiency servos trimming the amplifiers (five loops total in their implementation).
Source quote & editorial note
peak efficiency did not correspond to 120 phase difference between the dees
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 11
Editorial note, tabletop extrapolation: Measure the quantity you care about at the electrode (same moral in ucrl-3153 p.7): derive a next machine's tuning/phase feedback from the dee pickup, and before trusting LDMOS drain current or forward power as a tuning indicator, verify at the electrode that its optimum coincides with the dee-voltage optimum - the historical machine's did not.
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Size deflector gaps by the VE relationship: for equal sparking probability with given materials, gap voltage times cathode gradient is constant - the quoted relation (the experimentally tested gap range is the report's: scan re-read queued).
V(kV) * E(kV/cm) = const; equivalently V ~ K*d^0.5Source quote & editorial note
for equal probability of sparking with given materials, the product of gap voltage and cathode gradient is a constant.
Editorial note, tabletop extrapolation: For a next machine's deflector the trade falls out of a chosen VE number: a 3-mm gap at VE = 1.5e4 (kV)^2/cm predicts ~67 kV at ~220 kV/cm - far beyond tabletop needs (dg-590's few kV), which is the real point: tabletop deflectors sit deep inside the bulk-breakdown envelope, and surface/edge engineering rules instead (dg-591).
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Derate the deflector to VE = 1.5e4 (kV)^2/cm for day-to-day operation even though 2.25e4 was held in tests: a one-third margin below best-demonstrated holding.
VE_design = 1.5e4 (kV)^2/cm vs 2.25e4 achieved (Fig. 10 design chart)Source quote & editorial note
In order to provide an adequate margin for day-to-day operation, a design value of 1.5 X 10^4 should be used.
Editorial note, tabletop extrapolation: The most quotable deflector design number in the collection: design to VE = 1.5e4 (kV)^2/cm and treat the tested 2.25e4 as commissioning margin - as the source machine practiced. Transfer it as a starting point under the usual conditions (electrode material, finish, conditioning - dg-353, dg-295), and verify on the actual electrodes.
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Electrode material ranking by measured spark damage in a magnetic field: stainless steel (316 was the tested grade), inconel, molybdenum, K-monel, titanium, and nickel comparable and best; copper, tantalum, aluminum intermediate; silver worst. Carbon resists damage but loses its bake-in within minutes of removing voltage. K-monel and nickel spark dust is magnetic; stainless and the others' is not.
best: 316SS/inconel/Mo/K-monel/Ti/Ni > Cu/Ta/Al > Ag; carbon anomalousSource quote & editorial note
stainless steel, inconel, molybdenum, K-monel, titanium, and nickel seem to be comparable and were the best materials. Copper, tantalum, and aluminum were intermediate. Silver showed the most severe spark damage. Carbon appeared to resist spark damage well, but would not remain baked out. Heard and Chupp claim that after baking out carbon electrodes and turning the voltage off for even a few minutes, the whole bake-in process had to start over again. The spark dust of K-monel and nickel was found to be magnetic. That from stainless steel and the other materials tested was not.
Editorial note, tabletop extrapolation: 316 stainless is the economical best-tier candidate for the next machine's deflector electrode (cheap, machinable, tested) - validate under the intended field, finish, gap and stored energy; copper and aluminum ranked intermediate in this test, which argues against them for HV surfaces where a best-tier metal is just as easy to use.
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Each electrode material tested showed an apparent critical magnetic field - ranging 4 to 15 kG across materials - above which spark damage was severe and below which negligible; the field did not lower first-spark voltage, but crater damage accumulated in-field lowers holding voltage.
apparent B_critical: 4-15 kG, material-specific - the threshold for YOUR material decides, not the range's edgesSource quote & editorial note
There seemed to be a critical magnetic field for each material beyond which the spark damage was severe and below which the spark damage was negligible. The critical fields ranged from 4 to 15 kG.
Editorial note, tabletop extrapolation: The reference machine's ~6 kG is above the 4 kG end of the tested range, so no advantage can be assumed without knowing the chosen electrode material's own threshold. Conditioning at reduced magnet current is a hypothesis worth testing - it cannot prevent severe damage from later sparks at full field if the material's threshold sits below the operating point, so validate at full field before trusting it.
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Added gap capacitance had a strong, nonmonotonic effect on bake-in: a 24-pF gap baked in to only 10 kV, adding 0.0125 uF raised the held voltage six-fold to 60 kV, and 0.5 uF cut it to 5 kV with severe craters (dc tests, no magnetic field).
dc, no B: 10 kV @ 24 pF -> 60 kV @ 0.0125 uF -> 5 kV @ 0.5 uF; note 0.5*C*V^2 at these points is ~1.2 mJ / 22.5 J / 6.3 J - capacitance, not a single spark-energy scalar, was the tested variableSource quote & editorial note
when a 0.0125-uF capacitor was added across the gap, the electrodes baked-in to 60 kV, a six-fold increase. Adding a 0.5-uF capacitor across the gap reduced the breakdown voltage to 5 kV.
Editorial note, tabletop extrapolation: For the deflector supply, the transferable idea is that conditioning behavior depends on the discharge circuit, not just the gap: compute the total fault energy (all capacitance plus supply feed-through), current-limit and interrupt faults quickly, and establish any deliberate conditioning-energy setting by controlled test - not by defeating arc extinction.
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Budget conditioning time at roughly 30 sparks per cm^2 of high-voltage surface, with ~1 s of vacuum recovery per spark, i.e. ~30 s/cm^2 of bake-in; all tested materials baked in similarly except 316 stainless, which required about ten times as many sparks to reach ultimate voltage.
~30 sparks/cm2; ~30 s/cm2 bake-in time; x10 for 316SSSource quote & editorial note
all of them baked in in a similar fashion except 316 stainless steel, which required about ten times as many sparks to reach the ultimate breakdown voltage. It takes about 30 sparks per cm2 to bake in high-voltage-electrode surfaces. Since it takes about a second for the vacuum to recover following a spark, the bake-in time of an electrode is about 30 sec/cm2.
Editorial note, tabletop extrapolation: Applying the source's scaling to a palm-sized ~100 cm^2 electrode gives about 50 minutes of spark time - or roughly 8.3 hours for 316 stainless - excluding setup, failed ramps and downtime. Write conditioning into the next machine's ops checklist as a scheduled activity, not a nuisance.
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Minimize high-voltage electrode surface area: less area means less bake-in sparking to clean up cathode spots and less contamination collection; the 88-inch tailored its field window to the beam - 0.5 in of field height for a 0.25-in beam.
field height ~ 2x beam height; radial field extent from incoherent oscillations (0.1-0.4 in at the 88-Inch)Source quote & editorial note
the high-voltage electrode should have the minimum possible surface area. This minimizes the amount of sparking required to bake out the cathode spots and reduces the amount of electrode contamination.
Editorial note, tabletop extrapolation: Measure or track the next machine's actual beam envelope at extraction radius - vertical oscillations, alignment and median-plane shift included - set the field window from that worst case plus explicit margin, and keep the HV bar as small and short as the trajectory allows; the 88-inch's 2x is their outcome, not a sizing law.
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Keep the minimum radius of curvature of the high-voltage electrode no less than about half the gap, to prevent appreciable field-gradient magnification at edges.
r_min >= gap/2 on all HV electrode edgesSource quote & editorial note
The minimum radius of curvature of the high-voltage electrode should be large enough to prevent appreciable field-gradient magnification. In practice, the minimum radius should be no less than about half a gap.
Editorial note, tabletop extrapolation: Direct machining rule - for a next machine's 3-mm deflector gap, radius every HV edge to at least 1.5 mm and polish.
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Rigidly support the high-voltage electrode at both ends: a cantilevered deflector bar self-oscillates like a tuning fork (dark-current force modulation closes an electromechanical Colpitts loop, observed at 20 cps) and sparks at reduced voltage. Insulator supports raised VE from 1.23e4 to 1.47e4 immediately.
VE 1.23e4 (cantilevered, oscillating) -> 1.47e4 (insulator-supported), same crowbar settingSource quote & editorial note
At the smaller gaps the electrode vibrated like a tuning fork in a tuning-fork oscillator. ... The forces driving the electrode were electrostatic; the device that provided the pulsating force was the dark current. ... Simplifying this circuit by the techniques of network analysis the system reduces to that of a Colpitts oscillator. ... The period is 50 msec corresponding to a vibrational frequency of 20 cps. ... Curve 1 was taken before insulators were installed and electromechanical oscillation occurred, resulting in VE = 1.23 x 10^4 (kV)^2/cm; curve 2 was obtained with insulator supports which prevented electromechanical oscillation, crowbar was set at 0.4 A, resulting in VE = 1.47 x 10^4 (kV)^2/cm
Editorial note, tabletop extrapolation: Very much in reach of amateur trouble - a small cantilevered electrode has low mass and compliance. Support a next machine's deflector bar on insulators at both ends and check the deflector voltage on a scope for slow oscillation buildup.
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Face the surfaces sparks land on (the spark "anodes") with tungsten sheet: 15-mil tungsten overlapped so only tungsten is exposed raised the held VE from 1.93e4 to 2.25e4 (+17%), because sparking occurs when electron power density vaporizes the anode, and tungsten vaporizes at the highest power density. Tungsten also resisted spark damage best.
VE 1.93e4 -> 2.25e4 (kV)^2/cm with W anodes (+17%); Table I Rms VE 1.57e4 (mixed metals) vs 1.9e4 (W)Source quote & editorial note
With the tungsten anodes, the VE number increased to 2.25 X 10^4 (kV)^2/cm, an increase of 17% in VE number. In addition, we found that the tungsten anodes resisted spark damage better.
Editorial note, tabletop extrapolation: A cheap, historically demonstrated upgrade candidate: line the grounded surfaces opposite the next machine's HV bar with thin tungsten sheet, edges overlapped so only tungsten is exposed - then verify in the actual geometry, since breakdown gains depend on geometry, finish, stored energy and conditioning; molybdenum is a plausible substitute only on its best-tier spark-damage ranking (dg-744), not on this VE test.
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With spark-current control at the supply and tungsten anodes, the report could compensate for deflector capacitance: at lower capacitance they could crowbar at higher spark currents, and vice versa (their tests spanned tens to hundreds of pF - figures queued for scan re-read).
compensation relationship: lower C_deflector <-> higher tolerable crowbar current; re-optimize the crowbar per configurationSource quote & editorial note
we could compensate for deflector capacitance; at lower capacitance we could crowbar at higher spark currents, and vice versa.
Editorial note, tabletop extrapolation: Cable and feedthrough capacitance in a tabletop deflector still stores 0.5*C*V^2 right at the gap, where a supply-side crowbar cannot intercept it - so it is a design input, not a non-issue: compute the local stored energy at maximum voltage and add local series impedance or other discharge-energy limiting, then set the crowbar point for the configuration as the source did.
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Carbon septa held well without beam - a VE number of 1.7e4, about 75% of the metal-septum value - but beam heating evaporates carbon onto the HV electrode and collapses voltage-holding to as little as 25% of normal, recoverable only by venting and cleaning the deflector. Carbon's evaporation is itself thermal erosion: at power, the contamination and the survival question are the same physics.
carbon: VE 1.7e4 ~ 75% of metal (beam-off); beam-heated contamination can cut deflector VE to 25% of normalSource quote & editorial note
we could obtain a VE number of 1.7 x 10^4. This is about 75% ... When we increased the beam current, the carbon evaporated from the septum, contaminated the high-voltage electrode, and very little voltage could be held. ... one can easily evaporate enough carbon from the septum to reduce the deflector's VE number to 25% of its normal value. This requires letting the machine's vacuum down to air and cleaning the deflector
Editorial note, tabletop extrapolation: A next machine's beam power is watts, not kilowatts, so a carbon septum's activation advantage may yet win at sub-MeV - but the mechanism is temperature-driven and thin-foil hot spots concentrate it, so default to a tungsten or molybdenum septum and revisit carbon only with septum-temperature estimates in hand.
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Dark current transports anode material to the cathode (up to 1 copper atom per 2 electrons, by evaporation) even with zero sparks, so a dissimilar anode coats and degrades the cathode; and diffusion-pump oil vapor raises dark current three orders of magnitude by cracking carbon onto electrode surfaces. Hydrogen "ion scrubbing" (200-300 micron H2, ~100 mA glow discharge from a 480-V transformer for ~1 h) reduces deflector dark current about five-fold.
dark current x1000 with oil vapor vs Hg-pumped clean system; ion scrub = 200-300 u H2, ~100 mA, ~1 h -> dark current /5Source quote & editorial note
Hydrogen is let into the vacuum tank until the pressure becomes 200 to 300 u. ... A discharge current of about 100 mA is maintained for about an hour.
Editorial note, tabletop extrapolation: The reference machine and a next machine use oil diffusion pumping, so the dirty-system dark-current regime is the thing to MEASURE, not assume. The hydrogen ion-scrub is a historical conditioning procedure to adapt, not a weekend recipe: it needs an isolated, current-limited supply (a variac is not isolation and 480 V is lethal), controlled H2 admission with pressure regulation, a safe purge/exhaust path, and interlocks - reviewed against the actual apparatus before first use.
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Diagnose whether a deflector is sparking-limited by plotting voltage vs gap on log-log: if the points follow a VE line (V^2*d = const, log-log slope 1/2), sparking phenomena set the limit; departures flag something else at work - to be identified by investigation, not assumed.
log V vs log d following the VE-line slope (1/2 for V^2/d = const) => spark-limitedSource quote & editorial note
a deflector is limited by sparking phenomena and not from an extraneous cause can be tested simply by a log-log plot of the voltage versus gap to see that it follows a VE line.
Editorial note, tabletop extrapolation: Free instrumentation for a next machine: run the V(d) test during commissioning with several repeated gap settings (conditioning history scatters single points). The report's practice of insulating each ground electrode and metering intercepted current as an alignment monitor is worth copying too - reported practice, scan re-read queued for the exact passage.
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Design the deflector supply to limit the energy delivered per spark, not to prevent sparks: the 88-Inch supply stores only 2.5 J at 120 kV (distributed across 1200 diodes), sparked virtually every second for 24 h/day for many days without damage, and its spark will not puncture 5-mil aluminum foil.
E_stored = 2.5 J at 120 kV; survives ~1 spark/s continuousSource quote & editorial note
it stores only 2-1/2 joules and, at most, this is distributed among 1200 diodes. ... There is so little energy in a spark from this rectifier that it will not puncture even a piece of 5-mil aluminum foil.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 28
Editorial note, tabletop extrapolation: The governing philosophy for a next machine's deflector supply: limit the energy delivered per spark rather than trying to prevent sparks - low stored energy is an equipment-survival property, and a sub-joule store at 50-100 kV is achievable. It is not a personnel-safety property: such a supply remains dangerous to people, and in human contact the supply's follow-on current adds to the stored energy. Personnel protection stays with enclosure, interlocks, grounding and discharge practice (dg-522, dg-654).
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The 1963 solution for a deflector supply: a 100-kc six-stage Cockcroft-Walton from inexpensive parts - boards of 100 series silicon diodes (each graded by a 250 pF / 500 V ceramic), 900 pF 30-kV TV-type ceramics between decks - delivering 120 kV at 5 mA.
6-stage CW, 100 kc, 12.5 kV pk drive -> 120 kV / 5 mA; grading 250 pF per diode; deck caps 900 pF 30 kVSource quote & editorial note
Each circuit board consists of 100 Unitrode, Type UT71, silicon diodes connected in series. Each diode is shunted by a 250-pF, 500-V, ceramic capacitor to divide the inverse voltages equally.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 10
Editorial note, tabletop extrapolation: Today this is a standard multiplier stack; keep the two features that matter - per-diode grading capacitors (transient sharing; add static resistors or integrated HV rectifiers for dc sharing) and high drive frequency, which buys regulation into a varying load. What frequency does NOT buy is low stored energy: 0.5*C*V^2 is set by the capacitors, so compute the stack's accessible spark energy and add local limiting before pointing it at a sparking deflector.
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Crowbar the oscillator screen grid, not the HV: the report's 3D22 thyratron grounds the screen on spark detection - sensed through a 30-ohm ground-return shunt, capacitively coupled and RC-filtered against RF - cutting power to the deflector fast enough that at sensitive settings 'the power supply can be turned off before a spark becomes visible', with an automatic recycle.
crowbar senses I via 30-ohm return shunt; cutoff in a few us; recycle 1 s; spark duration = f(bias setting)Source quote & editorial note
at the more sensitive positions of the crowbar current setting, the power supply can be turned off before a spark becomes visible.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 28
Editorial note, tabletop extrapolation: The feature to replicate in a modern build: fast drive-kill on spark detection with an operator-adjustable threshold, used deliberately during bake-in (UCRL-10654's practice). A solid-state inverter's gate shutdown gives the fast drive-kill - but killing drive is not a crowbar: energy already stored in the output stack and cable still feeds the spark (dg-285), so pair gate-kill with a dump path or series resistance rated for that stored energy.
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The cited multiplier column spaced its boards ~2 in, for a nominal maximum design gradient of 10 kV per inch along the open-air column, with the diode pattern arranged to minimize board-level gradients where deck-to-deck potential appears.
cited apparatus: ~10 kV/in nominal maximum along its open-air column (12 boards, 8-in-OD lucite, 27 in tall) - a design point, not a universal air ruleSource quote & editorial note
The spacing between boards is about 2 in. and provides a nominal maximum design gradient of 10 kV per in.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 10
Editorial note, tabletop extrapolation: For an amateur HV column, run the real layout numbers: air clearance and surface creepage separately, field stress at conductor curvatures, contamination and altitude derating, and a controlled HV test - matching the historical 10 kV/in exactly (6 in at 60 kV) leaves zero headroom by construction.
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In the cited 100-kc stack, diode storage time did not spoil rectification into the capacitive load - the load still charged to peak. (The report also irradiated diodes to improve rectification above 100 kc; the direction and size of the back-resistance change need the scan re-read before quoting.)
cited circuit: ~2 us storage acceptable at 100 kc into a capacitive loadSource quote & editorial note
the diode charges a capacitive load to the peak value, and the stored charge does not subtract (appreciably, at any rate) from the output voltage.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 10
Editorial note, tabletop extrapolation: Historical for parts choice - modern fast-recovery diodes moot the issue - and do NOT generalize the tolerance: reverse-recovery charge at 100 kHz can mean reverse current, heating, and poor sharing in other topologies. Select diodes on reverse voltage, recovery charge, leakage and sharing arithmetic; spend the savings on voltage rating and grading.
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Regulation is limited by the precision divider: for 0.01% deflector-voltage stability the cited system's divider resistors had to track within about 3 C of each other (the carrier-frequency, loop-bandwidth and divider-construction details are the report's - re-read queued).
f_carrier 100 kc -> f_unity 2500 c/s; 0.01% regulation; divider spec 36 ppm/C, dT < 3 CSource quote & editorial note
for a stability of 0.01% the temperature difference between resistors must be within about 3 C.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 21
Editorial note, tabletop extrapolation: Deflector voltage stability maps directly (first-order) to extracted-beam steering stability, so buy or build the divider first - and set the actual tolerance from a beam-clearance budget at the septum (beam size, orbit spacing, drift) rather than assuming either 0.01% is needed or 1% is fine.
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Filter CW ripple using the deflector itself as the filter capacitor: a series resistor from the Cockcroft-Walton to the deflector forms a one-pole RC with the deflector capacitance (the report: 100 kOhm into ~250 pF, a 6.7-kc pole giving ~15x attenuation at 100 kc), and the same resistor limits what supply-side stored energy reaches a spark.
pole f = 1/(2*pi*R*C_defl); report's point: 100 kOhm, ~250 pF -> 6.7 kc, ~15x at 100 kc; steady drop = I_load*R; resistor must be rated for dc drop, pulse energy and full voltageSource quote & editorial note
We can attenuate this ripple by using an RC filter consisting of a series resistance connecting the Cockcroft-Walton to the deflector, and a capacitance which is the deflector capacitance.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 30
Editorial note, tabletop extrapolation: Pick R from the measured deflector capacitance, ripple frequency, allowable voltage drop and the discharge-energy model - and note what the resistor cannot do: the 0.5*C*V^2 already ON the deflector side discharges into the arc regardless. Size the part honestly (dc dissipation I^2*R, pulse rating, voltage grading) - at the report's own 5 mA, 100 kOhm burns 2.5 kW only if run continuously at that current, so check the real duty before calling any resistor cheap.
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Magnetic shielding of glass tubes near the cyclotron is mundane but mandatory: the deflector oscillator and crowbar tubes sitting in the ~150 G stray field at the magnet yoke worked under tight-fitting 1/8-in mild-steel cylindrical caps.
~150 G stray field -> 1/8-in mild steel caps sufficedSource quote & editorial note
the deflector oscillators are located close to the magnet yoke of the cyclotron in a field of about 150 G, magnetic shields had to be put over the 4CW2000 oscillator tube and the 3D22.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 19
Editorial note, tabletop extrapolation: Map the field where equipment will sit and shield or relocate per COMPONENT tolerance: transformers, inductors, Hall sensors, relays and fans all care about DC field to different degrees, PMTs need residual fields far below 150 G (high-permeability or multilayer shields), and a mild-steel can's attenuation depends on geometry, seams and saturation - the cited caps are proof the approach works, not a universal thickness spec.
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Derive extraction-element timing from turn separation: with ~0.1 in radius gain per rf cycle and deflector bars 1 in apart, ions cross the bar aperture in ~10 rf cycles, so the pulse must fire within +/-5 rf cycles.
aperture transit ~ (bar spacing)/(radius gain per turn) rf cycles; at ~10 Mc, 10 cycles ~ 1 us, so the firing window is ~+/-0.5 us; rise time is budgeted separately from the allowable field transient while ions occupy the deflectorSource quote & editorial note
the increase in radius of the burst of ions per rf cycle is approximately 0.1 inches and the deflector bars are spaced one inch apart, the pulse must occur within +/- 5 rf cycles.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 8
Editorial note, tabletop extrapolation: Synchrocyclotron-specific hardware (a CW deflector needs no pulse), but the requirements chain - turn separation sets element aperture sets timing budget - is the template for sizing ANY extraction element, including a next machine's septum entrance.
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The 184-inch pulsed electric deflector needed ~75,000 V/cm - about 190 kV across bars spaced one inch - to shift the center of rotation of its full-energy beam into the lowered-field magnetic channel.
E ~ 75 kV/cm; V = E*d ~ 190 kV across 1 in (2.54 cm)Source quote & editorial note
The electric field between the deflector bars necessary to shift the particle center of rotation enough to allow it to pass through the magnetic channel is about 75,000 volts per centimeter.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 8
Editorial note, tabletop extrapolation: Scale perspective without a false law: the required field follows from the integrated kick theta ~ q*INT(E dl)/(p*v) - beam rigidity, electrode length, needed displacement and septum clearance all enter, which is why UCRL-10654 quotes 150-200 kV/cm at 50 MeV while this machine used 75 kV/cm at 200 MeV. Compute a sub-MeV machine's requirement from its own kick integral; it will come out modest, but earn the number.
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Derate pulsed switches for what operation does to them, not the data sheet: 5C22 thyratrons rated 16 kV could not run above 11 kV because the plate voltage reverses in 0.3 us each shot, arcing plate to grid; and where duty exceeds one tube's peak-current rating the report parallels tubes with ballast inductances (their ~5000 A service).
operate 5C22 at <=11 kV (rated 16 kV) under 0.3-us voltage reversal; parallel N tubes with ballast inductance to share 5000 A each bank (verified on page image)Source quote & editorial note
These tubes cannot be operated at plate voltages above 11,000 volts, even though rated at 16,000 volts, because, in operation, the plate voltage reversed in 0.3 us causing arcing between plate and grid.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 13
Editorial note, tabletop extrapolation: The derating discipline - waveform-specific stress, not catalog rating - transfers to every switching element an amateur uses: MOSFET/IGBT avalanche and dV/dt limits in a Marx or inverter play exactly the role the 5C22's reversal limit played here.
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To fire many parallel switches simultaneously, the cited system fed the grids from artificial transmission lines: a 1000-V, 20-ohm trigger of ~0.20 us produced positive ionization of all the tubes in 0.10 +/- 0.01 us (the tube count and per-tube line topology are the report's construction - re-read queued).
per-tube pulse-forming line, 1 kV / 20 ohm / 0.2 us; jitter < 0.01 us across 16 tubesSource quote & editorial note
These lines provide a 1000 volt trigger of 20 ohms impedance for approximately 0.20 microseconds. Applying this trigger to the grids results in positive ionization of all the tubes in 0.1 +/- 0.01 us.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 13
Editorial note, tabletop extrapolation: Relevant only if a next machine adds a pulsed element (fast chopper, time-of-flight kicker): pulse-forming-line triggering is the classic paralleling technique, one option beside modern isolated solid-state drivers - and note the quoted 0.1 +/- 0.01 us is turn-on delay with spread, from which inter-channel jitter is bounded, not measured.
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Fast-pulse transformer lore: keep leakage inductance down by paralleling coils and minimizing core cross-section (1.5 x 1.5 in Hipersil, 2-mil laminations); at 6 kV/turn, interlaminar insulation arcs - splitting the core into two segments halves per-segment voltage and halved those losses; ~90% of input power ends up as core heat (500 W, cores reach 200-300 C), demanding non-shorting water-cooled jackets; vacuum-fill the lucite case with de-aerated oil to kill corona. Result survived 300 kV = 3x rated output.
2:17 turns, 6 kV/turn, two coils paralleled halve leakage L; core split halves interlaminar V; tested 300 kV vs 100 kV service (verified on page image)Source quote & editorial note
Approximately ninety percent of the total power input to the system is eventually dissipated in the transformer cores as heat. At rated operating levels this loss is approximately 500 watts.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 12
Editorial note, tabletop extrapolation: Transferable craft here is the failure mode (interlaminar voltage at high volts-per-turn) and the de-aerated-oil practice - which reduces bubbles and partial discharge, not corona from bad geometry. The 300-kV survival was that transformer's result, not a portable 3x proof-test rule: overvoltage testing at these levels is itself hazardous and can leave latent damage, so test to an applicable HV standard's waveform, duration and partial-discharge limits, remotely, with discharge provisions - not to a generic multiple.
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Specify pulse-discharge capacitors for the real waveform: they had to survive complete charge reversal in 0.3 us, 100 times per second - the best commercial units (GE 0.03 uF / 16 kV, four paralleled per transformer) still failed every 10-20 hours at 11 kV, and their ~0.13 uH internal inductance ate the rise-time budget (total allowance ~0.1 uH referred to the primary). A one-ohm line of 50 paralleled RG-8U cables worked electrically but was abandoned as bulky (6000 ft of cable).
reversal stress 0.3 us full reversal at 100 pps; L_internal 0.13 uH vs 0.1 uH total budget; MTBF 10-20 h (verified on page image)Source quote & editorial note
the capacitor must withstand a complete reversal of charge in 0.3 us 100 times a second without failure.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 14
Editorial note, tabletop extrapolation: Two lessons that outlive the hardware: (1) reversal fraction and reversal time belong in a pulse capacitor's complete duty spec - alongside peak/RMS current, dV/dt, temperature and derating, all of which shorten life too; (2) ESL budgets, not just C and V, set rise time. The paralleled-coax alternative is a distributed pulse-forming line, not a lumped capacitor - engineer it as one (impedance, delay, termination, voltage rating, stored energy).
-
DC resonance charging through the pulse capacitors' voltage reversal gave a step-up beyond the textbook maximum: 11,000 V at the thyratron plates from a 2,750-V supply - four to one against the usual two to one - because each shot leaves the capacitors reversed.
cited circuit: V_plate/V_supply = 4:1 (vs 2:1 classical resonant charging), via post-pulse capacitor reversalSource quote & editorial note
a plate voltage of 11,000 volts on the thyratrons can be maintained with a power supply voltage of 2,750 volts, a step up ratio of four to one as compared with a maximum of two to one in the usual case. The reason for the higher step up ratio is found to be in the voltage reversal of the pulse discharge capacitors each time the system is pulsed.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 15
Editorial note, tabletop extrapolation: Pulsed-modulator craft, not CW-deflector material; file under 'if a next machine ever needs a kicker'. The ratio is topology- and loss-dependent - simulate or measure the actual waveform before sizing a supply on it, and rate every capacitor, switch and insulator for the real reversal stresses.
-
Report and accept the shortfall: the effective rise time came out about 0.15 us against the implied 0.1-us target, and the authors felt that increasing the peak voltage compensates for the longer rise time in this system.
t_rise achieved 0.15 us vs 0.1 us spec (+50%); compensate with higher V_peak (verified on page image)Source quote & editorial note
the effective rise time is about 0.15 us, 50 percent more than that desired. ... it is felt that increasing the peak voltage compensates for the longer rise time of the pulse.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 16
Editorial note, tabletop extrapolation: A commissioning lesson in trade-offs: extraction elements have one strong knob (voltage/field) that can sometimes buy back deficiencies in the others - design in voltage headroom, but check what the slower edge costs in turn selectivity and what the higher voltage costs in breakdown and switch margin before leaning on it.
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Precessional/regenerative extraction must satisfy the quoted three requirements: (a) arrest the precession so the radial-oscillation maximum recurs at one azimuth, (b) obtain sufficient gain per turn - enough to step over the septum wall WITH entrance margin, and (c) minimize losses from axial blowup.
requirements: precession arrested; gain/turn > septum wall + entrance margin; axial losses boundedSource quote & editorial note
The extraction requirements, simply stated, are: (a) The precession must be arrested (b) Sufficient gain per turn must be obtained (c) Losses owing to axial blowup must be minimized.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 7
Editorial note, tabletop extrapolation: The cleanest checklist in this collection for what a next machine's precessional-assist extraction must accomplish - phase-lock the precession to place orbit maxima at the septum azimuth, then count gain-per-turn against septum thickness. Machine-class independent.
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Start the extraction perturbation at a "synchronous radius" defined as where the perturbation field begins and where unperturbed particles would circulate with zero radial amplitude - chosen just inside the radius of normal beam destruction (for the 184-inch, n = 0.155 at 79.8 in, just inside the n = 0.2 point). Reducing this radius eases extraction but costs extracted energy.
184-inch example n(79.8 in) = 0.155; dn/dr ~ 0.055/in inside, 0.138/in outsideSource quote & editorial note
The synchronous radius suitable for deflection in the cyclotron is just inside the radius at which normal beam destruction occurs.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 7
Editorial note, tabletop extrapolation: The siting logic transfers, the threshold does not: put a next machine's septum or regenerator equivalent just inside where its OWN analysis says the beam dies - measured field map, tune calculation and tracking, not a universal n = 0.2 wall (linear radial stability formally extends to n = 1, and real loss radii are set by resonances, apertures and field errors). And every mm inward is extracted energy given away.
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Design a regenerator by the source's seven-step procedure - from nonlinear equations of motion on the measured field through amplitude-dependent tunes to the required momentum kick and its field perturbation (the step contents and gain expressions summarized here are the report's derivation - re-read queued for the equations and variable definitions).
a = -sin(wr*th1)/sin(wr*(th2-th1)), wr = wr(r>R); delta(p') = -p0''*sin(wr*th2)/ sin(wr*(th2-th1))Source quote & editorial note
The determination of the required perturbation for extracting the beam of a synchrocyclotron is made in seven steps.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 6
Editorial note, tabletop extrapolation: The workflow (measured field -> amplitude-dependent tunes -> impulse-matrix tracking -> element strength) is exactly the CYCLOPS-lite pipeline planned for a next machine; the peeler-regenerator field shapes themselves are synchrocyclotron machinery and need not transfer. Treat the sine-ratio gain coefficient as branch- and model-specific once the re-read pins its definitions - it is singular near its denominator zeros, so no monotone smaller-interval-more-gain rule survives unqualified.
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Express regenerator strength as integrated field-times-angle - with B0 in gauss and angle in radians the perturbation integral INT(dB dtheta) reads in gauss-radians, the source's unit convention (its formula, worked table and B0 are the report's data - re-read queued).
integrated perturbation = INT(dB dtheta) [G-rad]; conversion: 1 kG-deg = 17.45 G-radSource quote & editorial note
When B0 is in gauss, B-theta is in gauss-radians.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 17
Editorial note, tabletop extrapolation: The gauss-radian bookkeeping is a handy unit for ANY azimuthally localized field bump (harmonic coils, shims, channel compensation) on a next machine. What fraction of B0 an effective bump needs is geometry-dependent - the same integrated strength over 20 or 60 degrees is a 3x different local field - so compute the integral for the actual bump, without a stock percent anchor.
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In the cited regenerator calculation, the disturbance to axial motion at 1-in axial amplitude was about twice the corresponding radial disturbance from the same field perturbation - large-axial-amplitude particles were the vulnerable population in that analysis.
delta(z') ~ 2x radial disturbance at 1-in axial amplitude; d(axial)/dr of Br from curl B = 0 -> Br = (dBz/dr)*zSource quote & editorial note
For a 1-in. axial amplitude this disturbance is about twice as strong as that occurring in the radial motion from the same field perturbation.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 18
Editorial note, tabletop extrapolation: The transferable warning: any radial-field-gradient extraction element has an off-midplane Br ~ z*dBz/dr whose vertical effect can focus or defocus depending on gradient sign and trajectory - include the deflector fringe and any field bump in the next machine's 3-D tracking rather than assuming the sign or which particles go first.
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Include the magnetic channel's own field in the orbit calculation: the computation lets one modify the regenerator field to account for the channel effect, so that maximum-effort corrective shimming of the channel is not required.
treat channel fringe as a fourth orbit region; adjust regenerator to compensateSource quote & editorial note
The computation enables one to modify the regenerator field to account for the channel effect, and, thus, the maximum effort of corrective shimming for the channel is not required.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 20
Editorial note, tabletop extrapolation: Direct analog for a next machine: the septum and exit-channel iron (or deflector entrance fringe) perturbs the last internal turns - model that perturbation in the tracker and consider compensating upstream (harmonic coil, shim, or the bump program) as ONE option alongside local shielding or shimming of the channel itself; co-optimize rather than nulling one element in isolation.
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RF resonant extraction, as the source frames the choice: among the allowed drive harmonics l, choose the smallest - it needs the least precise match between perturbing frequency and particle motion, which matters where the edge field (and radial tune) changes rapidly (the force model, sector geometry and resonance equation are the report's analysis - re-read queued).
omega = omega0*2*sqrt(1-n)/l, l = 1,2,3...; perturbation F = A*rho*cos(omega*t) for rho>0 in a 60-deg sectorSource quote & editorial note
It is an advantage to choose the smallest value of l, since the choice allows the least sensitivity in matching the perturbing frequency to the particle motion.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 7
Editorial note, tabletop extrapolation: A candidate extraction assist worth a TRACKER experiment before hardware: note that for l = 1 with nu_r near 1 the drive lands near TWICE the revolution frequency, and the required gradient, electrode voltage, bandwidth against tune spread, and isolation from the main RF are exactly what the tracking study must produce before 'an electrode pair and a small oscillator' can be promised.
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The rf gradient needed is modest: the study's IBM 650 median-plane orbit calculations used E = 4.3 kV/cm (design ceiling 'less than 5 kV/cm') applied over a 100-160 degree azimuth region beyond the synchronous radius, for 50-MeV deuterons at 17 kG (n = 0.1) - a field the authors believed easily obtainable from an oscillator independent of the main dee rf, tunable in frequency and amplitude.
E_rf = 4.3 kV/cm, 60-deg sector, two parabolic + one flat electrode; 50-MeV deuterons, B = 17 kG, r0 = 33.68 in, n = 0.1Source quote & editorial note
where we use E = 4.3 kv/cm as the electrical gradient. ... This rf electrical-field gradient, less than 5 kv/cm, is believed to be easily obtainable by an oscillator which is independent of the cyclotron oscillator and which can be tuned to the optimum frequency and amplitude. ... Calculations on the IBM 650 have been done in the median plane only. The perturbation is introduced when the particle is beyond the synchronous radius in a region from 100 to 160 [deg].
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 8
Editorial note, tabletop extrapolation: At a next machine's scale the voltages are small - 4.3 kV/cm across a 2 mm gap is ~860 V peak - but feasibility still means vacuum-RF behavior, feedthroughs, tuning and breakdown checks, and the scheme was never demonstrated on hardware in this report: a promising computed option, not proven practice.
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The variable-energy argument for electrical extraction elements: the source's system - with tunable frequency AND gradient - eliminates the difficulties fixed magnetic extraction systems have on variable-energy machines, where static perturbations set into the pole geometry cannot follow a changing energy and field.
tunable (f, E) replaces fixed (B-bump geometry) for variable-energy operationSource quote & editorial note
The possibility of changing the electrical frequency and gradient to match operating conditions eliminates difficulties arising in magnetic extraction systems for variable-energy machines.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 4
Editorial note, tabletop extrapolation: Supports the next machine's plan-of-record (electrostatic deflector, no fixed magnetic channel) in spirit: an educational machine running several field/energy points wants extraction strength on a knob. A plain electrostatic deflector carries the voltage knob - not the source system's frequency knob - and that adjustability is exactly what a fixed B-bump lacks.
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Vertical beat-frequency loss is the destructive dual of rf extraction: when the source's resonance relation holds AND a vertical electric field proportional to the vertical displacement exists, the axial equation of motion is absolutely unstable - in the 184-inch, even the weak vertical component of the accelerating voltage lost the beam impressively fast.
two conditions per source: its Eq. resonance relation (displayed equation not OCR-readable - scan re-read queued for the exact form) + E_z proportional to z -> absolute axial instabilitySource quote & editorial note
the other necessary condition is that there be a vertical electric field which is proportional to the vertical displacement of the particle from the midplane of the cyclotron. In the weak vertical field component of the accelerating voltage in the 184-inch cyclotron the beam loss was impressively fast. An analysis shows that under these two conditions the equation of particle motion is absolutely unstable.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 5
Editorial note, tabletop extrapolation: A real design caution at any scale: an E_z gradient of the right symmetry near a nu_z resonance can dump the beam. Note dee misalignment gives mostly a dipole-like midplane E_z, not the z-proportional gradient this parametric resonance needs - but asymmetric liners and gap geometry can supply the gradient term, so keep the dee/dummy-dee vertically symmetric and check nu_z against strong rf harmonics at operating field.
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Do not expect an rf perturbation to kick particles out in one pass: in the analyzed arrangement, orbit precession caused repeated phase-dependent encounters with the perturbation, and ultimately all particles were perturbed to larger radial oscillation amplitudes.
amplitude growth is episodic over many turns; ultimately all phases perturbed to large amplitudeSource quote & editorial note
because of the precession of orbits all particles are ultimately perturbed to larger radial oscillation amplitudes.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 9
Editorial note, tabletop extrapolation: Sets expectations for any resonant/precessional scheme on a next machine: the growth is episodic over many turns, so judge schemes in the tracker by turns-to-extraction and septum-hit fraction rather than single-pass kick size - the detailed evolution is deterministic and scheme-dependent, so track your own.
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Condition the RF system past its working dee voltage and hold it there: the 63-inch reached 75 kV dee-to-dee under vacuum after routine difficulties and then maintained it for long periods without tendencies to failure - sustained hold, not a momentary peak, was what let them call the RF solved.
acceptance pattern: sustained hold above working voltage under vacuum; the cited 75 kV is that machine's demonstrated pointSource quote & editorial note
A dee voltage of 75 kv dee-to-dee was reached after some routine difficulties were overcome. The cyclotron now maintains this voltage for long periods of time without showing any tendencies to failure.
Editorial note, tabletop extrapolation: The transferable practice is endurance-above-operating-point as the acceptance test for the LDMOS upgrade - with the margin chosen from the new system's own component deratings (capacitors, feedthroughs, transistor SOA), stored energy and interlocks, and with arc and X-ray monitoring during the test. A margin that survives only seconds is not margin; a margin that exceeds a component rating is not a test, it is a failure in progress.
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On the 86-inch, dee-voltage pickup rectification moved from germanium diodes - whose location let cyclotron neutron bombardment affect the resistivity calibration - to a Type 2C40 vacuum-tube rectifier, unchanged by neutron bombardment; with it, the calibration remains constant unless the probe-to-dee distance changes.
Source quote & editorial note
The location of the germanium crystals was such that neutron bombardment from the cyclotron affected the resistivity calibration. With the present system, the vacuum tube rectifiers are unchanged by neutron bombardment and, unless the probe-to-dee distance is changed, the calibration remains constant.
Editorial note, tabletop extrapolation: Two transferable halves, properly scoped: (1) semiconductor sensors near the chamber are a calibration-drift RISK once neutrons appear - characterize candidate devices at the expected fluence rather than banning them; (2) a capacitive dee-voltage pickup is calibrated GEOMETRY - fix and document the complete pickup geometry and signal chain, or every calibration is void. Bears directly on retiring the reference machine's uncalibrated ~1.3 kV dee-voltage number.
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Build a self-calibration into beam calorimetry: ORNL inserted an electric boiler (three 9-kW heaters, recording wattmeter) in the target cooling-water line so the operator could calibrate the water delta-T recorder against known electrical power up to 27 kW in a few minutes, any time.
calibrate water delta-T calorimeter with in-line electric heater of known powerSource quote & editorial note
It is now possible for the operator to obtain in a few minutes a complete calibration of the probe water temperature differential up to a maximum power of 27 kw.
Editorial note, tabletop extrapolation: The trick transfers if the calibration heat matches the beam's thermal path: a nA-to-uA tabletop calorimeter (thermistor on an isolated cup) can be calibrated with a surface-mount resistor dissipating known milliwatts - verify the heater and beam deposit heat comparably, calibrate over the working range, and budget for backscatter, escaping radiation and conduction losses before calling the result absolute.
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Cross-check calorimetric beam power against electrically computed power at every operating point: on the 86-inch, calculated and cooling-water-measured power agreed within 5% across the tested range - persistent disagreement flags an instrumentation or beam-loss problem.
P_beam = I_beam * (E_k/q) - kinetic energy per charge, not dee voltage; cited machine's achieved agreement: ~5%Source quote & editorial note
The measured beam power is determined from the measured temperature rise in the target cooling water. The calculated power and measured power readings agree within 5%.
Editorial note, tabletop extrapolation: The redundancy principle transfers even at nA: Faraday-cup current times computed kinetic energy should match any independent measurement. Set your own acceptance band from the actual uncertainties (current, energy, calorimetry or activation), and treat activation as a separately calibrated fluence check - it needs cross sections, target data and timing, and works only above the chosen reaction's useful yield range.
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Ion-source axial position is a first-order machine parameter: raising the 86-inch source 1.5 in - leaving it one inch below the magnetic center, with the accelerating slit raised the same amount - was credited with taking protons from ~19 to ~24 MeV.
Source quote & editorial note
The increase in proton energy resulted from relocation of the ion source 1 1/2" upward; the source is now effectively only one inch below the magnetic center.
Editorial note, tabletop extrapolation: On the reference machine, treat filament/chimney height relative to the MAGNETIC median plane (find it by measurement - it need not match the mechanical midplane) as a tuned parameter worth systematic scans. What the height buys is centering, vertical transmission and usable radius; at a fixed field and radius the energy is p = qBr regardless, so measure where the gain actually comes from rather than expecting a fixed percentage.
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Diagnose an off-center beam from where it strikes: on the 86-inch, beam hitting the periphery of the south dee revealed the center of rotation was offset ~3 inches south, and the correction included moving the dees 1/2 inch south. Burn marks and asymmetric losses carry orbit-center information.
Source quote & editorial note
the beam striking the periphery of the south dee. This condition resulted from the center of rotation of the beam being offset to the south by a distance of approximately three inches. ... The dees were moved 1/2 in south, measured at the horizontal center line of the dees.
Editorial note, tabletop extrapolation: Witness marks on the reference machine's dee edges are a free orbit-centering CLUE - corroborate with radial probe scans and the field map before moving anything, since phase, axial focusing and apertures make similar marks; then correct at the source or dees once the cause is identified.
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Give the ion source a positive mechanical registration: a bracket on the 86-inch liner fixes the source one inch below field center, insures proper positioning AND grounding of the stem's lower end, guarantees the same position run to run, and reduces rf-pickup heating of the support tube.
Source quote & editorial note
To insure proper positioning and grounding of the lower end of the ion source, a bracket has been attached to the west side of the liner which places the ion source one inch below the center of the magnetic field. This arrangement insures that the position will be the same from run to run and also reduces heating of the tube due to rf pickup.
Editorial note, tabletop extrapolation: Cheap and directly imitable — once the optimum source position is found by scanning, capture it in a hard registration feature so it survives every source rebuild; grounding the support also kills a stray RF-heating path.
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Measure the z-wise (axial) beam distribution with a multi-segment probe at several radii: the 22-inch's five-segment measurement (its Figure 5) showed most proton loss to the dees occurs during early revolutions, with only a small percentage lost beyond half the maximum radius.
Source quote & editorial note
most of the loss of protons to the dees occurs during early revolutions. Only a small percentage of the beam is lost beyond one-half of maximum radius, Figure 5. ... [Figure 5:] Z-WISE BEAM DISTRIBUTION on Each of Five Segments
Editorial note, tabletop extrapolation: Both the finding and the instrument transfer as guidance: stack 3-5 insulated foils as a segmented z-probe on the reference machine to see where the beam sits vertically, and expect the early turns to deserve the tuning effort - on that machine, beam surviving to half radius mostly escaped further DEE loss; extraction, phase and radial channels are separate ledgers.
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Identify beam species with magnetic resonance curves: sweep magnet current at fixed RF and record probe current at full radius - H1+ and H3+ appear as separate peaks (68 gauss apart on the 22-inch; H3+ rides the third RF harmonic). At low arc current the H3+/H1+ ratio is high; raising arc current increases both total H1+ and the H1+/H3+ ratio.
resonance: B = 2*pi*m*f_RF/(h*q) - specify the harmonic h per peak (H1+ at h=1, H3+ at h=3); at the same B and radius the H3+ energy is 1/3 the H+ energySource quote & editorial note
At low arc current the ratio of H3+ ions to H1+ ions is high. The total number of H1+ ions and the ratio of H1+ ions to H3+ ions may be increased by increasing the arc current.
Editorial note, tabletop extrapolation: The prior art for a source-species test on the reference machine: a field sweep at fixed frequency is a species analyzer needing only the existing probe, and source arc power is the species-ratio control - expect molecular ions to be strong at weak arc, and raise the arc within the source's thermal and electrical limits when protons are wanted. (Fig. 6, PDF p.18, shows the resolved peaks.)
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Shortening the 22-inch ion-source arc slit from 2.5 in to 0.5 in increased the ratio of accelerated beam power to ion-loading power, as predicted - emission the dees cannot accept loads the RF without making beam.
Source quote & editorial note
the ion source arc slit was shortened from 2 1/2" to 1/2". Thereafter the ratio of accelerated beam power to ion loading power was increased, as predicted.
Editorial note, tabletop extrapolation: On a tabletop machine where every watt of RF matters: try slit length as an EXPERIMENT, watching accepted beam per unit dee loading rather than raw source output. The over-emission mechanism is the natural reading of the ORNL result, but slit changes also move plasma and extraction optics, so let the measurement decide.
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Negative dee bias can substitute weakly for an accelerating slit: on the 22-inch, increased (negative) dee bias raised full-radius beam by up to 30%, but only with no accelerating slit mounted - ORNL reports the effect 'is not observable when an accelerating slit is used'. [Corrected 2026-08-23: the earlier rule also said the slit 'outperforms the optimum bias'; the source shows the two are not additive, not that one beats the other. The sign of the bias and the with-slit null are on the cited page, just outside the quote - ORNL-1339 p. 16: 'This effect is not observable when an accelerating slit is used' and 'the increased negative bias potential gives non-optimum-phased ions ... a deeper penetration into the rf electric field'.]
Source quote & editorial note
an increase in bias potential on the dees increases the beam accelerated to maximum radius by a factor of as much as 30% when the cyclotron is operated without an accelerating slit (rf) mounted on the dee.
Editorial note, tabletop extrapolation: Worth a cheap experiment on the reference machine - with a proper RF-rated bias-injection network (choke/filter, insulation, supply protection), never a bare DC supply on a live dee. ORNL's stated reading is that bias pulls badly-phased ions deeper into the gap field; with a slit installed they saw no bias effect. The source does not rank the two approaches - test both on the actual machine.
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Declare a chamber vacuum-tight by isolated rate-of-rise, not ultimate pressure alone: the 63-inch was accepted at 1e-5 mm Hg with 0.00025 microns/sec (~0.9 mTorr/hr) valve-off.
method: pump down, soak, valve off, measure dP/dt; gas load Q = V*dP/dt; the cited 2.5e-4 micron/sec is that chamber's acceptance, not a portable numberSource quote & editorial note
the pressure was reduced to 10^-5 mm Hg. A rate of rise of 0.00025 microns/sec indicates that the system is vacuum tight.
Editorial note, tabletop extrapolation: Log an isolated rate-of-rise after every reassembly as a regression test against the machine's OWN baseline - the number folds together leaks, outgassing and permeation scaled by volume, so it does not transfer between chambers in either direction; where true leak-tightness must be established, helium leak testing is the tool.
Cited in: The Vacuum Budget of a Cyclotron
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Re-measure the magnetic field with the tank evacuated before commissioning: the 63-inch found distortion from atmospheric loading negligible, and its as-commissioned first-harmonic inhomogeneity measured ~0.03%.
first harmonic target ~3e-4 of main field (63-inch as-commissioned)Source quote & editorial note
It was found that distortion of the magnetic field when the tank is evacuated is negligible. Latest measurements of the magnetic field reveal a first harmonic inhomogeneity of approximately 0.03%.
Editorial note, tabletop extrapolation: Two transfers: verify a next machine's field map with the chamber assembled and pumped (pole deflection under vacuum load is a real worry that proved negligible for them - measure once to confirm); and read 0.03% as what a carefully shimmed classical machine ACHIEVED - the new machine's allowable first harmonic comes from its own orbit-centering budget, and note 0.03% of a 0.5-1 T tabletop field is 1.5-3 G, so gauss-level targets and fractional targets must be kept straight.
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Budget real machine runs for beam characterization: in the 86-inch's post-modification quarter, 15 of 50 tabulated bombardments (30% by run count) were beam-profile or energy-measurement runs - characterization scheduled as work, not squeezed in as overhead.
~1/3 of runs devoted to beam profile + energy measurement after any major changeSource quote & editorial note
The bombardments are tabulated below: Beam profile 10, Isotope production 8, Experimental 16, Energy 5, Physics 7, Radiation damage 4.
Editorial note, tabletop extrapolation: A quarterly cadence in miniature for the reference machine: after any change (RF upgrade, source rebuild), the run log should show dedicated profile and energy runs alongside the physics runs - the ORNL table records the proportion by count; durations and ordering it does not give, so import the habit, not a timeline.
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Corroborate beam energy with independent methods before calling it established: the 86-inch's ~23 MeV at 30.5 in was called well established after foil-stack range, calorimetry, and nuclear production yields agreed over many runs at the same radius.
E confirmed = foil-stack range + calorimetric P/I + activation yield, mutually consistentSource quote & editorial note
Energy measurements by foil stack, by calorimetry, and by production yields indicate the average energy of the beam is now approximately 23 Mev at 30.5 inches. This value is well established, since many runs have been made at this radius.
Editorial note, tabletop extrapolation: Directly actionable for the '~150 keV-class computed' number on the reference machine: convert computed to measured with independent checks where feasible - foil range/transmission steps (which at 150 keV means micron-class calibrated foils) and, at higher current after the RF upgrade, cup calorimetry with E = q*P/I and its backscatter/thermal corrections. A single method is weaker than agreeing methods.
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Take beam power up in steps with a calorimetric measurement at every level: the 41-kW record (1.85 mA average at 22.5 MeV) was reached by increasing from a steady 0.5 mA progressively, measuring dissipated target power calorimetrically at each step — so the record is a measured curve, not a single meter reading.
Source quote & editorial note
With the cyclotron operating steadily at 0.5 ma and at 22.5 Mev, the beam was increased progressively until the metered beam current approached 2 ma. At each level the power dissipated on the target was measured calorimeterically. The maximum beam power measured in this manner was over 41 kw, corresponding to an average beam current of 1.85 ma.
Editorial note, tabletop extrapolation: The stepped-ladder protocol transfers to any record attempt on the reference machine — each step cross-checks meter vs thermal response and catches secondary-emission or leakage error before it contaminates the headline number; a record with only one point behind it is fragile.
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Track the RF power balance as a commissioning health metric: on the 86-inch, 40% of the power expended in accelerating ions reached the target at high beam, twice the electrical efficiency seen at low beam - dee excitation losses are roughly fixed at a given voltage, so efficiency improves as beam (and with it ion-loading power) rises.
separate the denominators: target-transport efficiency = P_target/P_ions_accelerated (the quoted 40%); RF efficiency = P_beam/P_osc (a different, smaller number); dee excitation ~ fixed at set voltage, ion loading rises with beamSource quote & editorial note
the net ion-loading efficiency was 40%, that is, 40% of the power expended in acceleration of ions was to the target. There was a two-fold increase in electrical efficiency as the beam was increased.
Editorial note, tabletop extrapolation: On the reference machine at nA the beam power is invisible next to fixed RF losses - the transferable lesson is the metric, not the number: log P_beam/P_RF per run, and chase resonator Q and coupling rather than amplifier watts for efficiency on any small machine.
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Use expendable grazing-incidence targets for high-power tuning: aluminum targets struck at grazing incidence spread the power over a larger footprint and withstood full 86-inch beam during adjustment, reserving real targets for production.
alpha measured from the surface: footprint A = A_normal/sin(alpha), heat flux q'' = q''_normal * sin(alpha)Source quote & editorial note
grazing-incidence type aluminum targets were used because of the high beam intensities they withstand.
Editorial note, tabletop extrapolation: The geometry trick matters twice on a small machine: thermally on any upgrade path (do the target thermal model with actual beam energy, spot size and interception - even mW into an isolated foil or microscopic spot can damage it, so 'nA cannot melt anything' is not a law), and for beam viewing, where a tilted phosphor or foil presents more area to the spiral - a detector-specific claim to verify by eye, not assume.
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Support first beam with a radiation signature plus a physics argument, not probe current alone: the 63-inch's brass target at 21 in showed gammas at 8x background, and since singly-ionized nitrogen at that radius would carry only 2.5 MeV, the report concluded the observed burst was due to N3+.
species/energy check = radiation only possible if q/m assumption correctSource quote & editorial note
Since the singly-ionized nitrogen ions at this radius have an energy of only 2 1/2 Mev, it may be concluded that the burst of radiation observed was indeed due to triply-charged nitrogen ions.
Editorial note, tabletop extrapolation: The evidentiary pattern transfers - an observed nuclear signature whose energetics disfavor the alternative species is strong evidence - but treat it as evidence, not proof: identify the radiation, use modern Q-values and cross-sections, run detector controls, and exclude electron-induced X-rays, contaminants and other q/m candidates (and remember radiative capture has no threshold, only Coulomb suppression). The reference machine's 5.6x-background best-beam sits in this tradition as supporting evidence for acceleration, with species claims needing their own case.
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Map internal beam current vs radius early: first-month 63-inch probe currents ran 2000, 500, 170, 30 uA at 5, 10, 14, 18.5 in, were unreliable beyond that, with ~1 uA ESTIMATED at the 25.5-in extraction radius - a factor of ~2000 between the inner reading and the uncertain outer estimate during commissioning.
commissioning-era attenuation: ~3 orders of magnitude center-to-edge is normal, not brokenSource quote & editorial note
Current measurements beyond 18.5" were unreliable; the current at the maximum radius, 25.5", is estimated to be of the order of one microampere.
Editorial note, tabletop extrapolation: Calibrates expectations qualitatively, not in absolute scale: an untuned machine can lose orders of magnitude between small radius and full radius, so log the whole I(r) curve - its shape (where the loss happens) is the tuning roadmap. This is one machine's commissioning history, not a norm to be satisfied with.
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Bound beam energy and species by activation when direct measurement is unavailable: 63-inch targets (graphite, CuO, TaN) were bombarded and the induced activities (112-min F-18, 15-hr Na-24, 10-min N-13...) identified by decay curves, and the reaction thresholds then bounded the beam energy - a preliminary identification the source backed with target chemistry, not a half-life alone.
Source quote & editorial note
A carbon (graphite) target gave rise to 112-minute and 15-hour activities which are assigned to F 18 and Na 24 respectively.
Editorial note, tabletop extrapolation: Not a casual check, and not closed to the reference machine by any blanket "threshold": which reactions are open depends on the beam SPECIES and the target ISOTOPES - D-D is exothermic with no threshold, so 150 keV deuterons make neutrons and tritium, and neutrons can then activate surrounding materials by capture, with no charged-particle threshold at all (dg-1041, dg-1047). Before using activation as an energy bound: pick candidate reactions from modern Q-values, thresholds and cross-sections for the actual beam and target; treat a half-life alone as preliminary (ambiguous assignments, tiny near-threshold yields, contaminants that dominate) until backed by an absorber or spectrum check; and accept that deliberately activating a target means prompt radiation, a survey, dosimetry and handling the residual activity. [Corrected 2026-08-23: earlier wording said "below nuclear thresholds the 150-keV reference machine cannot use this" and called the method "only a GM counter and a stopwatch" - the same absolute already corrected at dg-1041, dg-685 and dg-695.]
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Make ion-source position adjustable from outside the vacuum: the 63-inch found source-to-field alignment 'extremely critical', necessitating external adjustments - the 86-inch's Selsyn-driven rotator is the report's example implementation (scan re-read queued).
Source quote & editorial note
The alignment of the source with the magnetic field is extremely critical, as was expected, and makes it necessary to provide for external adjustments of the ion source.
Editorial note, tabletop extrapolation: Strong design input for a next machine: budget at least one externally accessible source degree of freedom (rotation or z) - both ORNL machines provided it after finding the optimum unreachable blind. Adjustment under beam is the convenient form; adjust-then-pump iterations reach the same optimum, slower.
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Apply a small negative DC bias (1-2 kV on the 63-inch) to the dees while RF oscillation is being established, to sweep out ions formed during startup and prevent them loading or destabilizing the rising RF.
dee bias -1 to -2 kV on the 63-inch's ~50 kV dees (2-4% of dee voltage) during RF establishmentSource quote & editorial note
A negative voltage bias, 1 to 2 kv, is applied to the dees in order to sweep out any ions that may be formed while oscillation is being established.
Editorial note, tabletop extrapolation: Transferable as a startup practice: a bias supply that sweeps ions out during RF ramp-up is the classical cure for start-up loading (dg-320, dg-680 - polarity differs by machine and both worked). What voltage a small machine needs is found at the machine; the 63-inch's 2-4% of dee voltage is the documented anchor, not a scaling law.
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Fit carbon lips to dee edges where sparking limits voltage: installed on the 86-inch, in a new design, to reduce sparking at the increased 400-500 kV dee-to-dee voltage.
Source quote & editorial note
Carbon lips of a new design were installed on the edges of the dees to reduce sparking at the increased dee-to-dee voltage, 400-500 kv, required for operation at the high energy level.
Editorial note, tabletop extrapolation: The 400-500 kV is MW-era and does not transfer; the material practice is a candidate to test - if the reference machine's 5-13 kV upgrade sparks at the dee gap, carbon edge pieces are the period remedy and trivially machinable. Verify grade choice and watch for carbon dust on insulators; and note ucrl-10654's caveat that carbon loses its bake-in minutes after voltage-off (dg-744).
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Bench-test an ion source on a 180-degree beam path in the magnet before installing it: the 63-inch source was tested dc by collecting after a half-turn, measuring the species mix - 8 mA N+, 2 mA N++, 2 mA N+++ (the quoted result; the report's fuller qualification detail: scan re-read queued).
Source quote & editorial note
In dc tests the output of the source, measured after the beam had passed through a 180 deg path in the magnetic field, was: 8 ma of N+, 2 ma of N++, and 2 ma of N+++.
Editorial note, tabletop extrapolation: The 180-degree bend uses the cyclotron's own field as a mass spectrometer with the RF off — on the reference machine this is precisely the source-species test geometry: source + static field + offset collector measures the H+/H2+/H3+ mix directly before any acceleration studies.
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When a source underperforms, look at where the drain current goes: the 22-inch dc injection source gave only 30 mA against its predecessor's 75, and the report's definite clue was persistent high drain to the accelerating electrode - present even in dc tests - pointing at interception rather than production.
account for source output as beam + electrode drain; drain locates the lossSource quote & editorial note
It was never possible to make a dc test without high drain to the accelerating electrode. This is a definite clue to the lower output obtained in the rf tests.
Editorial note, tabletop extrapolation: Current bookkeeping is cheap diagnosis: meter the puller and chimney drains separately from the Faraday cup. A weak beam with a hot puller points first at geometry near the source exit - then confirm by varying extraction voltage, alignment and arc conditions, since plasma meniscus, secondaries and leakage also move those meters, and arc power can reshape the optics as well as the density.
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Isolate radiation effects with matched controls: ORNL found no evidence of thermally-driven mass transfer and associated the enhanced corrosion quite definitely with the proton irradiation - a conclusion earned by control work against the thermal alternative (the control constructions are the report's methods section - re-read queued).
Source quote & editorial note
no evidence of the mass transfer type of corrosion due solely to a thermal gradient is found. The enhanced corrosion observed in Figure 2a seems to be quite definitely associated with the proton irradiation.
Editorial note, tabletop extrapolation: The discipline transfers whole to any 'the beam did X' claim: run a sham control reproducing the specimen's full temperature-time history and every non-beam condition - identical-setup-minus-beam is only adequate when beam heating is negligible or separately reproduced. Log uncertainties honestly in the lab book while at it.
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Central-region orbit centering couples source radial position to dee voltage: with the Davis axial source confined to r < 2.5 in, the machine is forced to comparatively low dee voltages (20-30 kV) so the first-turn radius matches the available source position and the orbits stay centered — dee voltage is set by geometry, not by available RF power.
first-gap geometry couples V_dee to source/puller radius: r_1 = sqrt(2*m*q*V_gap)/(q*B) for acceleration from rest through the gap potential - initial energy and RF phase correct it furtherSource quote & editorial note
the ion source position is limited to a maximum radius of 2.5 inches. This forces operation at comparatively low dee voltages (20-30 kv) in order to center the orbits.
Editorial note, tabletop extrapolation: The design logic transfers directly to a next machine's central-region layout: pick dee voltage and source-puller radius TOGETHER from the first-orbit geometry. It also cuts the other way for the reference machine's 5-13 kV upgrade: raising dee voltage moves the optimum source position outward — re-scan source position after the RF upgrade.
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Distrust scale-model magnet studies at excitation extremes: the Davis model magnet could not be operated at the extremely low planned field level (3.5 kilogauss) - the quoted limitation; the full-scale consequences and iron rework are the report's account (scan re-read queued).
Source quote & editorial note
it was not possible to operate the model magnet at the extremely low (3.5 kilogauss) field levels at which we might like to operate the full scale machine.
Editorial note, tabletop extrapolation: Modern translation for the FEMM pipeline: a model (physical or FEM) validated at one excitation does not certify another — iron saturation state changes the profile shape, so re-run the field solution at every planned operating point, especially the lowest, and verify the real magnet across its full excitation range.
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Shape central-region iron with a plug and deliberately saturating caps so one geometry serves multiple field levels: the final Davis design put the 8-in axial plug 5.5 in from the valley floor with 3.5-in caps that saturate at high field - their incremental contribution shrinking - while filling in the central field hole at low field.
Source quote & editorial note
moving the 8 inch plug to 5.5 inches from the valley floor and to extend the caps to a length of 3 1/2 inches. These caps saturate at high levels, but fill in the central "hole" at low fields.
Editorial note, tabletop extrapolation: Deliberately-saturating iron as a field-programming element is a trick FEMM (with the real BH curve) models well: a piece sized to saturate at the main operating point contributes mostly at low field - but saturated iron keeps its magnetization, so verify the high-field map still meets spec rather than treating the cap as magnetically gone.
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Davis computed trim-coil settings with a linear program against Smith-Garren isochronous standards; the accepted fields' greatest deviation from isochronism was under 15 gauss in all cases - roughly 1e-3 of the working field, the calculation's achieved residual.
max |B - B_isochronous| < 15 G (~0.1-0.4% of field), trim settings by linear programSource quote & editorial note
The isochronous fields are obtained with trim coil settings computed by a linear program, and their greatest deviation from isochronism is less than 15 gauss in all cases.
Editorial note, tabletop extrapolation: Calibration, not criterion: what any machine tolerates is the accumulated RF phase slip - the signed integral of the frequency error over ITS acceleration history - so run the phase-slip integral in the tracker for the actual field map, turn count and dee voltage, and let that set the gauss tolerance; a few-tens-of-turns classical machine and a hundreds-of-turns AVF machine land in different places by exactly that arithmetic.
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Get candidate central-region starting conditions by backward tracking: Davis estimated them by placing ions on a known-good 12-in equilibrium orbit and de-accelerating them to the center, then launched forward acceleration runs from those conditions - bypassing the ill-defined source-gap region on the first pass.
integrate equations of motion with reversed energy gain from EO inward to r=0Source quote & editorial note
The starting conditions for all cases were estimated by starting the ions on an equilibrium orbit of 12 inch radius and de-accelerating them to the center.
Editorial note, tabletop extrapolation: Directly implementable in the Python orbit tracker: find the equilibrium orbit at modest radius (well-conditioned), integrate backwards keeping the RF phase time-consistent, and read off CANDIDATE source-slit and puller coordinates - then validate with a full central-region field model and forward tracking; the backward pass suggests the geometry, it doesn't determine it.
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A deliberate central field bump can beat the computed profile in practice: Davis start-up data with 42-MeV alphas showed possibly 10% more extracted beam running trim coil 1 at +22 A (producing the central radial bump) than at -145 A (the computed profile).
Source quote & editorial note
the beam measured at extraction is augmented by possibly 10% by using 22 amps in trim coil number 1 rather than -145 amps. The former produces the central radial bump.
Editorial note, tabletop extrapolation: Consistent with the classical-cyclotron instinct - a small central bump (field falling with radius from turn one) focuses the early turns where the ORNL 22-inch z-studies located most dee loss - as a HYPOTHESIS the correlation supports, not a demonstrated mechanism. Empirically checkable on the reference machine with shim washers at the pole center: calculate the phase-slip cost first, map the shimmed field, and measure both transmission and where the losses move.
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Cross a betatron resonance on paper before crossing it in beam: the Davis orbit code showed particles pass the 3/3 radial resonance at 6-7 in radius with build-up that 'is not excessive and soon damps to 0.3 inch' - the resonance was accepted quantitatively rather than avoided.
compute the FULL transient amplitude through the resonance and compare the maximum excursion (not just the settled value) plus beam envelope against apertureSource quote & editorial note
The particles pass through the 3/3 resonance at a radius of 6-7 inches. The computer calculations show that the radial oscillation build-up at resonance is not excessive and soon damps to 0.3 inch.
Editorial note, tabletop extrapolation: Method for the CYCLOPS-lite tracker: don't just plot nu_r(r) and forbid resonance lines - integrate through them with realistic errors and acceleration rate, and report maximum excursion in millimeters against the aperture. A fast-crossed resonance can be acceptable if the complete envelope keeps clearance; 'damps' in the historical usage reflects detuning and adiabatic effects, not dissipation.
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A computed field map validated by orbit code can produce first beam without empirical shimming iteration: Davis obtained a 21-MeV H2+ internal beam on the first attempt using the computed field, taken as confirmation of both the magnetic measurements and the orbit calculations.
Source quote & editorial note
the validity of the calculations and magnetic field data is supported by the fact that we obtained an internal beam of 21 MeV H2+ ions using the computed field on the first attempt.
Editorial note, tabletop extrapolation: The 1966 encouragement for a next machine's compute-first pipeline (field map -> tracker -> build): careful measurement plus an honest tracker produced first beam on the computed field, first attempt, on that machine. One result is precedent, not promise - keep shim stock on hand, and let the pipeline earn trust machine by machine.
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Sequence commissioning around your shielding, using a heavier/slower species first: Davis deliberately declined to accelerate protons until the shielding vault was complete, doing all early beam work with H2+ and alphas whose lower velocity and yield kept radiation manageable.
Source quote & editorial note
We have not attempted to obtain particle beams for the cases discussed here as we do not plan to accelerate protons until the shielding vault is completed.
Editorial note, tabletop extrapolation: Directly relevant to the plan's shielding gate: species choice is a radiological control. Commissioning on H2+ at the same B*rho halves the total kinetic energy and quarters the per-nucleon energy versus protons - same tuning fields, gentler consequences - and the proton program waits until the vault or survey case is ready. Davis's sequencing is the model; the record itself says only that they deferred protons until shielding was complete.
Cited in: Shielding a Small Cyclotron
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Design the magnet around the report's four field premises: a steel- and copper-free cylindrical 'gap' whose diameter is about nine times its axial height (the quoted ratio); mid-plane symmetry; no azimuthal dependence; and a field falling with radius gently enough that n = -(R/H)(dH/dR) stays well below 1/5 at all used radii - the report's working condition.
gap diameter ~ 9x gap height; n = -(R/H)(dH/dR) << 1/5 inside the used radius; field decreases linearly with radius to the gap edgeSource quote & editorial note
This region, called the "gap," should have a diameter about nine times as great as its axial dimension.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 6
Editorial note, tabletop extrapolation: CORROBORATING, not new - the same premises underlie Livingston-Blewett and Wouters (corpus already carries 0<n<1 stability). TID-454's working condition is the stricter n<<1/5; note its own 130-in/14-in example is 9.3x. The reference machine's 8-in poles over a wide gap fall far short of 9x, which is exactly why usable radius is scarce; a next machine's gap choice should respect this proportion.
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Use pole-tip efficiency E as a design scorecard: the report's analysis gave E = 0.64 as a realistic goal for experimental magnet design, within its framework of benchmark values for ideal and practical pole configurations (report-attributed; scan re-read queued for the definition and benchmark set).
E = 0.64 experimental design goal (tid-454); companion benchmarks (max 1, ~0.71 coils-far-from-gap, ~0.52 any-field pole) report-attributed pending re-readSource quote & editorial note
An effort to obtain a value of the pole-tip efficiency, E, which could be used as a goal for experimental magnet design gave E = 0.64.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 25
Editorial note, tabletop extrapolation: Gives the next machine's FEMM loop a quantitative habit: compute gap-flux/pole-base-flux utilization for each candidate tip and compare candidates against each other and against the report's 0.64 goal - treat the absolute expected range for a small pole as something the FEMM runs themselves establish.
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Cutting a groove into the pole face just inside the raised edge extends the useful field radius to about 96% of the pole radius - a result the report calls unquestionably correct; the ~92% raised-edge-alone baseline is report-attributed (scan re-read queued for its antecedent).
groove inside raised edge -> useful radius ~0.96*R_pole; baseline ~0.92 report-attributed; at unchanged B the energy gain is (0.96/0.92)^2 - 1 = 8.9%Source quote & editorial note
It is shown that this can be increased to about 96 per cent by cutting a groove into the pole face just inside of the raised edge. This result may be obtained in several ways and is unquestionably correct.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 25
Editorial note, tabletop extrapolation: On 8-in poles the 92->96% difference is ~9% in energy at fixed field - cheap to try in FEMM and on the real shims; the tapered-pole-superiority claim and the NYO-780 comparison need their own citations before leaning on them.
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Treat the analytic equipotential shim shape as a starting point: where the steel surface is not an equipotential, the source says the final contour is best determined experimentally - an approximate shim on an otherwise-final pole, refined against measurement.
Source quote & editorial note
The contour of the shim when the steel surface is not an equipotential is best determined experimentally. An approximate shim can be put on a pole which otherwise has its final form.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 8
Editorial note, tabletop extrapolation: The next machine's shim program: FEMM (finite permeability, saturation modelled) resolves much of what 1952 needed bench passes for - validate the final contour against a probe map where the nonlinearity is significant, as NYO-780 (p.7) did with its bolt-together model magnets.
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Estimate the field contribution of fully saturated cylindrical shim features by treating them as uniformly magnetized: cylindrical spikes act approximately as point charges m = M*A at their tips (plus images in the adjacent poles), with M = (B-H)/4pi (Gaussian units - in SI, M = B/mu0 - H).
Gaussian cgs: m = M*A, M = (B-H)/4pi at saturation; midplane field from point charges at spike tips + images (source Eqs. 7-8); SI: M = B/mu0 - HSource quote & editorial note
If the spikes are cylindrical, the field due to them may be treated approximately as that of point charges placed at their tips with strength m = MA.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 8
Editorial note, tabletop extrapolation: Handy closed-form sanity check for slender, demonstrably saturated cylindrical features (a spike or thin button) before FEMM; treat the excitation independence as approximate - the saturated region and residual susceptibility still move a little with drive - and don't stretch the point-charge picture to fat cones.
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Keep magnet coils as small as a reasonable power budget allows: coil resistance grows with mean circumference (the quote), and the steel circuit that must wrap around the coil grows with it - the report's steel-scaling expression accompanies the quoted argument (scan re-read queued).
R_coil ~ mean circumference; steel volume ~ (2*coil height + radial width); achieve small coils via high average conductivity (material, low temperature, high space factor)Source quote & editorial note
The resistance of the coil is proportional to its mean circumference ... the coil should be as small as is consistent with a reasonable power requirement.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 25
Editorial note, tabletop extrapolation: The compounding is the point - on any H-frame rebuild, fat coils cost twice (copper AND the longer steel circuit around them), so invest in space factor and cooling before adding turns.
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In the report's practice, a high-current low-voltage magnet coil needs insulation only to maintain mechanical separation of the conductors; the report pairs this with direct cooling through a few large channels in large conductors rather than many small ones.
Source quote & editorial note
In a high-current low-voltage coil, insulation is required only to maintain mechanical separation of the conductors.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 25
Editorial note, tabletop extrapolation: What transfers is the architecture - few turns of heavy conductor at high current, direct cooling through generous passages - which beats many-turn fine-wire coils on space factor and pumping pressure. The bare-minimum insulation standard does not transfer: a modern coil wants verified turn-to-turn and ground insulation against inductive transients (dg-218's dump events), abrasion, thermal aging and coolant exposure, cheap as modern materials make it.
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When no large winding machine is available (winding on site), build the coil as a flat-wound helix of conductor pieces fabricated as annulus sectors and joined into a continuous helix, cooled by water tubes on the inner and/or outer circumference.
Source quote & editorial note
A second type of coil which is more attractive, when the coil must be wound at the cyclotron site, is a flat-wound helix.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 26
Editorial note, tabletop extrapolation: Directly a garage-scale construction technique: cut flat copper sectors, stack into a helix, join into a continuous conductor - no winding mandrel needed. The joints are the engineering: braze for permanent low-resistance splices, bolt only with designed contact pressure and area (the report's joint-sizing criterion: scan re-read queued for the number), and place cooling per the report's tube arrangement.
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Choose coil proportions by minimizing total owning cost - the report optimizes the combined costs of steel, copper, and energy against the coil OD/ID ratio (its Eq. 114 and nomographs; details report-attributed, scan re-read queued for the equation and the 1952 unit costs).
minimize C(steel volume, copper volume, energy over machine life) over x = r_out/r_in; report's Eq. 114 with its 1952 unit costs - re-derive with current prices and audit dimensions first (one continuous watt for 10 years = 87.66 kWh before duty factor)Source quote & editorial note
The costs which are affected are the combined costs of steel, copper, and energy.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 30-32
Editorial note, tabletop extrapolation: This collection's only explicit dollar-optimization of magnet proportions: redo the sweep with 2026 unit costs (scrap steel, surplus copper, $/kWh over expected machine life and duty cycle) - after re-reading the source for the variable definitions, since a cost formula reused without its unit system is a trap. NYO-780 p.8 did the equivalent sweep by model.
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Total magnet cost is a SLOWLY VARYING function of coil outside diameter near the minimum, so deliberately build the coils smaller than the computed optimum and buy operating convenience and gap access for almost nothing.
Source quote & editorial note
For operating convenience, the coils should be made smaller than is indicated because the total cost is a slowly varying function of the coil outside diameter near the minimum of cost.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 30
Editorial note, tabletop extrapolation: Licence to trade cost-optimality for access, cooling clearance, or stock material sizes - the optimum is a plateau, not a peak. How much plateau: evaluate the cost function at the smaller diameter and report the actual penalty rather than assuming it is a few percent. Same flat-minimum finding as NYO-780 p.8 (coil height); cite both.
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The unit costs that drive magnet optimization could, in the source's judgment, only be truly determined after years of operation - so the first-pass optimization uses estimates, and refining it beyond the accuracy of those inputs is wasted effort.
Source quote & editorial note
It appears that the unit costs can only be determined after the cyclotron has been in operation for several years, so estimates must be employed.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 30
Editorial note, tabletop extrapolation: A 1952 statement of the plan's own doctrine, applied with modern tools: use estimated lifecycle costs with a sensitivity check on the uncertain inputs, update from quotations and commissioning actuals as they arrive, and avoid polishing the spreadsheet past its input accuracy.
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Expect the analytically computed optimum coil OD/ID ratio to be biased HIGH - the source says its assumptions make the given x too large - and note the optimum is scale-dependent: do not copy another machine's coil proportions across a size class.
Source quote & editorial note
It is quite clear from either equation that this factor, optimum x, depends on scale factor. The assumptions made cause the value of x given by the equation to be too large.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 31
Editorial note, tabletop extrapolation: Two cautions in one: treat big-machine coil proportions (including TID-454's own x~1.4) as non-transferable to an 8-12 in machine, and rather than mechanically shaving the computed value, redo the optimization at the actual scale with a geometry-dependent field/cost model.
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One square centimeter of TRUE metallic contact distributed over a coil joint carries 10,000 A with negligible resistance and temperature rise - the report's point being that electrical capacity is rarely the binding constraint once real contact is achieved, mechanical strength is.
~10 kA per cm2 of metallic contact with negligible drop; joint requirement ~ mechanical strengthSource quote & editorial note
One square centimeter of metallic contact distributed over the joint will carry 10,000 amps with negligible resistance and temperature rise.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 32
Editorial note, tabletop extrapolation: Bolted bus laps at amateur coil currents have huge nominal margin by this figure - but nominal lap area is not metallic contact area: oxide, pressure, fastener relaxation and thermal cycling decide the real contact. Prepare surfaces, clamp hard, lock against loosening, then verify with a four-wire millivolt-drop measurement and a full-current temperature check. A joint that passes those two tests is electrically invisible; one that hasn't been tested is a fire waiting for a loose bolt.
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Match the DC supply to the magnet coil so that (maximum voltage)/(maximum current) equals the coil resistance; otherwise part of the supply's capability can never be delivered.
V_max/I_max = R_coil for full utilization of the supplySource quote & editorial note
The generator should match the coil in the sense that the quotient of the maximum voltage output and the maximum current should be equal to the resistance of the coil.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33
Editorial note, tabletop extrapolation: When sizing a surplus supply for the next machine's coil - or the turn count for a given supply - pick turns so the coil's HOT resistance sits at the supply's V_max/I_max corner: copper rises 20-40% in resistance from cold, so a cold-matched coil starves at temperature. And confirm the supply can actually hold its corner continuously; not every surplus unit can.
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Keep the magnetic circuit short with wide, thin yoke sections, and proportion coils so that (coil OD - coil ID) over the sum of both coil heights is about 1 - both statements 'useful only as guides' per the source's own caution.
(OD - ID)/(h_coil1 + h_coil2) ~ 1, i.e. 2*(r_out - r_in)/(h1 + h2) ~ 1 in radial terms; yoke sections wide and thin (guides, not optimization results)Source quote & editorial note
Both the above statements need qualification and are useful only as guides.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33
Editorial note, tabletop extrapolation: Quick shape checks for an H-frame rebuild - square-ish coil cross section and flat wide return yokes - with the author's own warning not to treat them as optimization results.
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Put the magnetically good steel where it counts: the pole base is flux-critical and its optimum cross-section 'rather critical' - found from B/(dB/dH) equal to a cost ratio, landing near B ~ 21,000 gauss for low-carbon steel in the worked case - while the yoke's steel QUALITY matters much less.
solve B_B/(dB_B/dH_B) = cost ratio (Eq. 123); worked case gives 8.3e3 Oe -> B ~ 21 kG pole base (p.35), ~18 kG horizontal yoke (p.36), low-carbon steelSource quote & editorial note
it should be made of magnetically good steel, and the optimum size is rather critical ... the quality of steel used in this part of the magnet [the yoke] is less important.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33-36
Editorial note, tabletop extrapolation: For a next machine's steel shopping: spend on clean low-carbon (1006/1008) pole and pole-base stock and size the pole base deliberately - it is the critical dimension - while the return yoke tolerates lower-grade steel. Lower-grade still means characterized enough to size its area with margin (dg-132's measure-or-assume-conservatively), not mystery plate on faith.
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There is an optimum operating field for a given beam energy (bigger magnet at low field vs smaller at high field); it follows from balancing the marginal cost of scale (C = C3*S^3 + C2*S^2 + C1*S + C0, with E ~ S^2) against the marginal cost of excitation - and it cannot be pinned down without a model magnet close to final form.
C = C3*S^3 + C2*S^2 + C1*S + C0; E = E'*S^2; optimum where d(cost)/d(energy) via scale equals d(cost)/d(energy) via field (Eqs. 137-145)Source quote & editorial note
This field strength depends on the design and the size of the magnet and cannot be determined without a model magnet.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33-38
Editorial note, tabletop extrapolation: The steel-vs-power tradeoff behind "how hard to push B" - for a fixed 757-lb-class magnet the answer comes off the real excitation curve, not theory; FEMM plays the role of the model magnet for first passes.
Cited in: Choosing Your Machine
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Measure field shape as a RATIO to the center-of-gap field - paired flip coils, null-balanced long-period galvanometer: in most cases the ratio is less sensitive to excitation current than the absolute value, so the required accuracy of current control is reduced.
null condition (Eq. 147) gives flux ratio from resistance ratios; flip-coil pair on a shaft rotating 180 deg avoids commutatorsSource quote & editorial note
In most cases, the ratio is not so sensitive to the current used to excite the magnet as the corresponding absolute value and the required accuracy of current control is reduced.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 38-40
Editorial note, tabletop extrapolation: The principle survives the instruments: when Hall-mapping a next machine's shims, log B(r)/B(0) with an always-live reference probe at center. Simultaneous ratioing cancels the common-mode excitation drift - saturation-driven profile changes, probe drift and cross-calibration error remain, so keep decent regulation and repeat-check a few points.
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Compute free-molecular conductance of long ducts of ANY cross section from S = 400*A^2/(O*L) liters/sec with A in in.2, O (perimeter) in inches, L in inches (air, ~300 K; exact constant 403). Circular-duct equivalent: S = 6.3e4*sqrt(T/273M)*D^3/L cm3/s.
S = 400*A^2/(O*L) l/s (A in in.2, O in., L in.; air 300 K; exact 403); S = 6.3e4* sqrt(T/(273*M))*D^3/L cm3/s for circular ducts (Eq. 40-41)Source quote & editorial note
S = 400 A^2/OL liters/sec ... For convenience of calculation the value 400 is used rather than 403; the results are hardly affected since the formula is only an approximation.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 144-145
Editorial note, tabletop extrapolation: The workhorse formula for long, odd-shaped passages in a cyclotron - annular gaps around the dee, slots, duct runs - where circular-tube handbook formulas fail. Its own conditions ride along: LONG ducts in molecular flow, and 'only an approximation' by the source's own words; short apertures, bends and abrupt area changes take end corrections or the orifice forms (dg-839), and a complex dee cavity is a network of elements, not one duct.
Cited in: The Vacuum Budget of a Cyclotron
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The A^2/OL duct formula underestimates rectangular-duct conductance: the corrected value is C = K * C_approx, with the report's Table 4.3 giving K = 1.108 to 1.444 as a/b runs 1 to 10 - equivalently, the uncorrected estimate sits 10-31% below the true conductance. The cited design deliberately omitted K to keep pump sizing conservative.
C_corr = K*C_approx; K(a/b): 1.108/1, 1.126/1.5, 1.151/2, 1.198/3, 1.297/5, 1.400/8, 1.444/10; percentages referenced to the corrected value: estimate low by (1 - 1/K) = 10-31%Source quote & editorial note
when applied to ducts of other than circular cross section, sizable errors may be introduced ... the correction factor K, by which the right side of Eq. 41 must be multiplied to give a more accurate value.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 145
Editorial note, tabletop extrapolation: The correction handbooks skip - and a margin policy worth copying with its limits understood: omitting K is a duct-conductance allowance, not a system margin. Effective speed obeys 1/S_eff = 1/S_pump + 1/C, so when the pump dominates, the extra conductance buys little; run the series combination before crediting headroom.
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For molecular-flow orifices use S = 75*A liters/sec (A in in.2) when the orifice is small relative to its surroundings, and S = 75*A*Abar/(Abar - A) when it is large (Abar = total duct area containing the orifice); combine elements as an electrical network, 1/S_tot = sum(1/S_i) in series, S_tot = sum(S_i) in parallel.
S_orifice = 75*A l/s (A in in.2, ~11.6 l/s/cm2 air); large orifice S = 75*A*Abar/(Abar-A) (Eq. 43-44); series 1/S = sum 1/S_i, parallel S = sum S_i (Eq. 45-46)Source quote & editorial note
For an orifice small relative to the area surrounding it, S = 75A. For an orifice large relative to the area surrounding it, S = 75A Abar/(Abar - A).
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 145
Editorial note, tabletop extrapolation: With the duct rule this covers most of a chamber conductance budget: baffle holes, dee mouths and constrictions become orifice or short-duct elements in a network. Finite-thickness holes transmit less than the zero-thickness 75A form - they are short ducts; interpolate or use transmission-probability tables - and series elements combine only approximately, so the budget is an estimate the pumpdown curve then checks.
Cited in: The Vacuum Budget of a Cyclotron
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Model the whole vacuum system as an electrical equivalent circuit - every duct, orifice and perforation a conductance (resistance = 1/S), combined in series/parallel down to a single effective speed AT THE LOCATION THAT MATTERS (inside the dee, where the beam and source live), not at the pump flange.
Source quote & editorial note
the term "resistance" is used there to indicate the reciprocal of the conductance. The use of resistance presents perhaps a clearer picture through the use of an electrical analog.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 132
Editorial note, tabletop extrapolation: The report's method in one sentence - their 32-in pumps' 13,700 l/s collapsed to 8,300 l/s effective inside the dee (air; the report's own worked numbers). The size of that collapse is the reason to budget from the source outward, not the pump inward - compute the conductance chain for the actual geometry rather than assuming any fixed fraction survives.
Cited in: The Vacuum Budget of a Cyclotron
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Give enclosed RF volumes their own analyzed pumping paths, in parallel with the dee-mouth opening - the source treats added openings at the dee as pumping speed in parallel with the mouth.
Source quote & editorial note
This additional pumping speed then can be considered as being in parallel with that through the opening at the mouth of the dee.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 129
Editorial note, tabletop extrapolation: Dees are pumping dead-ends by construction, and the ion source dumps its gas inside one: added holes in the dee back or stem shrouds are valuable conductance exactly there - size and place each pattern with an RF-current and field review, a structural check, and a molecular-flow conductance estimate; below-RF-significant hole size is the starting constraint, not the whole analysis.
Cited in: The Vacuum Budget of a Cyclotron
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Size high-vacuum pumps by THROUGHPUT at the operating chamber pressure, not by rated speed: tabulate Q = P_B * S_PB for each candidate against the system's effective conductance, and require margin over the known gas load for outgassing (virtual leaks) plus some real inleakage. Their comparison: 32-in pumps swallow ~2x the gas of 20-in at the same 1.15e-5 mm Hg chamber pressure.
Q = P_B*2S_PB = S_EL*(P - P_B) = S_net*P (Eq. 24); compare pumps by Q at equal chamber PSource quote & editorial note
Thus the 32-in. pumps will handle almost twice as much gas as the 20-in. pumps, and the decision to use 32-in. pumps is an obvious one.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 135-137
Editorial note, tabletop extrapolation: The right way to evaluate a diff-pump upgrade for a next machine - work in throughput (torr-l/s) at the pressure the source needs, with the MFC's known gas feed as the load, instead of comparing nameplate l/s.
Cited in: The Vacuum Budget of a Cyclotron
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Anchor the vacuum design to the ion-source gas load: their 200 ml/hr (NTP) maximum injection = 0.042 liter-mm/sec (~0.04 torr-l/s), which against the effective pumping speed set the achievable operating pressure of ~4e-6 mm Hg.
200 ml/hr NTP = 0.042 liter-mm/sec; P_operating = Q_source/S_effective + P_pumpSource quote & editorial note
If 200 ml/hr is considered as a maximum rate of gas injection, this results in ... 0.042 liter-mm/sec.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 136
Editorial note, tabletop extrapolation: The same arithmetic the builder runs with the MFC: a 0.1-1 sccm hydrogen feed is 1.3e-3 to 1.3e-2 torr-l/s; divide by the honest effective speed FOR HYDROGEN at the chamber, then add the pump ultimate and the outgassing floor, to predict running pressure before touching hardware. The formula assumes the source feed dominates the incremental load - the flow-on/off test verifies that (dg-370).
Cited in: The Vacuum Budget of a Cyclotron
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In molecular flow the same duct has sqrt(29/2) ~ 3.8x the conductance for H2 as for air - but in the cited pump-limited system this bought very little net speed, because the diffusion pump's hydrogen speed, not the ducts, was the bottleneck there.
S_H2/S_air = sqrt(M_air/M_H2) = sqrt(29/2) ~ 3.8 (conductances only)Source quote & editorial note
The fact that the conductances are considerably greater for hydrogen, therefore will have very little effect toward increasing the net speed in this region.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 138-139
Editorial note, tabletop extrapolation: Kills a tempting error for hydrogen-fed machines: do not credit the 3.8x conductance factor to the whole system. Check which element (duct or pump) limits for H2 specifically, using the selected pump's own hydrogen speed and compression data - pumps differ.
Cited in: The Vacuum Budget of a Cyclotron
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Bound pump-down expectations analytically before build: the report's 15,000-liter chamber computes to 30 min roughing (760 mm -> 45 microns) plus 3 min high-vac (45 microns -> 4e-6 mm), leak-free with outgassing neglected - real times are then dominated by outgassing, especially after venting.
t = (V/S)*ln(P1/P2) per stage; their case 15,000 l, 30 min rough + 3 min high-vacSource quote & editorial note
Neglecting outgassing and assuming a perfectly tight system, the pump-down times are as follow.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 139
Editorial note, tabletop extrapolation: The calculation pattern transfers to any chamber: compute t = (V/S)*ln(P1/P2) per stage with the pressure-appropriate effective speed (roughing pumps slow markedly with falling pressure, and series conductance caps S). When the observed pump-down runs many times the ideal, treat the excess as a prompt to check - outgassing, leaks, conductance restrictions, pump condition, gauge error - rather than as proof of any one of them.
Cited in: The Vacuum Budget of a Cyclotron
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Protect against pump-oil migration mechanically: a solenoid bleeder valve opens automatically when a mechanical pump shuts down, breaking the line vacuum so oil cannot back up the line.
Source quote & editorial note
opened automatically when the mechanical pump is shut down so as to break the vacuum in the line and prevent the pump oil from backing up the line.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 140
Editorial note, tabletop extrapolation: Transfers directly to a garage system: an automatic vent interlocked with the roughing pump - or a vacuum-rated anti-suckback valve, which is not the same thing as a generic check valve - prevents the classic oil-suckback chamber contamination. The source's practice of putting flexible connections in vertical runs (so oil cannot pool in them) is worth copying too - reported practice, scan re-read queued.
Cited in: The Vacuum Budget of a Cyclotron
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Give the vacuum system an automatic fault sequence keyed to forepressure interlocks (the source's settings: diffusion heaters off and high-vac valve closed at 50 microns forepressure, booster blocks at 160), with thermal switches on pump casings, and cross-connected backing lines normally valved off so any two surviving booster or backing pumps can back all three diffusion pumps - the source's two-of-three redundancy.
Source quote & editorial note
They permit, however, the backing of all three diffusion pumps by a combination of any two of the booster pumps, should any one of the booster or mechanical backing pumps become inoperative.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 140-142
Editorial note, tabletop extrapolation: Scales down to one gauge and two relays: a foreline-pressure interlock that kills the diff-pump heater and an over-temperature switch on its casing are the two automatics that protect an unattended amateur system's pump and oil - necessary automatics, not a complete unattended-operation case. Setpoints come from the pump's own tolerable forepressure, not the source's 50/160 microns.
Cited in: The Vacuum Budget of a Cyclotron
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Weld direct vacuum connections where practical; make demountable joints as welding-neck flanges with DOUBLE O-ring grooves in a standard flat-face flange and a pump-out port between the gaskets - permitting leak checking the joint and guarding the inner seal.
Source quote & editorial note
welding neck flanges with double O-ring gasket grooves machined in a standard flat face flange and provided with a pump-out connection between the two gaskets.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 141
Editorial note, tabletop extrapolation: The double-O-ring-with-interspace-pumpout trick is worth stealing for any large troublesome amateur flange (chamber lids especially): sniff the interspace for leak location, or hold it at rough vacuum to intercept most of the atmospheric load across the inner ring - it reduces, not nulls, permeation, since the elastomer still outgasses and a gradient to the chamber remains.
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The cited swept-RF system split its deflector trigger into two stages - a frequency-sensitive circuit that GATES and a phase-sensitive circuit that TRIGGERS - so a coarse condition opens the window and the RF itself supplies the firing phase.
Source quote & editorial note
The frequency-sensitive circuit "gates" the phase-sensitive circuit, and the phase-sensitive circuit triggers the deflector.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 168
Editorial note, tabletop extrapolation: The architecture for a timed kick against an extraction gap when frequency and phase are not derived coherently from one reference: coarse condition (frequency, turn count, integrated field) gates, RF phase triggers. A modern phase-coherent synthesizer can supply both from one reference - then a single measurement suffices.
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To detect when a swept RF reaches a chosen frequency, do not build a stable tunable RF filter - heterodyne the RF against a crystal local oscillator and detect the transient through a low-frequency band-pass filter, making the trigger point adjustable via the low-frequency side and crystal switching (the report used a 1-1.25 Mc filter with switched crystals to cover 19-21.5 Mc).
trigger when |f_dee - f_LO| = f_IF - BOTH sign branches respond, so the unwanted (image) crossing must be gated out or rejected; report's implementation: f_IF ~ 1-1.25 Mc, crystals switched across the bandSource quote & editorial note
Block 4 is a local oscillator with a frequency about 1 megacycle below the desired deflection frequency P. When the dee-oscillator signal sweeps through point P, the 1-megacycle filter passes an a-c transient.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 168-169
Editorial note, tabletop extrapolation: Classic measurement doctrine - move the precision problem to a low frequency where stability is cheap. A modern mix-down marker inherits the crystal's stability only for the LO term: the IF filter's center drift, bandwidth and threshold timing all enter the marker's error budget, so build that budget rather than expecting crystal accuracy from junk-box filters.
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The report's crystal oscillators held frequency within one part in 10,000, ovened at the crystals' turnover temperature; its frequency-critical discriminator elements shared controlled-temperature enclosure (oven contents and the 140 F setting report-attributed - scan re-read queued).
crystal at its own turnover temperature in an oven -> df/f ~ 1e-4 for the cited oscillators (turnover is device-specific)Source quote & editorial note
The crystal oscillators, Nos. 3 and 5, will maintain a constant frequency within one part in 10,000.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 169-170
Editorial note, tabletop extrapolation: The stabilization pattern transfers even where the parts are now silicon: put the reference AND the analog discrimination components in one controlled thermal box, because the filter drifting is as fatal as the oscillator drifting - then budget the whole chain (oscillator, filter, mixer, threshold) instead of assuming the oven number covers it.
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It is theoretically impossible to filter a transient without introducing time delay - so do not fight detection delay: the source kept it to a minimum and biased the trigger to fire earlier on the pulse rise.
Source quote & editorial note
Unfortunately it is theoretically impossible to filter a transient without introducing time delay. The time delay thus introduced was kept to a minimum.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 170-171
Editorial note, tabletop extrapolation: General fast-timing wisdom for beam-pulse and kick timing chains: every smoothing stage costs latency. Measure the chain's end-to-end latency and compensate the FIXED part in the trigger schedule or delay setting; threshold bias (the historical method) only advances the crossing for a given waveform - it walks with amplitude and slew rate, so calibrate it over the expected pulses.
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A swept signal peaks in a band-pass filter LATER than the moment it crosses the filter's center frequency - so trigger timing calibrated at one sweep rate silently moves when the sweep rate changes; the cited system provided a per-repetition-rate bias adjustment (reported detail, scan re-read queued).
peak delay depends on filter bandwidth and instantaneous df/dt of the sweep - characterize against the actual chirp rate and filter responseSource quote & editorial note
the time at which the transient is at a peak is somewhat later than the time at which the dee-oscillator frequency is in the center of the filter pass band.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 171-172
Editorial note, tabletop extrapolation: Matters wherever a resonant pickup watches a changing frequency - a synchrotron RF ramp or an FM-tuned marker on a cyclotron: if the ramp rate changes, re-characterize the timing rather than assuming the old calibration.
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Reference a trigger threshold to the MEASURED critical firing voltage of the actual trigger device: find the just-fires bias experimentally, lock it, and make compensating adjustments relative to that point.
Source quote & editorial note
the bias adjustment is made with reference to the actual critical firing voltage.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 172
Editorial note, tabletop extrapolation: A self-calibration idiom worth copying into any comparator/discriminator in the DAQ: trim to the observed threshold at session start (their multivibrator = today's comparator with drifting offset). That removes the threshold error present AT calibration - within-session drift, and aging that changes delay or hysteresis rather than threshold, still need periodic re-trim or monitoring.
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Gain-stabilize a sparse narrow-pulse chain with a PEAK-reading automatic level control - the cited circuit 'had to work on a peak-reading principle' because the tiny duty cycle starves an average-reading loop - and put its detector at the final trigger point so the loop spans every gain stage before it.
Source quote & editorial note
the automatic pulse-height circuit had to work on a peak-reading principle.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 171
Editorial note, tabletop extrapolation: Directly applicable to pulse chains fed by beam pickups or PMTs at low rep rate: stabilize on detected peak height at the discriminator input. This compensates multiplicative gain drift in the stages inside the loop and reduces amplitude-induced time walk - pulse-shape changes, baseline shifts and discriminator drift are outside it, so keep a timing calibration (or constant-fraction discrimination) as well.
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The cited system suppressed an unwanted (image) response by DISABLING the circuit during the time window where it occurred, rather than building sharp switchable filters - chosen precisely because high-frequency switching circuits invite unforeseen trouble.
Source quote & editorial note
That alternative was abandoned in view of the susceptibility of high-frequency switching circuits to unforeseen difficulties.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 172
Editorial note, tabletop extrapolation: A complexity-avoidance pattern with 2026 force - blanking a known-bad time window (one line of firmware now) - valid when no wanted events occur in the window and the gate acts early enough that the front end isn't overloaded by the artifact; otherwise the analog filtering earns its complexity.
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Benchmark for a home-built trigger discriminator, vacuum-tube era: the report's instrument fired with probable error under 1 microsecond over a 19-21.5 Mc range (its input/output/pulse specifications are the report's data tables - scan re-read queued for the exact values).
reported: probable firing-time error < 1 us; range 19-21.5 Mc, with provision for changing itSource quote & editorial note
Probable error in firing time, <1 microsecond. Range of firing frequency, 19 to 21-1/2 megacycles, with provision for changing this.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 174
Editorial note, tabletop extrapolation: Calibrates ambition - microsecond-class event timing off a small RF sample needed no exotic parts in 1952. A modern comparator-plus-MCU implementation should do well against that; measure its jitter rather than assuming orders of magnitude, and copy the architecture, not the hardware.
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For geometrically similar coils at fixed current density, field scales with linear size (h/(f*r0*j0) invariant, so H ~ r0), while power and conductor volume grow as r0^3; at fixed target field instead, power grows only ~linearly with r0.
h/(f*r0*j0) = design constant; at fixed j0: H ~ r0, P and V_conductor ~ r0^3; at fixed H: P ~ r0 (Eqs. 1-2)Source quote & editorial note
the field obtained is proportional to the inside radius of the coil and a high field can be obtained by increasing the scale ... the power p and the volume of conductor v increase with the cube of the inside radius.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 116
Editorial note, tabletop extrapolation: SCALE-SCOPED (megagauss-era context), and useful for estimating specific coils: it explains why small-bore air-core inserts and compact analyzing magnets are economically comfortable while large air-core fields carry punishing power bills - run the numbers for the actual coil rather than treating the scaling as a feasibility verdict.
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Match design effort to field class: the source says power and maximum current density 'become important factors and more complicated designs are useful' for fields of 1e5 gauss and above - elaborate minimum-power current distributions (j ~ sin(theta)/r^2 kernels) are particularly motivated in that regime. [Corrected 2026-08-23: earlier text inverted this into a claim that near 1 kG air-core coil power is small and optimisation 'seldom worthwhile', which the quote does not say.]
ideal minimum-power distribution: j = k*sin(theta)/r^2 inside boundary r^2 = k'*sin(theta) (Eqs. 3-4) - relevant only in the high-field regimeSource quote & editorial note
For fields of 10^5 gauss and above, the situation is quite different; the power and maximum current density become important factors and more complicated designs are useful.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 122
Editorial note, tabletop extrapolation: Locates amateur work far below the exotic regime: for sub-kG correction coils, steering windings and test solenoids a simple winding is usually adequate - but 'usually' is earned by computing NI, resistance, I^2R heating, temperature rise and current density for every coil, since a small high-duty coil can be power-limited at any field. [Note revised 2026-08-23: earlier note said 'sophistication buys nothing'.]
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Build and run a scale model of the RF system before committing to the full assembly: the report's 3/4-scale oscillator program delivered the dee-voltage-vs-frequency curve, the tuning-capacity range and drive-power data, and the quoted 27% efficiency measurement that changed the final design to six type-880 tubes while power-supply capacity allowed it.
model resonant frequencies ~ 1/scale (their 3/4-scale limits were 5% high for the scale factor used)Source quote & editorial note
The fairly low efficiency, 27 per cent, indicates that it would be desirable to go to six type-880 tubes in the final model, especially since power-supply capacity is available for the additional tubes.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 162
Editorial note, tabletop extrapolation: The transferable method rule - prototype the next machine's dee/stem/liner as a cheap scale model (or full-scale mockup, given the small size) and measure resonance, Q and parasitics before final fabrication; NYO-780 p.29ff records the same practice. Cite both.
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Hunt parasitic RF modes early and kill them selectively: the report identified an unwanted ~50 Mc mode on its three-quarter-scale model - the oscillator stub forming a capacity-loaded half-wave line - and loaded it with a small coupling loop tuned to the parasite.
Source quote & editorial note
equipped with a small coupling loop ... used to load the unwanted mode, which on the three-fourths scale model was about 50 megacycles, in which the oscillator stub forms a capacity-loaded half-wavelength line.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 162
Editorial note, tabletop extrapolation: Both steps are amateur-accessible: find candidate modes cheaply (a scale model or a bench sweep of the real resonator), then load the parasite selectively into a lossy element that leaves the wanted mode alone. Scaling shifts parasitic frequencies, and the final amplifier's loading shifts them again - so verify and re-suppress on the fully assembled system; that matters the moment the LDMOS upgrade raises the reference machine's gap voltages.
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For a uniform field from a split coil pair at high field, the source's criticism is that thin-winding Helmholtz sections (cross section small next to radius squared) require excessive power; its doctrine is to set uniformity by a power-series expansion of the mid-plane field, choosing coil boundaries to null low-order terms rather than simply making the coils huge.
expand H(u) in powers of u in the mid-plane (Eqs. 1-3) and null low-order derivative terms by choice of coil boundary; thick sections (cross section ~ a^2) for power economySource quote & editorial note
Helmholtz coils have cross sections small in comparison with their radii squared, and thus require excessive power where a high field is required.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 108
Editorial note, tabletop extrapolation: The right doctrine for any air-core uniform-field fixture - probe-calibration coils, a beamline corrector, a small synchrotron's reference field: choose the winding section from the ampere-turns, resistance, I^2R and temperature-rise arithmetic, and reach for thick optimized sections when that arithmetic shows a power problem - a classic thin Helmholtz pair is fine where it doesn't.
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Derive an FM (frequency-vs-time) program from the constant-ion-phase condition and measured oscillator data rather than seeking an exact law - in the cited synchrocyclotron design, the required capacity-vs-time variation was 'not very critical'; and cycle dead time taxes average beam current directly, so minimize the return-to-start time.
df/dt from constant-phase relation integrated numerically against measured f-vs-C of the model oscillator (Eqs. 1-3); t_return <= t_accel for best duty cycleSource quote & editorial note
The operation of the oscillator determines the variation of capacity with time which will keep the ion phase constant. This variation is not very critical.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 152
Editorial note, tabletop extrapolation: For a small synchrotron's RF ramp the pattern maps with its own tolerances: f(t) and the allowable phase/frequency error come from the magnetic ramp, synchronous orbit and RF-bucket acceptance - the cited looseness belongs to that FM oscillator, not to synchrotron ramps in general; the duty-factor lesson (reset time is pure tax, minimize it within hardware limits) transfers as stated.
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Treat construction-material choice as a radiological design decision made at the drawing board, not a retrofit; where activation channels are open, prefer aluminum for in-beam and near-beam structures and minimize stainless steel.
Source quote & editorial note
a careful choice of materials of construction, for example, using as much aluminum as possible and very little stainless steel, should reduce the radiation problem significantly.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 18
Editorial note, tabletop extrapolation: ENERGY SCOPE: a 730-MeV machine's recommendation. At the reference machine's sub-MeV proton operation the spallation and (p,xn) channels behind it are closed, so bulk structural activation does not drive material choice at that scale - with the standing exceptions: thresholdless capture on some nuclides, light-element targets, and any deuteron operation. The drawing-board principle bites the moment a machine crosses into open-channel territory.
Cited in: Shielding a Small Cyclotron
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Different structural metals leave different residual-nuclide inventories under the same irradiation - the report's survey at its energy: aluminum yielded no long-lived activities they detected, iron essentially pure 300-day Mn54, stainless adds 27-day Cr51 and 71-day Co58 from its Cr and Ni, copper gives 12.8-hr Cu64 and Co58.
long-lived residuals at 730 MeV: Al -> none; Fe -> Mn54; SS(10%Ni,20%Cr) -> Mn54 + Cr51 + Co58; Cu -> Co58; yield ratio Cu64/Na24 ~ 50/1 (factor ~2)Source quote & editorial note
Aluminum yields no long-lived activities, while Co58 is produced from copper ... Stainless steel produces two long-lived isotopes, Co58 and Mn54, while only Mn54 is induced in iron.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 18
Editorial note, tabletop extrapolation: ENERGY SCOPE: nuclide-by-material bookkeeping from 730-MeV spallation; these channels are closed at sub-MeV proton energy. The durable pattern is inventory-follows-alloy-content (Ni -> Co58, Cr -> Cr51) - worth knowing when reading other labs' surveys. The report's list is what their instruments saw, not an exhaustive table: modern data adds Be-7 and Na-22 from high-energy aluminum, so treat any such inventory as survey-specific.
Cited in: Shielding a Small Cyclotron
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To learn what a machine activates, hang cheap witness foils of candidate materials (Al, Cu, Fe, stainless) at mapped positions before a run, then identify each induced activity by its gamma-ray energy AND its half-life from repeated NaI counts.
Source quote & editorial note
foils of aluminum, copper, iron, and stainless steel were affixed at various positions on the walls of the cyclotron vault and on the cyclotron vacuum tank.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 15
Editorial note, tabletop extrapolation: The one activation rule that applies at any energy, because it is a measurement, not a prediction: a witness-foil pack plus the next machine's NaI/PIPS counters is a near-zero-cost check. Read a null correctly - it bounds what those foils, positions, counting and cooling times could detect; strong practical evidence, not proof that nothing anywhere activated. Useful for licensing conversations and for catching surprises if beam or species ever changes.
Cited in: Shielding a Small Cyclotron
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Wrap one of a matched foil pair in cadmium to split induced activity into a slow-neutron capture part and a fast-particle part; at the 184-inch the Cd-wrapped (fast-only) copper foil showed ~1/1.6 of the bare foil's Cu64.
Cu64(Cd-wrapped)/Cu64(bare) ~ 1/1.6, i.e. ~40% of activation was thermal-neutron captureSource quote & editorial note
the ratio of Cu64 activity in the cadmium-wrapped sample (due only to fast particles) to that in the uncovered foil was ~1/1.6.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 15
Editorial note, tabletop extrapolation: ENERGY SCOPE: relevant only when neutrons exist to be moderated. The Cd-difference technique splits capture activation into below- and above-cutoff parts APPROXIMATELY - epithermal response and the wrapper's spectrum perturbation blur the split, which is why practice reports cadmium ratios rather than clean fractions. Keep it in the toolkit for any future neutron-producing experiment; meaningless for pure sub-MeV proton running.
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Size gamma shielding from the measured line energies, not worst case: for the ~510-810 keV residual-activity lines, lead half-thickness is 0.6 cm (2 cm buys 10x) and concrete 4 cm; small portable and permanent shadow shields then give safe access to key service points (valves, ion source, rf).
HVL(Pb, 0.5-0.8 MeV gamma) = 0.6 cm; 2 cm Pb = 10x attenuation; 6 cm Pb shadow shield: 100 r/hr -> 100 mr/hr; HVL(concrete) = 4 cmSource quote & editorial note
To reduce the radiation by an order of magnitude one needs only 2 cm of lead - an amount that can readily be made into a portable shield. Shadow shields of 6 cm of lead would reduce even the 100 r/hr radiation field to a quite tolerable 100 mr/hr. The same radiation has a half-thickness of 4 cm for concrete.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 18
Editorial note, tabletop extrapolation: ENERGY SCOPE: a sub-MeV machine on ordinary structural materials produces no comparable residual gamma fields (light-element targets, thresholdless capture and deuteron operation are the exceptions - see the safety pages). The transferable part is the sizing discipline: identify the actual photon energy first, then buy attenuation in half-thickness units - the same arithmetic sizes the lead around a NaI detector against room background. Note the report's own arithmetic: even 6 cm of lead leaves 100 mr/hr from a 100 r/hr field - reduced is not zero.
Cited in: Shielding a Small Cyclotron
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Localize an activation (or any radiation) source with a collimated NaI detector — crystal in a lead pig with a plugged hole for background — and compare aimed vs background spectra; at the 184-inch this proved the gap structures, not the magnet yoke, were the source.
Source quote & editorial note
the important source of radiation in the cyclotron comes from the gap and the structures in it, rather than from neutron-induced activities in the magnet yoke.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 12
Editorial note, tabletop extrapolation: An energy-APPROPRIATE technique: a lead collimator with a removable plug around a next machine's NaI turns it into a pointing instrument for X-ray leak hunting (RF multipactor sites, dee-liner discharge bremsstrahlung) on a running machine. Choose wall thickness for the photon energies in play - soft dee X-rays need little lead; harder sources need more, plus attention to fluorescence and off-axis penetration. The aimed-vs-plugged comparison is the transferable discipline.
Cited in: Shielding a Small Cyclotron
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Put a permanent wide-range dose-rate meter as close to the target station as it can live, read out on a chart at the console, and let the measured decay curve — not habit or guesswork — set the cooling time before anyone approaches.
Source quote & editorial note
use of a reliable radiation meter in the cyclotron near the targets ... takes much of the guesswork out of the question "How long should the target cool?"
McWalters et al., Radiation Exposures of Personnel at the 60-inch Cyclotron — UCRL-8276 (1958) — p. 16
Editorial note, tabletop extrapolation: ENERGY SCOPE: Crocker's 10-24 MeV/nucleon beams at tens of uA made 100-500 r/hr targets; a sub-MeV proton machine on ordinary targets produces no comparable residual source term (light-element targets and deuteron operation are the exceptions). The instrument discipline transfers exactly: a logged dose-rate channel at the machine - an instrument whose response covers soft X-rays (dg-559) - gives prompt X-ray dose during RF conditioning and a defensible record alongside the beam-current log.
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Treat handling time as a primary dose control and choreograph it - the report's crew worked to rehearsed routines (their figures: target setup ~3 min, removal ~1 min, dismantling under 1 min behind a 2-in lead-glass bench shield), and average exposure fell from 0.165 to 0.1 r/man/week between 1953-56 and 1957 while target changes exceeded a thousand.
dose = rate x time; Crocker trend 0.165 -> 0.1 r/man/week (1953-57) despite >1000 target changes in 1957Source quote & editorial note
Time is one of the most important factors in the amount of radiation received, and familiarity with the targets added to the speed of target setups and disassemblies
McWalters et al., Radiation Exposures of Personnel at the 60-inch Cyclotron — UCRL-8276 (1958) — p. 16
Editorial note, tabletop extrapolation: The practice - rehearse any hands-on task near a radiation hazard until it is quick and sure, and put a bench shield where hot items are worked - is the cheapest safety hardware there is, because dose = rate x time. Do not transfer speed to electrical work: HV and RF tasks are controlled by de-energizing, verifying zero and lockout (dg-522), where hurrying adds risk rather than removing it.
Cited in: Shielding a Small Cyclotron
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In target-handling work the hands take roughly ten times the whole-body dose, so extremity monitoring (finger films/rings) and tools that add inches of distance matter more than badge numbers suggest.
extremity dose ~ 10x whole-body dose for target setup/dismantlingSource quote & editorial note
Finger films show that the hands receive about ten times as much exposure as the body for target operations; i.e., setting up and dismantling.
McWalters et al., Radiation Exposures of Personnel at the 60-inch Cyclotron — UCRL-8276 (1958) — p. 16
Editorial note, tabletop extrapolation: ENERGY SCOPE: measured on multi-MeV activated targets. The geometry lesson transfers: the hands work closest to the source, where rates are highest (inverse-square for a compact source, and higher still in contact geometry, where the simple 1/r^2 picture breaks down) - so tongs that add inches and a ring dosimeter are the response if the machine ever handles activated or tritiated items. For energized circuits the analogue is distance by design - insulated tools and clearances - not speed (dg-871).
Cited in: Shielding a Small Cyclotron
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Quarantine the operations that activate the machine hardest (at Crocker, deuteron runs) into scheduled windows — end of week, mandated 25-30 min cooling, longer for prolonged runs — so the activation decays over the idle period instead of irradiating the next shift.
Source quote & editorial note
They are run only on Friday evenings and Saturday, and - if demands are high - on Sundays. For these bombardments a longer cooling time is required. A nominal time of 25 to 30 minutes is set
McWalters et al., Radiation Exposures of Personnel at the 60-inch Cyclotron — UCRL-8276 (1958) — p. 10
Editorial note, tabletop extrapolation: ENERGY SCOPE: Crocker's figures are (d,n) activation at tens of uA and ~20 MeV. Sub-MeV deuterons still make neutrons - D(d,n)3He and 9Be(d,n) are exothermic - so the analogue exists the day deuterium enters the machine (dg-121, dg-545). The scheduling pattern transfers either way: batch the nastiest operations (HV conditioning, any future deuteron or neutron work) into planned windows with a defined stand-down, rather than interleaving them with routine bench time.
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Expect the internal, in-vacuum components that the beam actually strikes to be the hottest objects in the report's accounting - a probe target may emit more than 10,000 r/hr, against the report's ~500 r/hr for the deflector and 100-500 r/hr for external targets at 5 minutes - and design their removal paths and storage shielding first.
internal probe target and exit strip: ~10,000 r/hr; deflector: ~500 r/hr; external targets 100-500 r/hr at 5 minSource quote & editorial note
An internal target (one that has been inserted into the tank on a probe) may emit more than 10,000 r/hr.
McWalters et al., Radiation Exposures of Personnel at the 60-inch Cyclotron — UCRL-8276 (1958) — p. 10
Editorial note, tabletop extrapolation: ENERGY SCOPE: these are 10-24 MeV activation levels. The design ordering survives: whatever intercepts full beam (probe tip, Faraday cup, target holder) concentrates the consequences. On a sub-MeV machine that is heat and sputtering today - and activation joins the list via thresholdless capture on some materials, light-element targets, or any deuteron operation, growing first at these same components if energy climbs.
Cited in: Shielding a Small Cyclotron
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Evaporate boron from a COVERED slotted boat machined from spectroscopic-grade carbon rod; the cover both cuts radiative heat loss (boron needs white heat) and stops the charge scattering out of the boat during heating.
boat from 5/16-in dia spectroscopic carbon rod, covered cavity (No. 1 drill, 0.228 in), charge ~250 mg amorphous boron powderSource quote & editorial note
It was found necessary, however, to use a covered carbon boat both to reduce the radiation cooling of the boron and to prevent scattering of the material during the heating.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 6
Editorial note, tabletop extrapolation: Boron is among the worst common elements to evaporate - it runs at white heat and attacks refractory-metal boats - and carbon-rod stock is cheap and machinable with ordinary tooling, so this is the boat design to copy for B-11 films. The recipe handles the isotope like any boron; the TARGET still needs its own qualification: verify enrichment survives the process, check carbon/carbide pickup, and measure uniformity and areal density before calling it experiment-ready.
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Working boron-evaporation parameters: pressure below 1e-5 mm Hg, ~280 A at 8 V (~2.2 kW) through the carbon boat to white heat, deposition onto 3.25 x 4-in glass plates; endpoint is visual — the charge stays darker than the boat until just before vaporizing, then brightens and disappears in seconds.
P < 1e-5 mm Hg; I ~ 280 A @ 8 V; T = white heat; substrate = cleaned glassSource quote & editorial note
Pressure was maintained below 1 x 10-5 mm of Hg while the boat was being brought to temperature. Then, by passing a current of about 280 amp at 8 volts through the boat, a sufficiently high temperature was reached (white heat) to vaporize the boron. The progress of the evaporation was followed by observing the material as it heated in the boat. The boron remained darker than the boat until just before vaporization, then it became bright and quickly disappeared. The boron was evaporated onto 3 1/4 x 4-in. glass plates.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 6
Editorial note, tabletop extrapolation: Scope honestly: this is EVAPORATION producing ug/cm2-class self-supported films - potentially suitable for a p+B11 cross-section or resonance-yield measurement once areal density, uniformity and purity are characterized - and NOT the route to a thick target for a maximum-alpha-yield demo. The hardware (2.2 kW low-voltage supply, 1e-5 torr bell jar) is within amateur reach ONLY with the engineering done: rated water-cooled feedthroughs for 280 A, fault protection, implosion screening, and hot-material handling.
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Budget boron-evaporation boats as consumables in the cited (carbon-boat, slotted) apparatus: hot boron converts the carbon boat to boron carbide, the slot clogs, and a boat survives at most two evaporations - so machine boats in batches before a target campaign.
cited apparatus: boat life <= 2 evaporations (B4C slot clogging; carbon boats)Source quote & editorial note
The boats are useful for only two evaporations at most since the slot rapidly becomes clogged with boron carbide.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 6
Editorial note, tabletop extrapolation: Plan an enriched-B11 evaporation campaign around several pre-machined spare boats rather than debugging mid-run. The failure mode is the carbon: refractory-metal boats, compatible crucibles or non-contact heating change or avoid it - candidate fixes to compatibility-test, not guarantees.
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Recover self-supported films by float-off: pre-clean the glass in Calgonite (detergent) solution, tilt ~20 deg, run warm tap water in slowly, cut the floating film to size, and lift it on 0.030-in aluminum frames; add a pinch of detergent to cut surface tension and pause before lifting clear so trapped water drains.
Source quote & editorial note
the method found successful here was to float the boron off the plate with warm tap water. Prior to evaporation the plate was cleaned by washing in a Calgonite solution and rinsed with water. The plates were placed at an angle of about 20 deg to the horizontal and water was allowed to run in slowly. The floating film was then cut into appropriate sizes, and the pieces were picked up on square target frames of aluminum 0.030 in. thick. ... breakage of films can be greatly reduced by adding a pinch of detergent, such as Calgonite, to the water to reduce surface tension just before the film is picked up, and also by stopping just before removing the frame from the water to allow trapped water to drain off.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 6
Editorial note, tabletop extrapolation: The film-recovery toolchain is modest (named detergent, tap water, glass plates) and the skill is in the sequence - which the card now quotes in full. Use the source's Calgonite or a validated low-residue lab surfactant rather than assuming any modern dishwasher detergent is equivalent. Practice on natural boron before spending enriched B-11.
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When a single-thickness film is too fragile, bring the frame up under the middle of the floating film so it folds double over the frame and the two layers adhere — Hoke and Newman's double 50-100 ug/cm2 enriched-B10 targets were far easier to make than single 25-50 films.
double-fold pickup; B10 double films 50-100 ug/cm2; carbon precedent 25-100 ug/cm2Source quote & editorial note
Stronger double films, which proved to be much easier to make, were made by bringing the frame up in the middle of the film. The film then folded over the frame
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 8
Editorial note, tabletop extrapolation: For a next machine's B11(p,alpha) internal-target work, the double-fold film is the mechanically survivable construction - but qualify its thickness against the experiment's energy budget with current stopping data: compute the proton energy loss and straggling through the actual post-fold areal density with PSTAR/SRIM at the actual beam energy before calling it thin enough for resonance-tail work (at ~170 keV the loss through these films is substantial, not negligible).
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For water-sensitive evaporated films (e.g. magnesium), first arc-coat the soap-primed glass with 5-10 ug/cm2 of carbon as a parting and backing layer, and ramp evaporator current slowly (10-20 min) so the charge outgasses quietly instead of spattering; conserve enriched isotope with a glass recovery hood over the source.
Mg: 3-mil Ta boat, ~3/4-in wide, P < 2e-5 mm Hg, I -> ~100 A over 10-20 min; C parting layer 5-10 ug/cm2; films 30-80 ug/cm2Source quote & editorial note
For the evaporation of magnesium, boats of 3-mil tantalum about 3/4-in. wide were used. The pressure was maintained below 2 x 10-5 mm of Hg, and the current was increased to about 100 amperes. The scattering of the MgO by violent outgassing can be minimized by increasing the current slowly over a period of 10 to 20 minutes so that the outgassing can occur quietly. ... the glass was coated with a weak soap solution (Calgonite) and allowed to dry before it was coated with about 5 to 10 ug/cm2 of carbon from an arc ... One function of the carbon layer is to help keep the magnesium from making contact with the water; magnesium is slightly soluble in water and decomposes to form Mg(OH)2. The carbon also helps hold the magnesium film together both while it is being removed from the glass and afterwards. ... a glass hood was constructed from lantern slide covers so that all of the collected material could be recovered.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 9
Editorial note, tabletop extrapolation: Three tricks generalizable WITH per-material validation: sacrificial arc-carbon parting layers under fragile or water-reactive films (validate compatibility - carbon can add reaction background or stick badly to another material), slow-ramp outgassing before full evaporation power, and a cheap glass recovery hood (lantern-slide covers) so enriched material can be recovered - recovered stock needs a purity check before reuse.
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Never quote an internal-target beam energy from the B-rho calculation alone: ORNL's 86-inch measurements indicated the proton energy might deviate as much as +/-10% from the H-rho value, and the energy of maximum intensity varied by several hundred keV under MINOR adjustments of ion-source position, dee voltage, magnetic-field tuning, and oscillator frequency.
observed: E(measured) - E(B-rho) up to +/-10%; dE(max intensity) ~ several hundred keV vs everyday tuning parametersSource quote & editorial note
Measurements of the internal beam of the ORNL 86-inch cyclotron very early indicated that the energy of the proton beam might vary as much as +/-10% from H-rho calculations. ... The energy of maximum intensity was found to vary by as much as several hundred kilovolts with minor adjustments of the ion source position, dee voltage, magnetic field tuning, and oscillator frequency.
Editorial note, tabletop extrapolation: The direct historical support for this collection's energy-convention discipline: the reference machine's '150 keV-class computed' is a convention, not a measurement, and its own discrepancy must be measured, not assigned ORNL's +/-10%. For a next machine's B11(p,alpha) work, where yield vs energy is steep, measure energy AT the target (absorber stack in front of the PIPS, or foil methods) every time tuning changes.
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Measure internal-beam energy with photographic film behind a stepped absorber folded from aluminum foil: expose briefly at throttled intensity (the report ran arc off, controlling current from the source, with the field deliberately detuned), leave an uncovered film strip as an intensity reference, and read densitometer values against a range-energy scale.
exposure ~0.1 uA-sec (Weston Speed 5 film); absorber = folded Al foil steps; monitor = neutron counter near targetSource quote & editorial note
A photographic film is covered with a stepped absorber (made by folding an aluminum foil), wrapped in aluminum foil, and exposed directly in the cyclotron beam.
Editorial note, tabletop extrapolation: At 150-170 keV the material budget dominates everything: compute proton range and straggling with PSTAR/SRIM through the CUMULATIVE areal density - wrapping foil, absorber steps, emulsion overcoat, detector dead layer - before trusting any variant, since micron-scale layers can stop such protons outright. The architecture transfers (stepped degrader + position-resolved readout + reference channel), but an ordinary PIPS is a single channel: use per-step exposures, a scanned detector, or a segmented one, and establish low-current operation for the actual ion source rather than assuming the arc-off trick.
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Know the accuracy floor of the cited absorber-based measurement: range-energy data and straggling limited the most-probable-energy determination to a few hundred keV, with the high-energy portion nearly as good, and the low-energy portion involving considerably greater uncertainty.
Source quote & editorial note
These factors limit the accuracy of determination of the most probable energy to a few hundred kilovolts. The high energy portion of the energy distribution can be determined with almost equivalent accuracy
Editorial note, tabletop extrapolation: The asymmetry - high-energy side of an absorber spectrum better determined than the low-energy tail - is the shape to remember, but the historical few-hundred-keV floor belongs to that apparatus: for a PIPS-plus-degrader setup, build the detector-and-degrader response matrix and quote separate uncertainties for mode, upper edge and tail rather than scaling ORNL's numbers.
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Turn a known activation excitation function into a beam spectrometer: bombard a stack of thin foils whose reaction is well measured, count each foil, and unfold activity-vs-depth into the energy spectrum - the steeply falling cross section makes the discretized system near-triangular, solvable foil by foil (stack details report-attributed; scan re-read queued).
A(r) ~ integral over R of sigma(R-r)*I(R) dR, discretized as block/line spectrum -> near-triangular linear system; choose Rn spacing to avoid oscillating/negative weightsSource quote & editorial note
the energy distribution of protons in the cyclotron beam is readily determined by measuring this excitation function and comparing it with the published data.
Editorial note, tabletop extrapolation: ENERGY SCOPE: Cu63(p,n)Zn63 needs ~4.2 MeV (verify against evaluated data at use time) - closed at reference-machine energies. What transfers is narrower than the note once claimed: the unfolding needs multiple independent response kernels, so a single B11(p,alpha) yield number constrains but cannot recover a spectrum; measurements at several calibrated degrader settings can build a response matrix, and a PIPS behind degraders is range spectrometry - a different, complementary method.
Cited in: Shielding a Small Cyclotron
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Distrust beam diagnostics taken with the machine deliberately detuned to reach diagnostic-friendly intensity — the operating conditions differ enough from normal running that the measured energy distribution may not be the operating one; state the caveat with the result.
Source quote & editorial note
the cyclotron operating conditions are so different from those used in normal operation that it may well be that the energy distribution is not the same.
Editorial note, tabletop extrapolation: Methodological honesty that transfers directly: IF detector protection forces attenuated or otherwise-configured beams for a measurement, log the machine state (dee voltage, field, frequency, source position, attenuation method) alongside every energy measurement so diagnostic-mode and run-mode data are never silently mixed - attenuation need not mean detuning, so record what actually changed.
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Map the beam on an internal target by sectioning the target itself: an array of thin strips (17 carbon foils, 1/32 x 5.5 in), pre-scored, bombarded once (15 min at 15 uA), then snapped into 1/2-in pieces and counted individually — yielding full 2-D isointensity contours of the beam spot from a single bombardment.
activity map via C12(p,pn)C11 (20-min) + long-lived impurities, cross-checked; resolution = section size (0.5 in) x strip pitchSource quote & editorial note
each carbon foil was broken into 1/2-inch sections, along previously made scorings, and counted in a Geiger counter.
Cohen, Spatial Distribution of Current on an Internal Cyclotron Target — ORNL-1348 (1952) — p. 5
Editorial note, tabletop extrapolation: ENERGY SCOPE: C12(p,pn) needs ~20 MeV, so the activation readout is closed at tabletop energies. Keep the geometry, swap the readout - a probe-tip mosaic of insulated segments read as Faraday collectors gives a one-shot 2-D map IF built properly (guarded insulation, secondary-electron suppression, RF isolation, calibrated electrometers); a witness material (film, phosphor) needs calibrating at the actual energy, spot size and vacuum before its image is trusted. Either way the map decides where the B11 target goes and how big its hot spot runs.
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The turn-to-turn radial step at the target edge is a direct RF-phase meter: from dE/E = 2 dr/r and dE = 4 V0 cos(theta) per turn (two dees), a measured dr at known radius, energy, and dee voltage yields the ion phase — ORNL 86-inch values ran 50-72 deg for 240-335 kV dee-to-dee.
dE/E = 2*dr/r (nonrelativistic, E ~ r^2); per turn with two dees dE = 4*q*V0*cos(theta) = 2*q*Vdd*cos(theta) (V0 = peak dee-to-ground, Vdd = peak dee-to-dee) => theta = acos(E*dr/(2*q*r*V0)) = acos(E*dr/(q*r*Vdd)); source table (dr in, Vdd kV, theta deg): A(0.29, 315, 60), B(0.19, 315, 72), C(0.22, 240, 60), D(0.40, 335, 50)Source quote & editorial note
From (5) the measurement of dr is essentially a determination of the phase.
Cohen, Spatial Distribution of Current on an Internal Cyclotron Target — ORNL-1348 (1952) — p. 9
Editorial note, tabletop extrapolation: Energy-independent physics: a differential probe (shadowed double tip) or the sectioned-target map gives dr, and with the dee voltage - stated in ONE convention, peak dee-to-dee or dee-to-ground, never mixed - that is a direct measurement of ion RF phase, the quantity a next machine's field-tolerance budget protects. A rare experimental handle on phase for machines with no beam-position monitors.
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Control the ion-source ground connection deliberately: an ungrounded source floats toward the accelerating-slit (dee) potential, reducing the slit's effect - ORNL's measured radial widths then approached the no-slit theoretical predictions. A floating source is a different machine configuration, not a small perturbation.
Source quote & editorial note
leaving the ion source ungrounded has a very substantial effect, since it then floats nearer the potential of the accelerating slit which is attached to the dees. This reduces the effect of the latter and the radial width approaches the theoretical predictions for a cyclotron without an accelerating slit.
Cohen, Spatial Distribution of Current on an Internal Cyclotron Target — ORNL-1348 (1952) — p. 9
Editorial note, tabletop extrapolation: Direct lesson for the reference machine's central-region debugging: the source body's electrical state - DC connection AND RF return impedance, since a floating body near driven dees picks up RF capacitively - is a real optics knob (or a real gremlin). Verify and log the filament/chimney ground path; an intermittent source ground would masquerade as day-to-day beam irreproducibility of exactly the kind ORNL-1347 warns about.
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Expect the surviving beam to self-select its RF phase: detuning the 86-inch field by 0.4% should have shifted the final phase 45 deg, but the measured shift was only ~10 deg because ions at the resonant phase were lost to defocusing and ions of more favorable phase became the dominant current — the machine partially hides detuning from you.
predicted d(theta) = 0.004 x 360 deg x N_turns (= 45 deg for these conditions); observed ~10 degSource quote & editorial note
the ions which were the chief contributors to the current at resonance are lost by defocusing and ions of more positive phases are now the chief contributors.
Cohen, Spatial Distribution of Current on an Internal Cyclotron Target — ORNL-1348 (1952) — p. 9
Editorial note, tabletop extrapolation: Explains an observation class on the reference machine: probe current can look tolerant of field/frequency error while the surviving phase distribution, turn spacing, transmission and attained radius shift underneath - reinforcing ORNL-1347's rule that current on target is not evidence the energy is what B-rho says (at a FIXED radius the momentum is still ~qBr; what moves is which ions get there and how). Whether self-selection broadens your tuning curves is testable with phase- or energy-sensitive measurements - treat the width cautiously either way.
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Set beam energy as an explicit compromise among cost, the physics value of higher energy, and the fraction of beam you can extract - the source's three axes; current they set separately, from what the research program needed.
Source quote & editorial note
The beam energy is really a three way compromise between cost, the advantages of higher energy, and the ability to extract a large fraction of the beam.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 20
Editorial note, tabletop extrapolation: Directly transferable process rule (their answer, 810 MeV / 100 uA, is not): write down the compromise axes for a next machine's energy point instead of inheriting a number.
Cited in: Choosing Your Machine
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State the hard requirements first (for a magnet: isochronous average field, adequate focusing, achievable power), then weigh remaining configurations against soft criteria like cost, ease of extraction, and maintenance.
Source quote & editorial note
Beyond these requirements the advantages and disadvantages of various magnet configurations that might be used become more subtle and must be weighed against such factors as the cost, ease of beam extraction, and maintenance requirements.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 162
Editorial note, tabletop extrapolation: Scale-free requirements-hierarchy discipline - with the hard-requirements LIST being machine-specific: for a classical weak-focusing machine it is the field law (falling field, n inside its stable band), focusing, and achievable power; isochronism is the AVF machine's version, and a synchrocyclotron's differs again. State yours first, then trade the soft criteria as the source does.
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A risk-retiring model's charter, in the source's words: examine practicability, reveal any unexpected phenomena, and demonstrate the feasibility of the riskiest subsystem - the purposes their electron analogue was conceived for.
Source quote & editorial note
conceived as an experimental device to examine the practicability of isochronous acceleration ... to reveal any unexpected phenomena ... and finally, to demonstrate the feasibility of a high efficiency beam extraction system.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 263
Editorial note, tabletop extrapolation: The three-purpose charter is scale-free for any model or prototype a program chooses to build; whether to build one at all is a cost-versus-risk call - FEMM plus the tracker is the tabletop program's cheap analogue. The keV-electron stand-in trick itself needs more than matched T/mc^2 to be faithful (rigidity and geometry must scale together).
Cited in: Choosing Your Machine
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When rejecting alternatives in a trade study, name each one's defects - the source's own practice in the quoted line: 'all suffer from one or more of the following defects', followed by the list.
Source quote & editorial note
All suffer from one or more of the following defects: excessive space requirements, lack of terminal space, lack of terminal auxiliary power, and lack of flexibility for future uses.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 149
Editorial note, tabletop extrapolation: Their injector shoot-out (tandem vs open-terminal vs pressurized vs Van de Graaff) models the documentation style for any subsystem selection in mark2_design_notes open decisions.
Cited in: Choosing Your Machine
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Choose sector number from the essential-resonance structure of the tune range you must traverse, then break ties with RF symmetry (how many accelerating gaps the geometry naturally supports).
systematic (structure) resonances: a*vr + b*vz = p*N for integer p (p = 1 is the fundamental sector harmonic), subject to order and symmetry selection rulesSource quote & editorial note
Six- and eight-sector machines are free from strong essential resonances ... also, the symmetry easily permits four accelerating gaps per revolution, a situation well suited to rf cavities.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 266-267
Editorial note, tabletop extrapolation: 810-MeV specifics (vr climbing to 2, spiral sectors) do not scale down; the method — list resonances crossed by your vr/vz trajectory before fixing N, then let RF layout break ties — applies to any AVF design.
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Consult fabricators about producible sizes and processes before finalizing magnet geometry, and let fabricability (available forging/plate sizes, machining method) drive the construction concept.
Source quote & editorial note
Representatives of the steel industry were consulted to determine the size of forging of the required shapes that could be practicably produced.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 136
Editorial note, tabletop extrapolation: Scale-free: for a next machine this reads 'call the waterjet/plate supplier before freezing the pole drawing' — same move as TID-454's cost-driven magnet design.
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Put the field-critical dimensions on iron geometry rather than on coil placement - the quoted design principle - and plan from the outset to shim the finished magnet: post-construction shimming is 'reasonable to expect'.
Source quote & editorial note
A magnet of this design places all the critical dimensions on the iron geometry and minimizes the sensitivity to errors in coil placement. It is reasonable to expect that the final magnet would have to be shimmed after construction
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 172
Editorial note, tabletop extrapolation: Directly scale-free: machined iron holds its dimensions in a way wound copper cannot, and 'shim after construction' is a scheduled step rather than a failure mode. Trim coils, where fitted, are a separate adjustability decision with their own warm-magnet limits (dg-160).
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Stage the model-magnet program: carry competing configurations through deliberately crude models to settle gross characteristics, then build one accurate model whose field maps are good enough for orbit computation.
Source quote & editorial note
The model tests to date have been directed at determining the gross characteristics of various configurations ... Future models will include one very accurate version on which measurements suitable for orbit calculation can be made.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 172
Editorial note, tabletop extrapolation: Maps onto the FEMM-first pipeline: cheap comparative FEMM runs play the role of crude models; only the chosen geometry earns a high-fidelity field map for the Python tracker.
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Match power-supply regulation to each coil's fractional contribution to the field: the source used transistor-regulated supplies of 1-part-in-1e4 stability for every coil contributing more than 1% of the field.
regulation stability ~ (field tolerance)/(coil's fractional field contribution)Source quote & editorial note
Transistor-regulated power supplies with 1 part in 10^4 stability are used to energize coils which contribute more than 1% to the magnetic field.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 274
Editorial note, tabletop extrapolation: Scale-free budgeting instinct (from a 42-gauss analogue machine): spend regulation money in proportion to field contribution. The 1% line and any source-sharing arrangements are that design's choices; the general form is regulation ~ field tolerance / coil contribution, applied against your own stability budget (dg-027).
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Hold the magnet gap to a relative tolerance of order a few parts in 1e4 of the gap when the field must satisfy an isochronism/focusing spec across the pole.
gap tolerance +/-0.004 in. on 8 in. gap = 5e-4 relativeSource quote & editorial note
Gap tolerance +/- 0.004 in.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 137
Editorial note, tabletop extrapolation: 810-MeV provenance: the spec belongs to a 53-ft isochronous magnet, and even the RELATIVE number (5e-4 of the 8-in gap) is that machine's, not a scale-free constant - the transferable content is the framing: derive the next machine's gap tolerance from its allowed field error via a magnetostatic model or measured dB/dg, then stack machining, assembly and thermal terms; sanity-check the result against the 5 G / 5-deg-phase budget.
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Choose the accelerating-structure topology by total-machine cost: if a dee-sized magnet gap prices the magnet unreasonably, move the resonator out of the gap (cavities between sectors) rather than paying for gap in iron and amp-turns.
Source quote & editorial note
The cost of the magnet would be increased unreasonably if a gap suitably large for conventional dees were provided. For this reason, a system for acceleration with vertically oriented resonant cavities was adopted.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 145
Editorial note, tabletop extrapolation: The specific topology (vertical TEM cavities) is 810-MeV-only; the transfer is the coupling: every inch of dee clearance is bought with magnet cost, so dee-gap and magnet-gap must be traded as one system, as in a next machine's gap decision.
-
Prefer the RF configuration you can analyze - the source chose the ordinary coaxial cavity as 'more amenable to design' - and set its free dimensions as documented compromises, theirs being voltage-holding ability against transit-time effects.
Source quote & editorial note
chosen for the final design since this is the ordinary coaxial cavity and is more amenable to design ... was chosen as a compromise between voltage-holding ability and transit-time effects.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 174-176
Editorial note, tabletop extrapolation: Scale-free method: a dee-stem system is likewise a transmission line with machine-fixed dimensions and a few free ones - when sizing the planned higher-voltage dee (the 5-13 kV upgrade), name each free spacing's compromise pair in the design notes the way the source names theirs.
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Build a scale model of the resonator to validate the design method: theirs certified the calculation - 151.3 Mc/s predicted, within 4% of measurement - and caught a several-percent construction error in the spacing near the median plane; both are the quoted outcomes.
Source quote & editorial note
Checking of the model dimensions revealed a construction error of several percent in the spacing near the median plane ... a resonant frequency of 151.3 Mc/s was calculated for the model; this is within 4% of the measured value.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 177
Editorial note, tabletop extrapolation: Scale-free double duty: a bench mock-up of a next machine's dee/stem before the LDMOS amplifier arrives certifies the calculation and catches build errors - and while it sits on the bench, sweeping for higher-order modes and measuring Q are nearly free additions (dg-664).
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Budget RF power in explicit named lines - the source's budget: computed cavity loss 500 kW + beam power 160 kW + contingency 200 kW (about 30% on top of the computed lines) = 860 kW total.
P_total = P_cavity + P_beam + P_contingency (source: 500 + 160 + 200 kW; contingency ~30% of the computed lines)Source quote & editorial note
Computed power loss in cavity 500 kW; Beam power 160 kW; Contingency 200 kW; total 860 kW
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 180
Editorial note, tabletop extrapolation: The kilowatts are 810-MeV numbers; the structure sizes the planned 100-500 W LDMOS chain honestly - compute the resonator loss (dg-313), add beam and coupling loads, then carry contingency as a NAMED line of the source's ~30% class instead of hiding margin inside each estimate.
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Select the amplifier-to-resonator coupling by its behavior during a spark: the source's scheme reflected a large resistive load to the amplifier plates when the cavity sparked, DECREASING tube plate current - prefer arrangements with that property.
Source quote & editorial note
Thus, when a spark occurs in the cavity a large resistive load is reflected to the plates of the power amplifier and the tube plate current would decrease.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 182-183
Editorial note, tabletop extrapolation: Scale-free fault-mode-first design: dees spark at every scale, so choose a next machine's amplifier coupling for arc behavior, not just matched-condition efficiency - establish what YOUR coupling does to the device when the load arcs (some couplings raise device stress instead), then layer the protection accordingly (dg-338, dg-679). Directly relevant to protecting an LDMOS pallet.
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Measure the minimum (threshold) accelerating voltage that still produces beam, and read its radius-dependence as a diagnostic: a threshold nearly independent of radius points to central-region limits rather than distributed field errors.
Source quote & editorial note
The threshold is practically independent of radius ... the threshold seems to be limited by conditions at the center, phase-slip or otherwise, rather than by field errors throughout the machine.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 285
Editorial note, tabletop extrapolation: Usable on the reference machine now with its existing probe: a dee-voltage threshold scan at several probe radii - holding source output, frequency, field and geometry fixed - helps distinguish central-region limits from accumulated field errors; it is an indicator to combine with other diagnostics, since source drift, detection threshold and interception can each move the measured threshold.
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Size the pumping system from the outgassing load rather than the volume: the source ASSUMED net pump speed at 25% of mouth speed for its baffles and valves, and found published outgassing data high against measurement by ~20x at 1 hour and ~2x at 20 hours.
S_net ~ 0.25 * S_mouth; Blears data vs measured: ~20x high at 1 hr, ~2x at 20 hrSource quote & editorial note
The net speed of these pumps was assumed to be 25% of the speed at the mouth of the pump, because of the usual losses in baffles and valves.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 158
Editorial note, tabletop extrapolation: Scale-free in structure, not numbers: size from the outgassing load, compute the actual duct and baffle conductances (1/S_eff = 1/S_mouth + 1/C - the vacuum deep dive's budget method), and treat handbook outgassing rates as early-time bounds. The 25% is what THEIR plumbing cost them; the reference machine's SI100 stack has its own conductance chain to compute.
Cited in: The Vacuum Budget of a Cyclotron
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Set seal policy by radiation dose and replaceability, as the cited design did: elastomer seals only where the predicted 10-yr dose was below 1e8 rad AND the seal is easily changed; elsewhere their choice fell to metal seals, with the interspace of large double seals pumped (design practice reported around the quoted criterion).
elastomer allowed where 10-yr dose < 1e8 rad AND easily changed (their criterion)Source quote & editorial note
elastomer seals are used only where the predicted 10-yr radiation dose is less than 10^8 rad and where the seal is easily changed.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 157
Editorial note, tabletop extrapolation: The decision MATRIX (dose x replaceability -> seal type) is scale-free and becomes relevant the moment a next machine makes real beam current near median-plane seals; the 1e8-rad line is that design's criterion for its compounds and lifetime - qualify the actual elastomer against predicted dose, temperature, compression set and access before borrowing the number.
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Check whether electrostatic or magnetic deflection wins at your particle velocity before designing an extractor: the equivalent magnetic field for a given force shrinks as B = E/v, so E-fields lose effectiveness as velocity rises.
B_equiv = E/v; their case: 4.4 kV/cm on the Analogue scales to 700 kV/cm at 810 MeV vs only 2,800 gauss magneticSource quote & editorial note
electric fields are relatively ineffective at high particle velocities, but the force on an ion due to a magnetic field is proportional to velocity.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 151
Editorial note, tabletop extrapolation: At 150 keV protons (v ~ 5.4e6 m/s) the comparison runs strongly toward electrostatic: modest septum fields equal coil fields that are awkward to engineer at that scale, which is why documented small machines extract electrostatically. Run the B = E/v arithmetic before copying any big-machine magnetic-channel scheme - the crossover is a computation, not a law.
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Before believing an internal-probe beam-attenuation curve, rule out probe-edge scattering: the cited report re-attributed an apparent current drop primarily to electron scattering from the probe tip, concluding actual beam loss, if any, was very small.
artifact severe when (range in probe)/(radial beam width) >~ 1Source quote & editorial note
this drop is primarily a result of electron scattering from the probe tip. It is now believed that the actual beam loss, if any, is very small.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 278
Editorial note, tabletop extrapolation: Direct transfer to the reference machine's probe work: an apparent current fall-off with radius can be instrumentation, not physics - test by swapping probe material and geometry and by biasing, and think about where particle range in the probe sits relative to the beam dimensions, before redesigning the machine around an artifact.
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In weak-guide-field machines or field regions, measure and where necessary compensate the ambient (geomagnetic) field: in the cited 42-gauss electron Analogue, canceling the horizontal geomagnetic component eliminated an observed beam attenuation.
Source quote & editorial note
When the horizontal component of the geomagnetic field was canceled, this attenuation was eliminated.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 276
Editorial note, tabletop extrapolation: Earth's field (~0.5 G total; the horizontal component is what mattered there) is normally a negligible perturbation inside the reference machine's 0.59-T gap, but real for any low-field electron-analogue experiment, long injection path, or fringe-field beamline - measure the local vector rather than assuming.
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The cited machine came to traverse the difference-coupling resonance vr - vz = 1 without attenuation, even with the horizontal field uncompensated - beam that once died at the resonance passed cleanly.
Source quote & editorial note
It is now possible to accelerate the beam through the difference-coupling resonance vr - vz = 1 without attenuation, even without the horizontal magnetic field compensated.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 285
Editorial note, tabletop extrapolation: Central-region collimation and source definition are high-leverage (relevant to the planned source-species test): a better-defined beam gives resonances and apertures less to eat. That is margin against loss mechanisms that scale with beam quality - not against gas scattering, RF faults, or extraction geometry, which have their own fixes.
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Assume the shielding estimate will prove low and the experiment space too small - the quoted history: shielding initially provided 'has later proved to be inadequate' and experiment areas are 'now too small in almost every installation'. Design margin and expansion room in from the start.
Source quote & editorial note
Historically, the shielding initially provided for high-energy accelerators has later proved to be inadequate ... The experiment areas are now too small in almost every installation.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 184
Editorial note, tabletop extrapolation: Scale-free planning doctrine, and this collection's first design-stage statement of it: leave physical room (and structural capacity) to add shielding around a next machine before the first neutron is made.
Cited in: Shielding a Small Cyclotron
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Design shielding so the stricter general-population dose limit is met in all regularly occupied adjacent areas, even where regulations would allow worker limits - the source's practice, under their era's limits (5 rem/yr occupational, 0.5 rem/yr public).
design limit = public limit in inhabited adjoining areas (their era: 5 / 0.5 rem/yr; current US: 5 rem/yr occupational vs 0.1 rem/yr public - a factor of 50)Source quote & editorial note
we have designed the shielding so that the limits for general population are observed in the regularly inhabited work areas adjoining the accelerator and experiment rooms.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 186
Editorial note, tabletop extrapolation: Directly transferable posture for a residential-basement machine: the family upstairs is 'general population', so design to the CURRENT public limit at occupied locations - in the US today 1 mSv (0.1 rem) per year, fifty times below occupational and five times stricter than the source's era ratio - and take the numbers from the jurisdiction's own regulations (/legal/), not from a 1965 report.
Cited in: Shielding a Small Cyclotron
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Build the shield estimate as an explicit chain - dose limit, source term, attenuation, secondary buildup - recording at each approximation which direction the error runs; the source's own example neglected secondary production and target attenuation together because the net stayed conservative, and only to within the precision of the other data.
Source quote & editorial note
we have neglected both the secondary production and target attenuation; this results in a conservative estimate still within the precision of other data.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 189
Editorial note, tabletop extrapolation: Scale-free methodology (their 810-MeV cascade physics is not): carry the same per-step bookkeeping on a next machine's estimate. The quote's specific lesson: omissions can run in opposite directions and partially cancel, so direction is tracked per step, never assumed - and the net conservatism is only as good as the input data's precision.
Cited in: Shielding a Small Cyclotron
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Separate the radiation components by the question each answers: the penetrating high-energy component sets shield thickness, while the soft/evaporation component sets activation and the dose at surfaces — do not size one problem with the other's source term.
Source quote & editorial note
The thickness of shielding required for a high energy accelerator is established chiefly by the cascade nucleons ... The evaporation particles must be taken into account, however, in determining the activation of materials
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 186-188
Editorial note, tabletop extrapolation: The sort-by-question habit is the transferable part: identify which radiation component sets shield thickness and which sets activation and surface dose for YOUR source term. For a D-D-capable machine that is fast-neutron moderation for thickness, with capture gammas and nuclide-specific activation as separate questions carrying their own data - not a clean analogue of the source's cascade/evaporation split, which is high-energy physics.
Cited in: Shielding a Small Cyclotron
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When your field has no literature on a subproblem, adapt the quantitative methods of the nearest mature field and say so — here, accelerator maze design taken wholesale from nuclear-reactor duct shielding.
Source quote & editorial note
References to maze design for high energy accelerator shields are almost completely absent from the literature. We have based our design on the methods used for nuclear reactor shielding.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 199
Editorial note, tabletop extrapolation: Scale-free research method as practiced there: when the accelerator literature lacked the subproblem, they adapted reactor-shielding methods and said so. The pointer stands with its age showing: reactor duct/labyrinth texts remain a usable starting point for amateur questions this corpus lacks - checked against modern references (NCRP 144-class) wherever safety rides on the answer.
Cited in: Shielding a Small Cyclotron
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Design mazes and penetrations by multiplying per-element transmissions: straight-leg duct attenuation grows with length/radius, each bend attenuates by roughly (1/3)csc(theta) in their data (~0.1 per 90-deg bend with an extended entering leg), legs must never sight intense sources, and parallel ducts sit several diameters apart.
T_total = product(T_leg_i) * product(T_bend_j); T_bend ~ (1/3)csc(theta); extended entering leg adds ~3xSource quote & editorial note
the attenuation at a bend is approximately 1/3 csc(theta) ... An additional factor of 3 attenuation at bends may be gained by extending the entering leg beyond the bend
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 200-204
Editorial note, tabletop extrapolation: The product-of-elements method transfers to a next machine's cable penetrations and entry labyrinth; the factors do not transfer blind - they are low-energy-neutron empirics from that facility's geometry, and spectrum, wall material, duct size and coupled legs move them. Use the method with factors from a current reference (NCRP 144-class data), never sight a source down a straight leg, and verify the result by survey.
Cited in: Shielding a Small Cyclotron
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Leave a designed-in recovery path in shielding layouts: if a maze or penetration proves inadequate, there should be a pre-planned location (an extended leg, a spare recess) where a plug or door can be added later.
Source quote & editorial note
Should the maze design shown prove inadequate ... the attenuation can be greatly improved by the addition of plugs at the bends. The extension of the leg beyond the corner offers a convenient location for a plug door
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 204
Editorial note, tabletop extrapolation: Scale-free insurance: reserving a plug location costs little at design time - some space and a formed recess - and buys a recovery path if the survey finds the maze wanting. Initial shielding estimates often need adjustment, which is why the survey decides (dg-914's bookkeeping); this is the cheap way to be wrong.
Cited in: Shielding a Small Cyclotron
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Use stepped (labyrinth) joints on shield doors and plugs so ordinary construction tolerances are acceptable - with 12-in steps the report tolerated 1/2-in cracks - and account for the shielding thickness lost to mechanisms, which the report notes the wheel spaces inevitably cost.
Source quote & editorial note
The steps provided at the top and sides minimize the dimensional accuracy required. With 12 in. steps, 1/2 in. wide cracks between the plug and the wall are easily tolerable. ... Inevitably the effective thickness of the shielding is reduced somewhat by the space for the wheels.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 206
Editorial note, tabletop extrapolation: The stepped-joint principle scales to block-wall doorways and removable concrete/poly plugs around a benchtop target station - but the tolerable crack size was specific to their 12-in steps and their radiation field, so a scaled-down plug's steps and gaps are checked against its own field (survey), not copied. Where a mechanism eats thickness, make it up locally - added length, or denser material in that spot.
Cited in: Shielding a Small Cyclotron
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Trade shielding construction methods on delivered cost: their study found solid concrete walls placeable for about 2/3 the cost of walls cored with compacted rock fill - the quote; the roof-method comparison is the report's neighboring analysis (scan re-read queued).
Source quote & editorial note
solid concrete walls can be placed for about 2/3 the cost of walls cored with compacted rock fill.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 242
Editorial note, tabletop extrapolation: Their specific answer is 1963 Oak Ridge civil engineering; the transferable habit is costing shielding alternatives (block vs poured vs water vs borated poly) per unit attenuation before building any enclosure for a next machine.
Cited in: Shielding a Small Cyclotron
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Assign contingency per item, not as one number: the cited estimate averaged ~20% contingency but varied it from 15% to 40% per item according to the accuracy with which each estimate could be made (the engineering and escalation adders are the report's companion structure - re-read queued).
total = basic * (1 + ~0.15 eng) + per-item contingency (15-40% by precision) + escalation (their 4%/yr)Source quote & editorial note
the average contingency for the project is approximately 20%, but it varies on specific items from 15% to 40%, depending on the accuracy with which the estimate could be made.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 234
Editorial note, tabletop extrapolation: 1963 AEC percentages, but the structure transfers to any bill-of-materials estimate: catalog items get little contingency, anything not yet fully designed gets a lot - and write down which base each adder applies to (basic cost vs basic-plus-engineering) so the arithmetic is reproducible.
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Sanity-check derived unit prices against what was actually paid for the nearest precedent - the quoted practice: their $0.35/lb finished-magnet estimate judged reasonable against $0.26/lb actually paid for another large magnet; the report's appendix ties its cost lines to suppliers (scan re-read queued).
Source quote & editorial note
The estimate of $0.35 per pound for the finished magnet appears reasonable when compared with the unit price of $0.26 per pound paid for another large magnet at the Laboratory.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 245
Editorial note, tabletop extrapolation: Scale-free estimating hygiene: their App. F traces $11.5M to named suppliers; a next machine's BOM should likewise tie each line to a quote, a catalog page, or a reference machine receipt — and explain deltas ('more complex machining, more waste metal').
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Provision probable future additions now and keep their cost out of the baseline - the quoted split: 'provisions have been made in all plans to make the addition of the medical facility as simple and as economical as possible' while 'the cost of the medical facility is not included in the initial cost of the project'.
Source quote & editorial note
Provisions have been made in all plans to make the addition of the medical facility as simple and as economical as possible ... The cost of the medical facility is not included in the initial cost of the project
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 22
Editorial note, tabletop extrapolation: Scale-free scoping discipline for the business plan: design the educational-machine baseline with hooks for upgrades (extraction port, shielding growth, second station) without loading their cost onto gate-one.
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Put scheduling detail where the novelty is: the ORNL project network-planned the machine and beam handling - 'the major novelties and complexities' - and left the building and shielding out of that programming exercise, relying on conventional construction planning for them.
Source quote & editorial note
Because the major novelties and complexities of the project lie in the area of the machine and the beam handling, these areas were programmed. The building and shielding portions of the project were not programmed
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 252
Editorial note, tabletop extrapolation: Scale-free effort allocation: plan the risky subsystems (source, RF, field mapping) at fine grain; conventional logistics still get milestone-and-dependency tracking - procurement lead times, lifting, electrical and shielding milestones - just not fine-grained networks.
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Treat the first schedule as a hypothesis: when the critical path gives an unacceptable duration, re-evaluate every activity on it and resequence - ORNL completed the vault and building first so magnet assembly could begin earlier, cutting the ~8-year-10-month initial estimate substantially (figure sighted in the scan; the resequencing decision is the quoted mechanism).
Source quote & editorial note
All activities on the critical path were then re-evaluated ... It was decided that the cyclotron vault and cyclotron building could be completed first, to allow the magnet assembly to begin at an earlier date.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 258
Editorial note, tabletop extrapolation: Scale-free: iterate the schedule, overlapping long-lead assembly with remaining construction. Note what sat on their critical path per the report's activity lists - field plotting, re-plot analysis, iron alignment rechecks - field mapping is schedule, not an afterthought, at any scale.
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Resolve individual turns with a thin radial wire probe: a 0.020-in. tantalum wire scanned from 1.2 to 11.5 in. on the ORNL 22-inch showed distinct current maxima for orbits 1 through 12, spaced 5/8 in. for inner orbits at high dee voltage, the resolvable-orbit count being set (in that machine) by the dee potential.
uniform-field, centered-orbit estimate: dr per turn ~ r*(dE/E)/2, corrected by 1/(1+(r/B)dB/dr) with a field map; general form dr = dE/(dE/dr)Source quote & editorial note
The data show individual orbital positions from the first orbit up to the twelfth, the upper limit being determined by the potential on the dees.
Editorial note, tabletop extrapolation: A candidate measurement for the reference machine - measured turn spacing plus the field map gives effective energy gain per turn, which would anchor its uncalibrated ~1.3 kV dee voltage (via gap count, synchronous phase and transit-time factors, not directly). First check feasibility: at ~1.3 kV the inner-turn spacing may be smaller than the existing probe wire - compute dr against probe width before promising resolution. Fig. 12 (PDF p.41) shows the 22-inch doing this at 9.2-12 kV dee-to-dee.
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Expect spurious contributions in wire-probe current: on the 22-inch, probe current rose slightly with radius, attributed to increased thermal emission of electrons from the probe under bombardment by higher-energy protons - a baseline to separate from real beam structure before interpreting a radial scan.
Source quote & editorial note
There is a slight increase in probe current with increasing radius because of increased thermal emission of electrons from the probe as it was bombarded by protons of higher energy.
Editorial note, tabletop extrapolation: Same artifact family as the reference machine's Faraday-cup offsets - with the mechanisms kept straight: at nA and sub-MeV, deposited power is ~mW and an ordinary wire will not reach thermionic temperatures (do the conduction arithmetic before invoking it); SECONDARY emission and electronic offsets are the live suspects at that scale, so bias or shield the probe and log the baseline against beam-off checks.
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Make the deflector adjustable and expect a minority fraction: the 22-inch development deflector, with full adjustability, extracted 38% of a 1000-uA internal beam under the BEST conditions — treat tens of percent as a good small-machine electrostatic extraction efficiency, reached by tuning, not by drawing.
extraction efficiency ~38% at best on a 22-in-orbit machineSource quote & editorial note
A very effective adjustable beam deflector has been developed; under the best conditions, 38% of a 1000 ua internal beam has been deflected.
Editorial note, tabletop extrapolation: Sets expectations for any future extraction gate: design the septum/deflector with in-vacuum adjustability - the quoted 'very effective' unit was fully adjustable and even so extracted 38% at BEST. Tens of percent is the documented ballpark for classical deflectors (dg-496, dg-595); define success for your machine before the attempt, and account for where the undeflected majority goes (dg-260).
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On the experimental unit, with dees limited to 10 kV, injection potentials over 10 kV decelerated ions in the gap between the accelerating electrode and the dee; their fix was raising the dee-side capability - a redesign for at least 20 kV dee-to-ground.
first gap accelerates only while the signed electrode-to-dee potential difference is favorable (their case: V_inject > V_dee ran it backward)Source quote & editorial note
Since the dee voltage in the experimental unit was limited to 10 kv, application of injection potentials of over 10 kv resulted in deceleration of ions between the accelerating electrode and the dee.
Editorial note, tabletop extrapolation: Any source-bias or puller experiment must check the same ordering in ITS geometry: a dc extraction potential that overtops what the RF gap can supply runs the first gap backward. The check is signed potentials and timing at the actual gap - the source's inequality is that machine's instance of it, not a universal bound.
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In the cited high-potential arc source for multiply charged ions, two things were found: electrode alignment with the magnetic field is critical, and admitting gas greatly reduced the average electron energy - high-energy electrons appeared only with no gas feed.
Source quote & editorial note
The alignment of the electrodes with the magnetic field is critical. High energy electrons are obtained when no gas is fed to the chamber, but when gas is introduced the average electron energy is greatly reduced
Editorial note, tabletop extrapolation: For the reference machine's filament source and the planned source-species test: align the source to B before blaming the arc supply, and treat arc electron energy as gas-pressure-COUPLED - which direction and how strongly, for the actual source, is a pressure-scan-plus-mass-analysis measurement, not an inherited monotonic law about H+/H2+ balance.
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Ion-source output was found approximately proportional to the effective slit length in the cited 22-inch tests (the aperture dimensions and output currents are the report's data - re-read queued).
I_source ~ proportional to slit length at constant width, arc, and extractionSource quote & editorial note
The output of the ion source was found to be approximately proportional to the effective length
Editorial note, tabletop extrapolation: The chimney-slit length is a free knob - to first order, more length is more current at constant width, arc and extraction - but pair any lengthening with the z-distribution probe check (the same machine's earlier quarter tied arc-slit length to z-wise beam loss), and verify the gain survives to TRANSMITTED beam, not just source output.
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Judge injector/source changes by transmitted beam at radius, not by current near the source: on the 22-inch, current at 1.5 in continued rising with accelerating potential while beam at 10.5 in optimized at 3 kV or less - a divergence the report read as changes in ion focus.
optimum V_inject (by full-radius beam) was 1-3 kV, arc-intensity dependentSource quote & editorial note
Since the current measured at 1.5" continues to increase with accelerating potential while the beam measured at 10.5" is optimized at 3 kv or less, changes in ion focus are indicated
Editorial note, tabletop extrapolation: The central tuning trap: a source tweak that fattens the inner-radius signal can starve the Faraday cup at full radius - so score source changes at the radius that matters (extraction or target), with the near probe as the diagnostic companion rather than the scoreboard.
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Survey the median plane and magnetic center with a floating current-carrying wire loop: hung nearly friction-free, it sits in unstable equilibrium at the median plane and tends to center itself on the magnetic center of the field; loops of several diameters map the field region (22-inch practice; the report's wire gauge and current are report-attributed - scan re-read queued).
Source quote & editorial note
the position of unstable equilibrium at the median plane can be found The current-carrying loop also tends to center itself with respect to the magnetic center of the field
Editorial note, tabletop extrapolation: A near-zero-cost magnet diagnostic - but engineer the five minutes it runs: compute the wire's I^2R heating and use a current-limited supply with short energizations, restrain the loop and add travel stops (a free conductor in a tesla-scale field moves hard when energized), and keep hands clear at switch-on. Use it as the coarse locator of median plane and center, then confirm with the Hall-probe map.
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Small-machine magnet survey results, 22-inch: the magnetic median plane coincided with the geometric median plane within +/-0.125 in (checked at 6-, 11- and 22-in diameters) and the magnetic center with the geometric center within +/-0.25 in - measure both; they are separate alignments.
median plane within +/-0.125 in.; magnetic center within +/-0.25 in. (22-in. machine)Source quote & editorial note
the median plane of the 22-inch cyclotron, at 6", 11", and 22" diameter, coincides with the geometric median plane within +/- 0.125" and that the magnetic center coincides within +/- 0.25"
Editorial note, tabletop extrapolation: The measure-both discipline transfers; the inch values do not - they are one machine's observed alignments, not acceptance limits. Derive the reference machine's own tolerances from its pole radius, gap, harmonic budget and central-region sensitivity, then survey against those.
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Check dee-voltage clearances OUTSIDE the vacuum tank too: the ORNL ion-source testing unit's dee voltage was expected to be capped not by in-vacuum gaps but by a 1.5-in dee-stem spacing in air outside the tank.
Source quote & editorial note
The dee voltage will undoubtedly be limited, though, by the spacing between the dee stems outside the vacuum tank, which is only 1.5" at one point
Editorial note, tabletop extrapolation: For the LDMOS upgrade toward 5-13 kV dees, walk the whole RF path on BOTH sides of the wall - feedthroughs, stem gaps in air, coupling hardware, creepage across insulator surfaces, and the vacuum-side gaps and multipactor windows - and let field analysis, ratings and conditioning tests say which limit binds first; the cited machine's air-side cap is one historical outcome, not a law.
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The pole iron is the durable identity: ORNL's 1949 test cyclotron was the '22-inch' by maximum orbit, and after the rework it was 'more appropriately identified as the 44-in. cyclotron' - renamed for its equivalent pole diameter, the report's own naming logic.
Source quote & editorial note
Inasmuch as the equivalent diameter of the pole pieces is 44 in., the machine is more appropriately identified as the 44-in. cyclotron.
Editorial note, tabletop extrapolation: The reference machine's H-frame is the analogous asset: energy upgrades - gap, shims, dees, RF power - can stage around the same 757-lb iron for years. The platform reading is the editorial lesson drawn from ORNL's staged reuse of one magnet line (1.5 MeV, then 5 MeV, then proposed heavy ions); the quote itself carries the renaming.
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DC accelerating-electrode geometry for a cyclotron source resisted a priori design in the cited program: of several dc electrode geometries tested on the 44-inch, none accelerated the proton beam to maximum radius as well as the standard rf accelerating electrode - the plain rf gap stayed the benchmark.
Source quote & editorial note
Direct-current accelerating electrodes of several geometries have been tested, but none were found to accelerate the proton beam to maximum radius as well as the standard type of r-f accelerating electrode.
Editorial note, tabletop extrapolation: A caution for any puller-electrode or biased-extraction scheme on the reference machine: after four quarters of ORNL trials, dc injection still lost to the ordinary rf gap on that machine. Simulate candidate geometries (fields calculate fine; the plasma boundary is the uncertain part), validate experimentally, and keep an unmodified configuration as the control in every source A/B test.
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Shift the beam center electrically with 'half-coils': an insulated conductor wrapped halfway around the pole piece, attached so the pole completes the circuit (the 600 A / 3.6 in / energy-sweep performance figures are the report's account - re-read queued).
600 A opposing half-coil set -> 0.5 oersted/in. gradient across an 86-in. poleSource quote & editorial note
One of these coils consists of an insulated conductor wrapped half-way around the magnet pole piece and attached so that the pole piece completes the circuit.
Editorial note, tabletop extrapolation: A field-trim knob that steers orbits without touching iron - as a modeling hypothesis for a next machine: specify ampere-turns and the return-current path, run the magnetostatic and orbit analyses (FEMM models it directly), check contact heating and forces, and only then test; variable-energy operation is a beam measurement away, not a feature to advertise from the wiring diagram.
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Material choice for beam-intercepting hardware must include activation: a thin-wall stainless septum mockup handled 190 W per inch of water-cooled tube, but type 304's extreme induced radioactivity disqualified it and drove a switch to aluminum alloy — thermal adequacy is not the whole selection (86-inch deflector development).
bench test - 0.025-in.-OD, 0.003-in.-wall SS tube, 7.7 in.3/min water, ~190 W/in.Source quote & editorial note
The extreme radioactivity induced in type 304 stainless steel makes its use undesirable, the use of an aluminum alloy is now being investigated.
Editorial note, tabletop extrapolation: At sub-MeV energies on ordinary structural metals activation is small where it occurs at all - thresholdless capture and deuteron operation are the exceptions - and the selection logic transfers whole: thermal adequacy is not the whole selection. Prefer aluminum or graphite for probes, septa and slits anywhere protons above a few MeV are contemplated, and let the licensing story inherit the same reasoning.
Cited in: Shielding a Small Cyclotron
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A variable-energy cyclotron is a credible Van de Graaff alternative in the 5-10 MeV band: ORNL's study concluded feasibility, with energy definition better than +/-10 keV achieved by collimation plus magnetic analysis of the deflected beam - selection, not correction: the analyzer transmits a narrow band and discards the rest, trading current for resolution - and 1-10 uA deflected.
energy definition < +/-10 keV via deflected-beam collimation + magnetic analysisSource quote & editorial note
such a cyclotron is feasible, that an energy definition of less than +/-10 kev could be achieved, and that deflected beams would be in the range of 1 to 10 ua
Editorial note, tabletop extrapolation: Direct prior art for the plan's educational variable-energy concept: vary energy with field/frequency plus a movable target (cf. the 44-inch spacer), and buy energy DEFINITION with a simple analyzed beamline - accepting the current it costs - rather than machine perfection.
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For the 86-inch Be-on-aluminum neutron targets, flux brazing was rejected: the extreme probability of large flux inclusions between the beryllium and the aluminum base would seriously impair heat transfer. The reported alternative - vacuum-furnace brazing with a thin Al-Si interlayer - is report-attributed (scan re-read queued for the interlayer spec and bond result).
0.006-in. Al-Si (11.5% Si) interlayer, vacuum furnace -> 100% bondSource quote & editorial note
The method of brazing is considered unsatisfactory because of the extreme probability of leaving large flux inclusions between the beryllium metal and the aluminum base, which would seriously impair heat transfer.
Editorial note, tabletop extrapolation: The corpus's targetry shelf is thin, and the transferable core is real: flux is a void-former at exactly the interface a beam target cannot afford. For a next machine's boron or beryllium targets on copper or aluminum, treat flux-free vacuum or controlled-atmosphere brazing as the candidate route - and qualify it with coupon brazes, sectioning and thermal cycling, because wetting and expansion behavior change with each material pair.
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Thick-target neutron yield planning number: bombarding beryllium with ~20-MeV-class protons on the 86-inch gave approximately 1 neutron per 50 protons — the machine served as a controlled fast-neutron source for a biology program on this basis.
Y(n) ~ 1 neutron / 50 protons, thick Be target, ~20 MeV protonsSource quote & editorial note
a beryllium target is bombarded with protons, approximately 1 neutron for 50 protons is obtained.
Editorial note, tabletop extrapolation: SCALE-SCOPED - this 2% yield is a ~20-MeV number; at the reference machine's and a next machine's energies (0.15-5 MeV) p-Be yields are orders of magnitude lower. Useful as the upper anchor when building the shielding/licensing dose model for any future MeV-class educational machine.
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Sequence rf design around measurement: ORNL designed every component of the 44-inch rf system EXCEPT the filament-coupling circuit, deliberately, because that circuit depends on the resonant dee system's electrical characteristics and "cannot be designed until these characteristics are determined" — leave the coupling stage undesigned until the tank/dee resonator is built and measured.
Source quote & editorial note
Since this circuit depends upon the electrical characteristics of the resonant dee system, it cannot be designed until these characteristics are determined.
Editorial note, tabletop extrapolation: The template for the reference machine's LDMOS upgrade - freeze the amplifier and dee-resonator designs, but specify the matching/coupling network only after measuring the real dee system's f0, Q, and shunt impedance on the bench. Ordering the coupling parts first is the classic mistake this rule prevents.
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One machine, two energies by mechanical reconfiguration: on the ORNL 44-inch, shifting the position of the dees and target selects a working radius of 11 in. or 20 in., while the ion source position remains unchanged and the beam orbits remain centered; the spacer dimension (14.5 in.) and the 1.5/4.9-MeV proton energies are reported in the companion specifications (ORNL-1670 and the ORNL-1663 spec table, dg-947).
fixed B and f; target radius 11 or 20 in. -> 1.5 or 4.9 MeV (E ~ r^2)Source quote & editorial note
a choice of radius, 11 in. or 20 in., is thus obtained by shifting the position of the dees and target. In either case the ion source position remains unchanged and the beam orbits remain centered
Editorial note, tabletop extrapolation: Variable energy WITHOUT retuning B or rf - E ~ r^2 at fixed field and frequency - by repositioning the dee assembly AND target together as ORNL did; a target-only intercept at reduced radius is a simpler tabletop variant (an extrapolation, not ORNL's method), and either way the delivered energy is verified from the mapped field and measured target radius, not assumed calibrated.
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Insulate the entire dee system from ground so a dc bias can be applied to control ion loading — designed into the rebuilt 44-inch from the start (and already proven on the 22-inch: ornl-1339 measured accelerated-beam gains from dee bias; ornl-1269's Fig. 12 ran 600 V bias).
Source quote & editorial note
The whole dee system is insulated from ground so that a bias potential may be applied to control ion loading.
Editorial note, tabletop extrapolation: The reference machine already uses dee bias; the design rule for a next machine is to make bias a first-class requirement - insulate the dee-stem support (see the ornl-1884 cantilever-on-insulators execution) rather than retrofitting isolation later.
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High dee voltage buys its clearance out of the magnet gap: to run 100 kV, ORNL removed the flat shims from the tank, accepting a wider 13.5-in. gap (and the field cost that implies) — dee-voltage ambition, aperture, and gap trade against each other and must be budgeted together (44-inch cyclotron).
Source quote & editorial note
The removal of the flat shims from the tank increased the magnet gap to 13 1/2 in. and provides sufficient clearance to permit operation of the dees at a potential of 100 kv.
Editorial note, tabletop extrapolation: For a next machine the same ledger applies at 5-13 kV: dee-to-liner spark distance plus dee aperture plus liner clearances must fit inside the gap, and gap given to voltage clearance is field taken from energy - in the gap-dominated, fixed-ampere-turn regime (dg-021's measured caveat on the ideal scaling). Decide voltage and gap together (dg-181).
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Scaling datapoint - the revised ORNL 44-inch as specified: 6400 oersteds in a 13.5-in. gap, 9.7 Mc/sec, up to 100 kV dee-to-dee, giving 1.5-MeV protons at 11-in. radius or 4.9 MeV at 20 in.
B = 6400 Oe, f = 9.7 Mc/s, V_dd <= 100 kV; E = 1.5/4.9 MeV at r = 11/20 in. (nonrelativistic check: 0.64 T gives ~1.5 MeV at 11 in)Source quote & editorial note
Beam radius, in. 11 / 20; Proton energy, Mev 1.5 / 4.9; Magnetic field, oersteds 6400; Magnet gap, in. 13.5; Maximum dee-to-dee potential, kv 100; Frequency, megacycles/sec 9.7 (spec table, condensed)
Editorial note, tabletop extrapolation: The nearest professional sibling to a next machine in this collection - same ~0.64 T field class and ~9.7 MHz as the reference machine's 0.59 T / 9 MHz. Use it to sanity-check B-f consistency; note the 100 kV (vs ~1.3 kV) buys energy per turn and fewer turns - less phase slip and interception - while the energy-radius relation stays set by the field.
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Develop cyclotron RF on an electrical model: the variable-energy oscillator test used an 8-ft section of the 63-inch dee-stem electrical model as its resonant system - the quoted practice; the dee-simulating capacitors and circuit-selection details are the report's own (scan re-read queued).
Source quote & editorial note
The push-pull circuit for this test was constructed by using an 8-ft section of the electrical model of the 63-in. cyclotron dee stems as the resonant system.
Editorial note, tabletop extrapolation: A bench-scale dee-stem mockup (pipe sections plus padding capacitors) lets the next machine's oscillator/coupling scheme be raced against alternatives for pocket change - the same measure-on-model philosophy as the deferred filament-coupling rule, one report earlier in hardware form.
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Coupled-secondary (transmission-line) tuning works but watch the Q: a series coil-and-variable-capacitor secondary magnetically coupled to the dee stems reflected a variable impedance into them, sweeping resonance from 6 to 12 Mc - but the secondary's comparatively low Q made the dee-stem resonant impedance vary markedly across the band.
reflected impedance of coupled secondary shifts f0; low secondary Q -> impedance swings with fSource quote & editorial note
This circuit consists of a coil and variable capacitor connected in series, plus the inherent resistance of both elements. The magnetic coupling between the dee stems and secondary circuit results in an impedance being reflected into the dee stems from the secondary. ... A resonant frequency varying from 6 megacycles to 12 megacycles was achieved with the particular circuit tested. ... the resonant impedance of the dee stems varies markedly with the frequency due to the comparatively low 'Q' of the secondary circuit.
Editorial note, tabletop extrapolation: Relevant if a next machine ever adds a variable-frequency or remote trim element: any lossy tuning appendage coupled to the dee resonator drags its shunt impedance (hence dee voltage per watt) across the tuning range - minimize tuner loss and measure loaded Q and shunt impedance over the whole range, whatever the tuner's construction.
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Flatten the base field BEFORE testing shims: the 44-inch pole faces (the tank walls themselves) were ground with a portable grinder toward +/-0.01% uniformity explicitly so the flat field "will then provide a standard base for the various magnetic shim designs that may be tested" — the order of operations (known-flat baseline, then shim experiments) is the rule; the tolerance number is secondary.
Source quote & editorial note
the magnet pole faces (tank walls) are being ground with a portable grinder to provide a very uniform magnetic field, as near +/- 0.01% as possible. This will then provide a standard base for the various magnetic shim designs
Editorial note, tabletop extrapolation: For a next machine's shim development: establish and map the unshimmed field to the best flatness attainable FIRST, so every FEMM-predicted shim is measured against a known zero rather than an uncharacterized pole error. Set the flatness target from a phase budget, not a fixed gauss figure: accumulated slip is roughly 360 deg x N_turns x dB/B for a uniform mismatch, so a many-turn low-voltage machine needs proportionally tighter field than a few-turn one. (Also proof that hand tooling on installed poles was acceptable ORNL practice - no magnet disassembly required.)
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Divide fabrication deliberately: ORNL contracted the liner, dees and dee-stem housing to an outside shop while making faceplates, dee stems, ion source, target probe and vacuum system locally - the quoted split; the contractor difficulties that followed are the succeeding reports' account (the 1670 -> 1795 -> 1884 arc).
Source quote & editorial note
The liner, dees, and dee-stem housing are being fabricated by an outside contractor. The faceplates, dee stems, ion source, target probe, and vacuum system were fabricated locally
Editorial note, tabletop extrapolation: The three-report arc remains this collection's cleanest outsourcing story: the contracted brazed, water-cooled vacuum parts were where the delays landed - one program's experience, and a fair prior. For a next machine: buy simple machining, keep leak-integrity parts in-house or design them repairable.
Cited in: The Vacuum Budget of a Cyclotron
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Commission in a designed-in reduced-energy state: the rebuilt 44-inch's 14.5-in spacer moved the dees back from the field center so the machine could run at ~1.5 MeV for test operation at very high proton currents, before removal for full 5-MeV running.
Source quote & editorial note
This spacer moves the dees back from the center of the magnetic field so that the machine can be operated at approximately 1.5 Mev for test operation at very high proton currents.
Editorial note, tabletop extrapolation: Mirrors staged-gate logic - plan a low-energy high-current commissioning configuration as a mechanical state, not an improvisation, so beam-physics problems are separated from full-energy behavior. Reduced energy closes many reaction channels but not all: thresholdless capture (12C(p,gamma), 14N(p,gamma)) and light-element targets remain live, and very high current makes small cross sections and thermal loads consequential - so each commissioning state still gets its own reaction check, survey and beam-loss budget.
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Automatic resonance tracking by sweep-and-store: a control that sweeps the oscillator across its band, stores the peak voltage seen across the coupled secondary, then re-sweeps and stops when the live voltage equals the stored peak, tuned to the SECONDARY'S resonance within ~0.1% (114-inch study, tested with a small oscillator).
two-pass sweep; stop when V_live = V_stored(peak); tuning error ~0.1%Source quote & editorial note
The error of the control in tuning the oscillator to the frequency of the secondary is of the order of 0.1%.
Editorial note, tabletop extrapolation: A 1954 peak-hold autotune implementable today in a microcontroller: sweep the exciter, record the dee pickup peak, re-sweep and lock. Two scope-of-validity notes: it locks to the CAVITY resonance, not to the beam-synchronous f = qB/(2*pi*gamma*m) - the field still sets that independently; and 0.1% was demonstrated unloaded, so validate peak detection and drift on the beam-loaded resonator before trusting it.
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Design water-cooled dees so the cooling circuit is reachable: leaks in the 44-inch dees' internal water tubes sat in 'very inaccessible locations' and delayed final assembly - repair required cutting windows through the dee sides, then closing them by Heliarc welding.
Source quote & editorial note
several leaks in very inaccessible locations have delayed final assembly. In order to repair the leaks in the internal water-cooling tubes it was necessary to cut windows through the sides of the dees. The windows were then closed by Heliarc welding.
Editorial note, tabletop extrapolation: If a next machine's dees carry water: treat internal cooling leakage as a credible failure and route tubing so joints and runs can be reached (or provide removable covers) where RF and vacuum allow; pressure-test the dee as a unit BEFORE it meets the liner; and note the historical recovery mode - cut a window, fix, reweld - is documented practice worth keeping in the back pocket.
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Expect the achieved field flatness to land short of the grinding aspiration: after a further half-year of grinding and shimming the tank walls, the 44-inch field stood "uniform to within 0.05%" against the +/-0.01% goal stated in ORNL-1670 — a 5x gap between target and achieved flatness at a national lab, and the machine proceeded anyway.
aspiration +/-0.01% (ORNL-1670 p. 20) vs achieved 0.05% after ~1 year of workSource quote & editorial note
Grinding and shimming of the tank walls to produce a flat magnetic field was continued. The magnetic field is now uniform to within 0.05%.
Editorial note, tabletop extrapolation: Calibrates expectations, not a budget line: sustained professional effort on the 44-inch bought 5e-4 base-field uniformity against a 1e-4 aspiration - so plan for the ground pole to fall short of its target and for shims to close the remaining gap, with the actual allowable derived from the machine's own phase-budget arithmetic and verified by mapping. How the 0.05% split between grinding and shimming the report does not say.
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Build the model magnet for measurement access: ORNL's 14.4-ton quarter-scale 114-inch model put the magnet gap in a VERTICAL plane 'to provide the greatest access for making field measurements' and made the pole tips removable 'so that shims of any shape can be inserted readily'.
Source quote & editorial note
The one-quarter-scale model magnet is of the closed-yoke type. ... Its total weight will be 14.4 tons; 12.7 tons will be iron and 1.7 tons will be copper. The magnet gap will be in a vertical plane to provide the greatest access for making field measurements. The pole tips are removable so that shims of any shape can be inserted readily.
Editorial note, tabletop extrapolation: For any next-machine shim-test rig (or a scaled FEMM-validation magnet), design for the measurement campaign: open sightlines for the Hall probe, pole tips that unbolt, gap oriented for jig access - the orientation serving the probe rather than mimicking the final machine is the editorial reading of ORNL's choice.
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Sliding RF joints, 114-inch study: at an RF load of 100 A per lineal inch the tested pneumatic-pressure movable contact held under a 10 C rise with only 0.5 gpm of cooling water (contact material and pressure-insensitivity claims report-attributed - scan re-read queued).
tested point: 100 A/lineal in, <10 C rise, 0.5 gpm (that joint, that geometry) - not a design allowableSource quote & editorial note
at an r-f load of 100 amp per lineal inch, the temperature rise could be held to less than 10 C by a water flow of only 0.5 gpm.
Editorial note, tabletop extrapolation: For a next machine's shorting planes and tuning bars, compute the actual RF surface current at the contact, then validate the joint thermally at that current and duty - the cited numbers say such joints are buildable, not that 100 A/in is free. The material lesson (plate stainless with copper; bare SS is an RF resistor) is sound skin-effect physics at any scale.
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Design subsystems as a reusable kit: the proposed 44-to-48-inch conversion needed only a new magnet and vacuum tank because the oscillator, dee system, vacuum system, ion source, target probe, and power supplies were all judged reusable — subsystem modularity is what makes a machine upgradable into a different machine (44-inch cyclotron).
Source quote & editorial note
All other components of the present 44-in. cyclotron, oscillator, dee system, vacuum system, ion source, target-probe, and power supplies, would be utilized.
Editorial note, tabletop extrapolation: A strong argument for clean interfaces between a next machine's subsystems: ORNL could contemplate a new machine class for the price of iron and a tank because everything else was JUDGED reusable - the judgment is the quote's; the adaptation cost of the reuse is not on this card. Design interfaces so the same judgment could be true of your machine.
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The ORNL 44-inch cantilevered the whole dee system from a mounting at the outer end of the dee stems, supported on insulators to permit applying a bias potential to the dees - one support plane carrying the entire resonant structure.
Source quote & editorial note
The whole dee system is supported by a cantilever mounting at the outer end of the dee stems. This mounting is supported on insulators in order to permit the application of a bias potential to the dees.
Editorial note, tabletop extrapolation: An attractive pattern for a next machine: one stiff cantilevered dee-stem mount outside the field region, isolated for DC bias, is mechanically simpler than distributed insulated supports. Design the RF side separately - insulating the mount enables bias but does not by itself define the RF return path, so engineer the ground plane, bypassing and bias feed network explicitly, and check insulator loading and flashover.
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Adapting existing equipment mortgages the machine: ORNL's own five-point verdict on the 63-inch - built fast from adapted parts, it ended up unshieldable, with marginal field (median plane drifts, hard to keep shimmed), dee-to-ground capped at ~40 kV by its bushing insulators, a 6-in. gap half of what was needed, and a single-species rf system — and none of the five "can readily be corrected".
Source quote & editorial note
a large amount of existing equipment was adapted for use in the accelerator, and many design compromises were accepted. Consequently, this machine lacks the versatility and reliability which are essential ... which cannot readily be corrected: 1. The cyclotron is not and cannot be shielded ... [the dee stems] must enter the vacuum through bushing insulators. This limits the maximum dee-to-ground potential to about 40 kv ... 4. The magnetic field gap is only 6 in., less than half of what it should be to obtain the desired output.
Editorial note, tabletop extrapolation: The counterweight to thrift - surplus-equipment compromises in shielding provisions, magnet gap, and insulator ratings are the ones a finished machine cannot shed. When designing a next machine around salvaged parts, check each against this five-item list; anything on it deserves new hardware.
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The 48-inch conversion spec set design dee-to-dee voltage at 200 kV against a 110-kV threshold for N5+ - a factor of about 1.8 over threshold.
V_design / V_threshold ~ 200/110 ~ 1.8Source quote & editorial note
Dee-to-dee r-f voltage (design), kv 200; Threshold voltage for N5+, kv 110 (Table 3, condensed)
Editorial note, tabletop extrapolation: Margin philosophy consistent with the 63-inch's 75-vs-60 kV acceptance hold (ornl-1339): documented machines bought well over threshold. For the LDMOS upgrade, compute the threshold dee voltage for the intended turn count and buy real headroom - documented precedents cluster around 1.3-2x. What the margin purchases (orbit count, loading headroom, species reach) is the editorial reading, not the table's statement.
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Site an accelerator below grade and the earth is your shield: the 48-inch room was planned "mostly below ground level" explicitly because it "will be easy to shield", at basement floor level for heavy-equipment transfer, adjacent to the existing building so utilities barely extend and the existing control station works without moving.
Source quote & editorial note
Being mostly below ground level, the room will be easy to shield. Placing the room at the basement floor level will make it convenient to transfer heavy equipment.
Editorial note, tabletop extrapolation: Directly relevant to the facility question for any MeV-class educational machine: below-grade siting was the study's shielding strategy, and siting beside existing utilities and controls was a cost line they weighed as seriously as the magnet. Earth shields in the directions it actually covers, by its actual thickness, density and moisture - it does not blanket-replace engineered shielding, and the uncovered directions, the roof, and every penetration still get the full design treatment (see the shielding deep dive).
Cited in: Choosing Your Machine · Shielding a Small Cyclotron
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Retire beam-dynamics risk deliberately: ORNL PLANNED an electron-model accelerator 'to be used in assessing the importance of imperfection resonances and the feasibility of their penetration' before committing to the 1-BeV proton machine - the plan is what the quote records.
Source quote & editorial note
Plans are being made for an electron-model accelerator to be used in assessing the importance of imperfection resonances and the feasibility of their penetration.
Editorial note, tabletop extrapolation: A historical instance of risk-ordered development: when the open question is orbit dynamics, a cheap electron model is one way to attack it before proton iron is bought - scaled properly (dg-892's rigidity caveat). The tabletop program's equivalent instruments are the tracker and measured field maps.
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A major rebuild of even a small, staffed machine runs about two years decision-to-tested-assembly: 44-inch revision design underway Mar 1953 (ORNL-1531), design essentially complete Mar 1954 (ORNL-1670), assembly approaching completion Sep 1954 with contractor rework (ORNL-1795), assembled and vacuum-tested but NOT yet on beam Mar 1955 — with ion source, oscillator auxiliaries, and shimming still open.
timeline: design start +12 mo = design done; +6 mo = assembly (blocked on contractor); +6 mo = assembled/vacuum-tested, beam still pendingSource quote & editorial note
The major components have been assembled and vacuum-tested (see Fig. 5).
Editorial note, tabletop extrapolation: Schedule realism, one datapoint thick: a professional division with machine shops took about two years from revision concept to vacuum-tested assembly, with outsourced fabrication the long pole (dg-951). A home program's periods stretch and compress differently; the census's one-to-six-year first-beam spread is the wider base rate.
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Architect an external beamline as condenser -> shielded slit -> analyzer: the cyclotron's apparent source is too fuzzy to analyze directly, so first focus as much beam as possible onto a precision slit, then use that slit as the sharply defined object for the analyzing magnet.
Source quote & editorial note
in order to produce a suitable object for the analyzing magnet, we introduce a second magnet whose sole function is to focus as much of the beam as possible on a precision slit.
Editorial note, tabletop extrapolation: DIRECT for any ANALYZED external line on a next machine - the canonical two-stage architecture: a condenser focuses as much beam as possible onto a precision slit, and that illuminated slit becomes the analyzer's cleanly defined object. Lines that only transport or irradiate skip the apparatus; the slit's shielding is the companion rule (dg-966).
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Put the beam-defining slit inside the shield wall, because the fraction of beam intercepted by the slit system is itself a strong radiation source; put the condenser as close to the beam exit port as fringe fields allow (minimizes horizontal spread), and give the analyzer a long image distance to reduce angular spread at the image.
Source quote & editorial note
A considerable amount of undesirable radiation will be produced by that part of the beam intercepted by the slit system. ... it is also desirable that the analyzer image distance be large, in order to reduce the angular spread of the beam at the image point. ... [placing the condenser farther from] the cyclotron port ... required larger condenser pole pieces in order to accommodate the horizontally spreading beam.
Editorial note, tabletop extrapolation: DIRECT and cheap to honor at layout time, nearly impossible later: treat every defining aperture as a place where beam power - and therefore radiation - concentrates. At 150-170 keV the intercepted beam makes mostly heat plus thick-target bremsstrahlung whose X-ray yield climbs steeply with voltage, so the slit belongs with the shielded, surveyed components, wherever the survey ranks it that day.
Cited in: Shielding a Small Cyclotron
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Prefer a strong-focusing quadrupole pair over a sector magnet for the condenser role: the study's comparison gave at least tenfold less weight and power (the quoted factor), a straight-pipe vacuum, and - because the beam is undeflected - field and lens tunability without geometry changes; the as-built pairing was 355 lb of doublet against an estimated 3 tons of sector magnet (p.32).
Source quote & editorial note
the weight and power requirements would each be less than the corresponding sector-magnet requirements by at least a factor of ten.
Editorial note, tabletop extrapolation: DIRECT - the as-built comparison (p.32) was 355 lb for the doublet pair vs an estimated 3 tons for a sector condenser. At a next machine's rigidity (~7x lower than Rochester's 4e5 G-cm) a doublet becomes a benchtop object; the no-deflection tunability argument is the one to remember when laying out the line.
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Treat the cyclotron as an astigmatic source when designing external optics: the effective vertical-plane point source does not coincide with the horizontal one (vertical object distance greater), the angular spread is greater in the horizontal plane, so the cited design made the first lens convergent horizontally and required the common image to be real and beyond the magnets.
Source quote & editorial note
the effective 'point' source in the vertical plane does not coincide with that in the horizontal plane and is such that the vertical-plane object distance V is greater. ... The second is simply that the common image be real and beyond the magnets themselves. ... Since it is known that the angular spread is greater in the horizontal than in the vertical plane, we make the first lens convergent in the horizontal plane.
Editorial note, tabletop extrapolation: DIRECT design input for next-machine transport modeling: fit separate horizontal/vertical source points and divergences from measured beam profiles (or a quadrupole scan) rather than assuming a stigmatic waist at the extraction channel - then let the measured two-plane phase space, not the historical ordering, choose the first quad's polarity.
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Size quadrupole aperture from the measured extracted-beam envelope with explicit margins - the report's arithmetic: the measured beam box gave semi-axis a = 3 cm, they applied 'an extra factor of safety' and took c = 1.5, hence poles at xy = +/-2.25 cm^2.
hyperbolic poles xy = +/-c^2; an inscribed ellipse of semi-axes A, B is tangent when c^2 = A*B/2; the report: a = 3, c = 1.5 -> xy = +/-2.25 cm^2Source quote & editorial note
With this as a guide we apply an extra factor of safety and take a = 3, c = 1.5, hence the magnet poles are given by xy = +/- 2.25 cm^2
Editorial note, tabletop extrapolation: DIRECT method, not numbers: measure the real beam first, then stack explicit margins on the way to the pole constant. A next machine's envelope comes from its own extraction simulation or measurement; margin-then-round-up is what prevents discovering an undersized bore after the coils are wound.
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Weigh pole-profile precision against need: the authors had custom milling cutters made to generate true hyperbolic quadrupole profiles and later concluded plain circular arcs would have been satisfactory for their quadrupoles.
Source quote & editorial note
Morley Machine Company, Rochester, N.Y., produced milling cutters conforming to this equation ... Subsequent work has shown that circular arcs would have been satisfactory.
Editorial note, tabletop extrapolation: A candidate money-saver for a next machine's quads: circular-arc (or round-stock) tips - validated by checking the integrated multipoles and end effects in FEMM against the beam's actual field-quality requirement, which is where the modeling time belongs; adequacy depends on aperture fraction used and multipole tolerance, so it is not automatic.
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Use effective (not physical) magnetic length for quadrupole optics: measurements on these magnets showed effective length up to ~20% greater than physical - their design treated 18.1 cm physical as 20 cm effective, a 10% correction.
l_eff ~ up to 1.2 x l_phys for these small-bore quads; all lens equations use l_effSource quote & editorial note
Measurements have shown that the effective length of the magnets is as much as 20% greater than the physical length.
Editorial note, tabletop extrapolation: DIRECT: for short quads the fringe extension is a first-order effect, not a correction - and it scales with aperture, which is why short, fat quads see the largest effect. Get l_eff per magnet from the FEMM/tracker pipeline; ignoring it produces significant focal errors.
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Run beam-transport quads at deliberately low field (~1 kG): avoids iron saturation, keeps excitation power low enough to skip water cooling entirely, and leaves headroom; since lens strength parameter lambda scales as B^1/2 for a given particle and energy, excitation current is a smooth tuning knob.
B = (lambda/l)^2 * (a/2) * B_rho ~ 1 kilogauss at design point; lambda proportional to B^1/2Source quote & editorial note
This low field avoids saturation difficulties in the magnet iron and high excitation power requirements. Furthermore, it enables us to dispense with water cooling in the windings.
Editorial note, tabletop extrapolation: DIRECT: at a next machine's rigidity, transport-quad pole-tip fields of a few hundred gauss are plausible - compute the actual requirement from aperture, length and focal geometry (the formula) - and where field and current density land as low as the source's, unsaturated iron with air-cooled random-wound coils is exactly the regime they describe. Confirm with the dissipation arithmetic before skipping water (dg-708). OCR trap - the text layer renders the B^1/2 exponent as B^2; page image verified B^1/2.
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Connect all four coils of a quadrupole strictly in series on one supply: paralleling (or individual supplies) makes it 'extremely difficult' to keep the four pole gradients equal - the quoted reason. The report sizes the winding by an ampere-turn path integral with explicit margin (the full specification: scan re-read queued; the previously published card's winding detail was truncated).
series connection forces equal current through all four poles - gradient symmetry by circuit topology; NI sizing per the report's path-integral computation (full spec queued)Source quote & editorial note
the coils in each unit are connected in series since otherwise we would have extreme difficulty in maintaining uniform gradients.
Editorial note, tabletop extrapolation: DIRECT wiring doctrine for any home-built multipole: gradient symmetry comes from forced equal current, not matched resistances - which is also why surplus-wire coil construction works, since the series circuit forgives resistance mismatch between coils.
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Keep analyzing-magnet field below the onset of pole-edge saturation (here ~8 kG for a 4 cm gap C-magnet): above it the field grows less uniform near the pole boundaries, which is exactly where a wedge analyzer's focusing happens. This sets a minimum bend radius for the top energy (rho >= 47 cm for 7 MeV protons, B-rho = 3.8e5 G-cm).
rho_min = B_rho(E_max) / B_max(uniformity-limited); their case: ~3.83e5 G-cm at 7 MeV over 8 kG -> rho ~ 48 cmSource quote & editorial note
For fields above about 8 kilogauss, saturation effects begin to set in, and the field becomes less uniform near the pole boundaries.
Editorial note, tabletop extrapolation: DIRECT sizing rule with scale caveat: the 8 kG threshold is geometry- and steel-specific, but the logic (uniformity budget, not raw B_sat, sets the working field; bend radius follows) applies to any analyzer dipole on a next machine. At ~170 keV protons rho is a few cm even at modest fields - the analyzer becomes a bench magnet.
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Correct wedge-magnet geometry for fringe field by shifting the effective pole boundary outward: the report adds an empirical 0.4*G term (its Eq. III-23 form, with the csc factors for the entrance/exit angles) to the pole-face spacing relation.
D = X + (sin(Omega)/sin(gamma2))*Y1 + 0.4*G*(csc(gamma1)+csc(gamma2)) (Eq. III-23); symmetric case eps1 = eps2 collinear bisectorsSource quote & editorial note
The effect of the fringe field is to shift the effective pole boundary outward, and this is taken into account empirically by adding to the right-hand side of III-20(b) a term 0.4 G
Editorial note, tabletop extrapolation: For a next machine's analyzer designed in FEMM, the sanity check is the concept, not the constant: compute the effective field boundary from the longitudinal field integral of the simulated fringe and compare against the steel edge - an offset of very roughly half a gap is the expected order. Do not equate the 0.4G term with a tracking code's FINT parameter (FINT conventions carry fringe focusing integrals, a different quantity).
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Match model order to input-data quality: Rochester declined to base the magnet design on second-order calculations because the fringe-field corrections were 'not sufficiently precise to warrant' it - the quoted judgment; the wedge-design context and the clearance check they did run are the report's detail (scan re-read queued).
Source quote & editorial note
the methods for correcting for the fringe fields effects ... are not sufficiently precise to warrant basing the magnet design on the second-order calculations.
Editorial note, tabletop extrapolation: DIRECT design-philosophy rule for the whole next-machine campaign - match model order to input-data quality. Also note the companion check they DID run (pp.49-50), that the bent beam clears the back of the magnet with ~5 cm margin for the full 6 cm beam - a 30-second calculation that catches a catastrophic layout error.
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Test a magnetic line before beam with the floating current-carrying-wire technique - the standard check the report applied to its wedge analyzer (a taut wire carrying current I follows the trajectory of a particle with B-rho = T/I, given known tension and controlled sag); the commissioning details it credits the method with catching are report-attributed (scan re-read queued).
Source quote & editorial note
The operation of the wedge analyzer has been checked using the standard current carrying wire technique.
Editorial note, tabletop extrapolation: The wire method is a superb zero-beam measurement of magnet optics for a teaching lab or a first analyzer - state tension, sag and field-orientation assumptions when using B-rho = T/I. Budget alignment and tuning provisions into any multi-element line as a design habit; the cited line's transmission and energy-spread figures await the re-read before serving as benchmarks.
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A Buechner-Bainbridge 90-degree broad-range spectrograph (uniform field; source and focus each one characteristic radius outside the field boundary) covers a wide energy band in one exposure; the practical top of the band is set by chamber size - beyond ~1.3 E0 the exit chamber grows unreasonable - and single-focusing solid angle punishes the high end (detailed range/resolution figures report-attributed - scan re-read queued).
energy scales as (B*R)^2 for similar optics; the cited instrument: R = 50 cm at 14 kG for 33 MeV protonsSource quote & editorial note
an extension of the energy range much beyond 1.3 E0 requires an unreasonably large vacuum chamber at the exit of the magnet.
Editorial note, tabletop extrapolation: SCALE-HONEST only when the scaling is done: the geometry fixes E/E0 ratios, but reaching a given E takes B*R. For ~170 keV protons, B-rho ~ 0.06 T-m, so an R ~ 5-10 cm bench version needs roughly 0.6-1.2 T - iron-pole territory, not a few hundred gauss. Still compelling as a teaching-lab focal-plane instrument; copy the optics and size the field honestly.
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Relax instrument specs to the actual measurement: relaxing the original requirement for 'extremely high field uniformity' collapsed the Browne-Buechner-derived design to a simple C-shaped yoke - the quote; the specific relaxations (the uniformity figure, deferred pole-tip spacers, the rationale) are the report's detail (scan re-read queued).
Source quote & editorial note
By relaxing the original requirements for extremely high field uniformity, a considerable simplification of the Browne-Buechner design was achieved in reducing the magnet yoke structure to a simple C-shape.
Editorial note, tabletop extrapolation: DIRECT and very relevant to a next machine - the whole report is a case study in not copying the flagship instrument (Browne-Buechner at MIT) but re-deriving requirements from the local physics program. Compact C-yokes, deferred correction hardware ("add spacers only if needed" - they never were), and unconventional yoke placement are all fair game once the real spec is known.
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Reproducibility is the first test of a field error: uniformity maps at 6.8 and 14 kG showed few-tenths-percent nonuniformities identical in location and magnitude at both excitations, and the authors did not expect these variations to have significant effect on their instrument.
Source quote & editorial note
the location and magnitude of these non-uniformities were the same at both 6.8 and 14 kilogauss, and it was not expected that these variations would have any significant effect
Editorial note, tabletop extrapolation: Two ideas worth writing into a mapping procedure, each with its limit: (1) an error that scales rigidly with excitation CAN be absorbed by end-to-end calibration for a relative instrument - after a trajectory or resolution check shows it does not bend the optics; reproducible is necessary, not sufficient. (2) Degrading NMR signal above some field is a prompt to investigate - saturation inhomogeneity is one suspect among probe tuning, gradients and positioning; confirm with B-vs-I behavior before concluding.
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Build the analyzing-magnet vacuum chamber out of the magnet itself: the pole tips formed the chamber top and bottom, with thin non-magnetic stainless strips welded to the tips as side walls (the gap tolerance, brass spacers and baffles are the report's construction details - re-read queued).
gap 3/4 in uniform to 0.0001 in via brass spacers; 5-in-thick heat-treated C1010 tips, faces ground flatSource quote & editorial note
The tips formed the top and bottom of the vacuum chamber of the magnet, while the side walls of the chamber were strips of non-magnetic stainless steel welded to the tips.
Editorial note, tabletop extrapolation: The poles-as-chamber pattern eliminates the gap-wasting separate tank (the alternative Bromley rejected on machining/gasketing grounds, nyo-3823 p.6) - carry the METHOD and derive the gap tolerance from the analyzer's own field-error and resolution budget, minding weld distortion across the span.
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Provide a sight-line port directly opposite the entrance slit for optical alignment of an analyzing magnet, and a dedicated port for the field-measuring (NMR) probe - four ports total: beam in, beam out, alignment, field probe.
Source quote & editorial note
One of the other ports is located opposite the entrance slit to facilitate alignment of the magnet and the fourth one houses the nuclear magnetic resonance probe.
Editorial note, tabletop extrapolation: Cheap at design time and expensive to retrofit: a straight-through optical path (laser today) opposite the entrance slit plus a permanent probe port turn alignment and field checks from teardown jobs into routine ones - each port still buys its window, its leak path and its magnetic clearance, so put both on the port list and budget them honestly.
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To swing a multi-ton spectrometer around a target, the track was rendered flat and horizontal to within 0.01 in by a grinding machine rotated about the vertical center post - precision generated in place, self-referenced to the final axis (the bearing and drive arrangement is the report's construction - re-read queued).
Source quote & editorial note
The track has been rendered flat and horizontal to within 0.01" by a grinding machine rotated about the vertical post.
Editorial note, tabletop extrapolation: Two machine-design lessons to EVALUATE at any scale: generate precision in place with the tool swung about the final axis (kin to Wilson's lapped dees), and consider kinematic three-point support so the instrument neither rocks nor needs a precision floor - choosing the actual bearing layout from load, stiffness, overturning-moment and angular-accuracy analysis rather than copying the 5-ton architecture at 1/50 size.
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Calibrate a magnetic spectrograph with a monoenergetic alpha source stepped through field settings: with all exposures for equal times, the measured intensity of each group provided the relative solid angle as a function of focal position - plus the radius-vs-position map and a linewidth check against source width.
Source quote & editorial note
Since all exposures were for equal times, the measured intensity of each group provided a measurement of relative solid angle as a function of focal position.
Editorial note, tabletop extrapolation: Teaching-lab gold with its conditions stated: one sealed alpha source calibrates the focal-plane acceptance function that theory only estimates - under controlled equal-exposure conditions (stable source output, fixed geometry, detector response and processing held constant, no saturation). What it cannot test: proton-specific detector response and beamline effects, which need their own checks. Validate the peak-position convention against the actual detector's lineshape.
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Precompute the operating aids: the cited spectrograph combined its calibration data into a nomograph connecting proton energy, lithium NMR frequency, and image position on the focal surface by a straight line - setup and particle-group identification at the console, not the desk.
Source quote & editorial note
the information of Figs. 5 and 6 can be combined into a nomograph ... corresponding values of proton energy, lithium resonance frequency and image position on the focal surface
Editorial note, tabletop extrapolation: DIRECT for the teaching program: the 2026 equivalent is a small lookup app with nu*rho-vs-energy curves per probe nucleus and kinematics tables for the expected reactions (natural extensions of the sourced three-variable nomograph); run-time decisions need precomputed inverse tables, and students can build the nomograph itself as an exercise.
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Design the focal-plane detector for exposure multiplexing: a cassette holding three 80x200 mm emulsions allowed six different exposures without breaking spectrograph vacuum; alongside it the system used a solid-state counter array covering the focal region where only a few groups mattered (array details reported elsewhere in the source).
Source quote & editorial note
Three emulsions each 80 x 200 mm can be mounted in a special camera ... which allows six different exposures to be made without breaking the spectrograph vacuum.
Editorial note, tabletop extrapolation: The principle is vacuum cycles are the tax on focal-plane work - amortize them: a movable frame of film/CR-39 chips (integrating, etched after removal - a survey detector, not prompt readout) or a silicon strip/PIN-diode array (direct charged-particle detection; a bare SiPM is a photon detector and needs a scintillator) behind the next machine's analyzer. Their split - survey in emulsion, precision groups in counters - still maps cleanly.
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Opening a spectrograph's in-plane angular acceptance costs kinematic broadening of peaks when scattering off light nuclei; the cited instrument accepted that trade for large-angle reach.
Source quote & editorial note
In scattering from light nuclei, this introduces appreciable kinematic broadening of peaks as the entrance aperture is opened.
Editorial note, tabletop extrapolation: For a next machine's Rutherford-scattering station the same knob exists: closing the entrance aperture trades count rate for resolution. State the broadening honestly - dE ~ |dE/dtheta|*dtheta depends on beam energy, angle and kinematics in general; only the FRACTIONAL elastic broadening at fixed masses and angle drops out energy-independent - so compute it for the actual geometry rather than quoting a mass-ratio shortcut.
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A conventional cyclotron usually needs no beam sweeper for pulsed work - the source's point: the beam is already naturally bunched into RF-phase packets, so timing structure comes built in, unlike a Van de Graaff's DC beam, which must be swept or bunched.
Source quote & editorial note
the problem of obtaining a pulsed beam usually does not arise, because the beam of a conventional cyclotron is already naturally bunched.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 6
Editorial note, tabletop extrapolation: DIRECT and foundational for the experiment catalog: the reference machine at 9 MHz delivers phase-bunched beam at the RF period - a measurable, teachable property and the enabling fact for gated counting. 'Usually' is operative: time-of-flight at fine resolution, or experiments needing low repetition rate, can still require pulse selection or extra bunching - check bunch width and period against the experiment's timing demands.
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Derive the timing reference from the cyclotron oscillator itself, not from a beam-intercepting pickup: RF-derived reference pulses are insensitive to beam-current changes and are all smooth and identical in shape; the residual phase shift between beam bunches and oscillator when the magnet tuning changes is small enough in practice to ignore.
Source quote & editorial note
the pulses are obtained in a way which makes them insensitive to beam current changes, and b) all reference pulses are smooth and identical in shape.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 6
Editorial note, tabletop extrapolation: The most directly transferable finding here: the machine's RF is a free, stable timing fiducial at any scale - clock gated counting and TOF off a capacitive sniff of the dee. A fiducial is not a beam-arrival timestamp: beam phase relative to the RF moves with field tuning, loading and cable delays, so calibrate the offset against a real beam signal - and re-calibrate after retuning - before treating RF zero-crossings as beam time.
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RF timing pickup, as built: a short (~10 in) No. 12 wire antenna inside the oscillator enclosure a foot or two from the grid circuit - loose capacitive coupling - feeding a pulse circuit whose input carries fundamental and harmonics, shaped with a shunting cable stub; output pulses about 10 V high with rise time of order 5 ns.
reported: ~10 V pulses, rise of order 5 ns; stub retuned after frequency changesSource quote & editorial note
connected to a short (10") antenna of No. 12 wire which extends inside the oscillator house to within a foot or two of the grid circuit of the oscillator. ... The output pulses are made about 10 volts high. ... time is of the order of 5 ns
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 8
Editorial note, tabletop extrapolation: Buildable on the reference machine: loose capacitive pickup plus stub-phased harmonic mixing sharpens the oscillator's waveform into a fast edge with zero active electronics at the pickup - noting a passive stub network can only re-phase and weight harmonics ALREADY in the picked-up signal (an oscillator's tank waveform has them; a purified sine does not). Check the pulse shape after every retune, and measure the actual 10-90% rise rather than assuming the vintage figure.
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Order a gated TAC's start/stop for rare events: START on the (rare) detector pulse, STOP on the next RF reference pulse, and gate the reference channel so stop pulses emerge only after a detector event - the converter then runs ~once per neutron instead of once per RF cycle.
Source quote & editorial note
stop trigger pulses emerge only after an event occurs in the neutron detector.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 8
Editorial note, tabletop extrapolation: The reversed (common-stop) architecture inverts the time axis and slashes unnecessary converter starts and their dead time (pileup in the detector chain is its own problem). With a modern TDC or digitizer you can instead timestamp both the detector and RF streams continuously and form differences offline - the gated arrangement remains the right shape for TAC-style hardware.
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Split slow pulse-height discrimination from the fast timing chain, and make the threshold resettable against a standard: the source gated its analyzer with a slow side-channel discriminator, reset after shutdowns to the peak of the observed gamma-ray pulse-height spectrum from a Cs-137 source.
Source quote & editorial note
The problem was to set the continuously variable slow discriminator dial so that the level of discrimination would correspond to a certain standard light signal from the scintillator. A Cs137 source was used as a standard. The discriminator level was set to correspond to the peak in the observed y-ray pulse height spectrum.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 13
Editorial note, tabletop extrapolation: Two transfers: keep the background-rejection threshold out of the timing path (the source's chains fought when combined), and standardize the threshold against a reproducible spectral feature - in an organic scintillator a Cs-137 source gives a Compton distribution, so define the set-point on its observed peak or edge, exactly as the source did with its own spectrum. A check source is cheap in effort; acquiring one follows the applicable sealed-source rules.
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Time-resolution budget honesty: achieved 2 ns FWHM in the favorable case, 2-3.5 ns typically, at ~1 ns/channel - the source notes it is easily possible to do worse with incorrect stop pulses or too-low photomultiplier voltage, and that the 1-in detector thickness, chosen for counting efficiency, contributed appreciably to widening (5 MeV neutron transit ~0.8 ns).
FWHM ~2 ns best, 2-3.5 ns typical; ~1 ns/channel; 1-in transit ~0.8 ns for 5 MeV neutrons (v ~ 3.1 cm/ns) - the geometric transit span, an upper bound on that term's FWHM contributionSource quote & editorial note
One channel is equivalent to about one millimicrosecond. ... The full width of the lines at half maximum is about 2 ns in this favorable case. Generally the widths have ranged from approximately this to about 3.5 ns, although it is easily possible to do worse by using incorrect stop signal pulses, or too low photomultiplier voltage, etc. ... the thickness of the [scintillon] neutron detector used in these measurements was 1 in, which made the counting efficiency high, but contributed appreciably to widening the peaks. The flight time of a 5 Mev neutron through the detector is about 0.8 ns, for example.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 11
Editorial note, tabletop extrapolation: DIRECT budgeting template: list every term (source bunch width, detector transit, electronics jitter, reference-edge slope) and know which one you bought deliberately. A next machine's TOF or coincidence lab should have students build exactly this budget before blaming the electronics.
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Set flight-path length against the room, not just the resolution equation: most experiments kept paths under 1.2 m to avoid difficulty with neutrons scattered from the solid concrete floor - the quoted choice; the timing-window mechanism and the detector-shield history are the report's account (scan re-read queued).
Source quote & editorial note
Most experiments have been made with flight paths less than 1.2 meters long in order to avoid difficulty with neutrons scattered from the solid concrete floor
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 12
Editorial note, tabletop extrapolation: DIRECT pair of lessons: (1) geometry (short path, floor clearance, timing window) is often cheaper background suppression than shielding mass; (2) never bolt on a detector shield whose effect on efficiency you haven't calibrated - it converts a known instrument into an unknown one. Both transfer to any next-machine counting station.
Cited in: Shielding a Small Cyclotron
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Anchor absolute counting efficiency to a well-known reaction and cross-check by an independent method: the source calibrated with D(d,n) (cross sections then known to 4%), then verified via induced activity - N-13 positron annihilation flux compared against an NBS-calibrated Na-22 source with a coincidence counter - agreeing within 10%.
Source quote & editorial note
Calibration curves were obtained by use of the D(d,n) reaction, the cross sections for which are known to 4% accuracy. ... the yield of annihilation radiation from the N13 decay positrons was compared with the known flux of annihilation radiation from a sodium 22 source calibrated at the Bureau of Standards. A coincidence counter setup was used for these measurements. Results obtained in this way agreed to within 10% with expectations from the absolute calibration of the neutron detector
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 12
Editorial note, tabletop extrapolation: Metrology doctrine that transfers whole: one calibration path is an assumption, two are a measurement. For a next machine's yield claims, require a primary calibration plus an activation- or source-based cross-check, use CURRENT evaluated cross sections at the actual energy and angle (the 4% was the authors' 1950s assessment), and treat the disagreement as a diagnostic to explain - folding it into the systematic only once understood.
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A simple single-scattering model predicts organic-scintillator neutron efficiency usefully: eff = (1 - E0/En)*(1 - exp(-nH*sigma_np*l)). The source calls the first factor exact and response-shape-independent - which holds given its implicit assumptions: isotropic center-of-mass n-p scattering (uniform recoil spectrum), a single hydrogen scatter, and a sharp threshold; find E0 per threshold setting from a calibration reaction.
eff = (1 - E0/En)(1 - exp(-n_H*sigma_np(En)*l)); valid as a first-order model for thin hydrogenous scintillators; degrades with n-p anisotropy at higher energy, carbon interactions, proton escape, multiple scatteringSource quote & editorial note
The first factor in (1) is exact. It does not depend on the exact shape of the response curve (pulse-height vs proton recoil energy) of the scintillator.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 15
Editorial note, tabletop extrapolation: A lovely teaching derivation - a two-factor closed form students can test against a calibration reaction - and the transferable habit is identifying which factor rests on which assumption. Validate against calibration or Monte Carlo for the actual detector and energy range before leaning on it.
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When slow neutrons from one burst can be overtaken by fast neutrons from the next (frame overlap), cut the beam-pulse rate by electrostatically deflecting bunches at a subharmonic of the machine RF - ~3 Mc effective rate virtually eliminated the source's problem. Prefer odd division ratios: at even ratios bunches pass at both zero crossings of the deflection voltage, changing the effective scaling (1:6 passes every third bunch, not every sixth).
f_scaled = f_cyc/3 typical (3.3-5 Mc from 10-15 Mc); even subharmonic 1:2k passes bunches at both voltage zerosSource quote & editorial note
In our case reducing the frequency of beam pulses to about 3 mc can virtually eliminate the problem.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 16
Editorial note, tabletop extrapolation: Check overlap arithmetically for the actual spectrum and flight path - t[ns] ~ 72.3*L[m]/sqrt(E[MeV]), so even an all-sub-MeV spectrum overlaps at a 10 MHz rate over a 1 m path, and D-D work adds multi-MeV neutrons on a sub-MeV machine. The subharmonic plate pair is a genuinely cheap cyclotron chopper for periodic bunch rejection and duty-cycle control - single-bunch selection needs a gating scheme beyond a sinusoidal drive - and the odd/even zero-crossing subtlety is real circuit physics worth teaching.
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Design auxiliary RF systems with the minimum number of tuned circuits - the cited scaler had exactly one (the deflection-plate tank itself), so changing cyclotron frequency meant retuning one circuit (the divider's lock ranges and gating scheme are the report's implementation - re-read queued).
multivibrator locks at f_cyc/3 for 2-5 Mc output over 10-15 Mc input; one tuned circuit total (deflector tank)Source quote & editorial note
In order to simplify tuning procedures the scaler system was designed with a minimum of tuned circuits; there is only one, the tank circuit associated with the beam deflection plates.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 17
Editorial note, tabletop extrapolation: Every tuned circuit is a knob someone must retune at every frequency change - minimize them by design. On timing: the cited system took its precision edge directly from the oscillator, a sound default; a modern divider or PLL can carry timing when its phase error and jitter are characterized against the experiment's budget - the rule is budget-the-jitter, not never-divide.
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Retire RF-system risk with a scaled electrical model before cutting full-size metal: build the complete RF circuit at reduced scale (frequency scales inversely with size), verify tuning range, voltage distribution, and power on the bench, then commit to full-scale construction on the model dimensions. The 184-inch followed a three-stage chain: calculation (MacKenzie BP-140), half-scale model (this report), full-size bench test before installation.
half-scale resonates at ~2x full-scale frequency, and characteristic impedance is scale-invariant - for geometrically similar structures in the same mode with the same dielectric; lumped parts, couplers, losses and joints break exact similarity, so the model verifies the geometry-dominated partSource quote & editorial note
Performance of the model is considered sufficiently satisfactory to proceed with the full scale design and construction based on the model dimensions.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 16
Editorial note, tabletop extrapolation: A next machine's dee/stem/tank is already benchtop-sized, so the transferable form is the mockup itself — a cheap RF-only copy (no vacuum) of the dee-liner geometry, swept with a VNA before the vacuum parts are machined. Same lineage as UCRL-64 and MDDC-1045 already in this collection.
Cited in: Choosing Your Machine
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Scope the model to the physics it must answer: only the RF circuit was reproduced - the vacuum system, purely mechanical equipment, and the dee-bias insulation were omitted, the last explicitly because 'it had no radio frequency function'. Known omissions were listed, not ignored.
Source quote & editorial note
Only the radio frequency circuit was simulated in the model, the vacuum system and purely mechanical equipment was not included. Insulation required for the application of bias voltage to the dee and condenser rotor was not included as it had no radio frequency function.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 7
Editorial note, tabletop extrapolation: License to mock up the next machine's RF cavity in bare copper/aluminum on a bench plate - no chamber, no pumps - provided every electromagnetic boundary that shapes the mode is reproduced: RF-current surfaces (liner included), coupling structures, and any dielectric near high fields. A bare-metal model validates resonance and field geometry; Q, loss and breakdown under vacuum still need the real thing.
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Extrapolate model power to full scale as P ~ V^2 with a shunt-impedance credit for scale (skin effect: doubled size at halved frequency raises Q and R_sh by sqrt(2)); the report's numbers track the law closely - 520 W at 1.5 kV on the half-scale model against 146 kW at 30 kV full scale (the law predicts 147 kW; rounding in one of the printed figures accounts for the difference).
P_full = P_model*(V_full/V_model)^2*sqrt(s), s = model/full linear scale; printed pair agrees to ~1% (146 vs 147 kW - dg-501-style note, not exact)Source quote & editorial note
For 30 kv on the full scale system the above power input figures become 146 kw at 9.25 mc, 132 kw at 12 mc, 146 kw at 15 mc, and 98 kw at 23 mc for continuous operation.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 15
Editorial note, tabletop extrapolation: The V^2 term is the live part for power budgeting: measured drive power at a safe low dee voltage extrapolates as (V_target/V_test)^2 on the SAME matched, linear, unloaded cavity - so a 1500-V measurement anchors the 5-13 kV LDMOS requirement, with beam/plasma loading, thermal drift of losses and amplifier efficiency budgeted on top, and the extrapolation ending where multipactor or breakdown begins.
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Three parasitics set a dee system's resonant range and deserve first attention: the capacity presented to the dee by the dummy dee, the minimum capacity of the tuning element, and the inductance at the dee throat (stem junction). Reducing any one raises the frequency.
Source quote & editorial note
These were the capacity presented to the dee by the dummy dee, the minimum capacity of the rotor, and the inductance at the throat of the dee.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 10
Editorial note, tabletop extrapolation: Direct checklist for why a tank on the reference machine or a next machine does not resonate where the lumped-element estimate says — dummy-dee proximity, feedthrough/trimmer minimum C, and stem-to-dee transition inductance are the three knobs.
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Tune with every electrode in place: inserting the dummy dee alone dropped the model's upper frequency limit from 48.8 to 44.5 mc and the lower from 19.9 to 18.8 mc — a ~9% detuning from one grounded electrode. A resonance measured on a bare dee is not the operating frequency.
dummy-dee insertion alone: -9% on the upper limit (48.8 -> 44.5 mc)Source quote & editorial note
the insertion of the dummy dee had dropped the upper frequency limit from 48.8 to 44.5 mc, and the lower limit from 19.9 to 18.8 mc
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 9
Editorial note, tabletop extrapolation: Final RF tuning of a next machine's cavity must be done with dummy dee, source structure, and probes installed - the model's single grounded dummy dee moved the band edges ~9%, and each added structure perturbs by its own amount: measure or simulate the shift for the actual geometry rather than budgeting any particular percentage in advance.
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Keep a two-sided trim toolkit for a cavity that lands off-frequency: a shorted stub (shorter than lambda/4 at the operating frequency, hence inductive) attached to the dee RAISES resonance; added dee-to-liner capacity plates LOWER it. The source's measured costs: stubs +3 Mc for +25% drive power; 200 uuf of plates -1 Mc for +5% power.
shorted stub < lambda/4 acts inductive, raises f (here 47 -> 50 mc, +25% power); added C lowers f (200 uuf: 19.5 -> 18.5 mc, +5% power)Source quote & editorial note
a shorted stub - a section of transmission line less than a quarter wave length at 50 mc - was connected to each side of the dee.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 9
Editorial note, tabletop extrapolation: The recovery plan if a next machine's fixed-frequency cavity misses its target after assembly. Both fixes tax drive power, and the directions dictate the design bias: aim the design HIGH in frequency if you want to trim with the cheaper capacitive side (which only moves frequency down), or low if you accept stub-trimming up. The cited shift/power figures are that cavity's calibration, not guaranteed ranges.
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The dee throat (stem junction) is a current maximum and the region most sensitive to volume or inductance changes: resetting small dee-to-liner clearances there moved the upper limit 46.2 -> 47.1 mc and cut power 6%. Detail the throat drawings and hold the clearances.
Source quote & editorial note
This region is a current maximum point at the highest frequency and most sensitive to volume or inductance.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 10
Editorial note, tabletop extrapolation: On a small machine the dee-stem-to-chamber-wall clearance is the candidate critical region - it plausibly sets both the resonant frequency and where I^2R heating concentrates. Confirm with an eigenmode/surface-current calculation (or low-power RF measurement with a thermal camera) for the actual cavity, then machine that region to drawing rather than shimming by eye.
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Acceptance criteria for a dee driver, 1947 edition: (1) dee voltage at least twice the DC plate voltage; (2) the oscillator must remain stable while sustaining an arc drawn from the dee face — a deliberate spark test simulating in-tank discharges; (3) RF plate voltage not excessive; (4) phasing capacity near the calculated value.
Source quote & editorial note
The dee voltage must be at least twice the d.c. plate voltage. 2. The oscillator must be stable enough to sustain an arc drawn from the dee face (simulating discharges in that region). ... 4. The phasing capacity, as calculated in MacKenzie's report ..., should be as near [the calculated value] as possible.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 12
Editorial note, tabletop extrapolation: The requirement transfers as a criterion, not a procedure: the planned LDMOS amplifier must demonstrably survive dee-side arcs before it is trusted in vacuum, where conditioning sparks are guaranteed. For solid-state that means proving the protection chain - VSWR trip, drain clamping, fast drive-cut (dg-338, dg-679) - against controlled fault tests, not drawing an open arc onto an unprotected amplifier the way the 1947 tube crews could.
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Feedline lengths hide in-band resonances: an overlong plate line developed a resonant dip in the dee-voltage response, worsening with length, and a 1-2 inch change tilted the response across the band. Choose line lengths empirically for flat response, starting from the calculated values.
Source quote & editorial note
A deviation of an inch or two one way or the other will cause this response to rise or fall at either end of the range.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 13
Editorial note, tabletop extrapolation: Even a fixed-frequency amateur system inherits this through the amp-to-dee coax and its stray resonances: sweep the ASSEMBLED feed system, not just the cavity, and choose line lengths from the measured input impedance and matching bandwidth at the operating frequency. The cited inch-scale sensitivity belongs to that swept resonant feedline - your system's sensitivity scale comes out of your sweep.
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Check every ancillary choke and feed for self-resonance near the operating band: the model's filament-heating chokes were resonant at 18 mc - in-band - which the report suspected as the cause of a sharp dee-voltage drop near that frequency.
place choke self-resonance >= ~3x operating frequency (18 mc in-band fault -> 60 mc fix)Source quote & editorial note
the original ones used were resonant at 18 mc, which may account for a sharp drop observed in the dee voltage as this frequency was approached.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 13
Editorial note, tabletop extrapolation: Filament, bias, meter, and interlock leads entering the tank all need chokes whose behavior is MEASURED across the operating band - impedance or insertion loss over the whole band, not just the self-resonant frequency - because a choke resonant near the operating frequency silently loads the dee.
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Measure inaccessible element capacities by bridge subtraction: measure with the moving element in and out and subtract to isolate each element, then series-combine. The model's rotary-condenser swing: 1370 uuf max to 50 uuf min - printed as ratio 27.6, though 1370/50 computes to 27.4 (a source arithmetic slip or a rounded input; dg-501 pattern).
C_element = C_assembled - C_element_removed; series C = 1/(1/C1+1/C2); swing 1370/50 uuf = 27.4 (source prints 27.6)Source quote & editorial note
Ratio Max-capacity/Min-capacity = 1370/50 = 27.6
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 14
Editorial note, tabletop extrapolation: Same differential technique as Koeth's Rutgers dee-capacitance note in this collection: an LCR meter plus one disassembly step estimates the selected lumped capacitances in a tank model - subject to fixture and stray-capacitance errors, which set how many elements one subtraction chain can honestly resolve.
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Power and efficiency measured with no RF instrumentation in the power path: kill the RF by shorting the plate line to the housing (all DC input then appears in the triode plates), calibrate one pyrometer spot per plate against known DC input, then read true plate dissipation under RF from the calibration curve; the lab-built diode probe voltmeters were honestly rated +/-5-10 percent.
P_out = P_in(DC) - P_plate(from thermal calibration); probe error assumed +/-5 to 10%Source quote & editorial note
the errors in readings should be assumed to be +/- 5 to 10 percent. ... For power measurements, a Leeds and Northrup optical pyrometer, Cat. #8622-C, was used to observe plate dissipation in the triodes. ... In using the optical pyrometer, one spot on one plate of a triode was selected as the comparison point. The excitation was removed by connecting the plate line to the oscillator housing so that no r.f. currents would flow and all the power input would appear in the plates of the triodes.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 8
Editorial note, tabletop extrapolation: The thermal-reference trick survives translation with a defined reference plane: calorimetry on the LDMOS heatsink (or dee cooling loop) calibrated at DC gives THE HEAT INTO THAT PATH - write the full power balance (P_RF_out = P_DC - P_device - other paths) with matched thermal boundary conditions and steady state before quoting an output power; and publish instrument error bars the way Anderson did.
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A scale model's known infidelities must be listed with the results: the substitute 304-TL triodes have much larger internal inductance than the final 9C21s, and early power measurements were found very inaccurate due to plate-capacity differences between the two 304-TLs and the consequent difference in RF current distribution.
Source quote & editorial note
the inductance inherent in the 304-TL triodes is large compared with that in the 9C21 triodes to be used in the final oscillator. ... The power measurements at this stage in the experiments were found to be very inaccurate due to differences in plate capacity on the two 304-TL triodes and the consequent difference in distribution of r.f. currents.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 12
Editorial note, tabletop extrapolation: When bench-testing a next machine's RF with a stand-in amplifier or without the real chamber wall, write the fidelity caveats into the test log - the model predicts the cavity, not the parts that were substituted. (The filament-line impedance discontinuity previously listed here is dropped pending re-read - the scan discusses filament-line length effects but not that specific claim.)
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Model cyclotron acceleration as kick-plus-coast: an impulsive energy change at each gap azimuth followed by coasting on the static field map to the next gap - the source's validated approximation for its studied configuration; the kick is phase-dependent: dE = q*V_peak*T(phi,E)*cos(phi) (T the transit-time factor), or exactly q*INT(E.dl) at the crossing phase.
per crossing: dE = q*V_peak*T*cos(phi) (NOT an unconditional q*V_gap); r, p_r unchanged at a thin radial-gap kick; coast on the static map between gapsSource quote & editorial note
the acceleration can be considered to good approximation as being a simple impulsive change in the energy of the particle at the azimuth of the accelerating gap
Editorial note, tabletop extrapolation: The core architecture for CYCLOPS-lite - thin-gap kicks alternating with magnetic coasting maps - with phase carried as a dynamical variable from the first line of code; MSUCP-12's analytic gap field upgrades the kick to a distributed one when transit time matters, and a comparison against distributed-gap tracking on the actual geometry is the validation step, not the 1961 result alone.
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Build the orbit toolchain as two codes sharing one field representation: a closed-orbit finder using a linear transfer-matrix procedure, and a general tracker with median-plane-exact equations of motion, acceleration switchable on or off, the field supplied as tables of Fourier coefficients versus radius.
B(r,theta) = B0(r) + sum_j [H_3j(r) cos(3j*theta) + G_3j(r) sin(3j*theta)] - the 3j-only form is the source's perfect-120-degree-symmetry special case; a real as-built field needs the full integer-harmonic seriesSource quote & editorial note
The Fixed Point Code locates closed orbits by means of a highly effective linear transfer matrix procedure, the General Orbit Code tracks arbitrary orbits as desired either with or without acceleration effects. For both routines the magnetic field is described by tables of Fourier coefficients as functions of radius; each uses equations of motion which are exact in the median plane.
Editorial note, tabletop extrapolation: This is the CYCLOPS architecture in embryo (the lineage the planned "CYCLOPS-lite" copies); a next machine's tracker should likewise separate the equilibrium-orbit /tune solver from the general tracker, sharing one Fourier-vs-radius field representation fed by FEMM.
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To map the phase-space topology at an energy, locate the unstable fixed points first, then launch orbits displaced slightly from them - along the transfer-matrix eigenvector directions - and integrate both forward AND backward in time: the trajectories trace the stable and unstable manifolds (separatrices where the map is near-integrable), far cheaper than blanketing the plane with orbits.
Source quote & editorial note
the general orbit code is employed to trace forward and backward in time orbits with initial conditions displaced slightly from the unstable fixed points.
Editorial note, tabletop extrapolation: Directly reusable in a Python tracker (a symplectic or invertible integrator makes the backward branch trustworthy); the efficient way to draw the r-pr stability picture near resonances - cross-check with a scatter of ordinary orbits where the manifolds tangle, since in a nonintegrable map they can intersect and form stochastic layers rather than clean boundaries.
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Median-plane-dominant tracking is a justified economy in the source's context: the small axial beam space holds surviving particles where the field's z-dependence is quite linear - so linearized vertical dynamics suffice, and the source spot-checked with off-plane trial runs.
Source quote & editorial note
the small axial beam space in a cyclotron constrains the particles to move in a region where the z dependence of the field is quite linear.
Editorial note, tabletop extrapolation: Build the next machine's first tracker around (r, pr, E, phase) PLUS linearized (z, pz) from the outset - the aperture does not hold particles near the median plane, it deletes the ones that leave, so vertical tune, resonance crossings and the physical aperture decide transmission. Full-3D spot checks then benchmark the linear model over representative launches; a handful of them is the check on the linearization, not a license to omit z.
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Orbit studies can run on measured scale-model fields long before the machine exists: the B26.1R field came from an 8.75-inch model magnet, radially scaled by 64/8.75 to the full machine, its average field modified to isochronism, its flutter smoothed of measurement errors, harmonics above 99 dropped as negligible, and perfect 120-degree symmetry assumed in the Fourier analysis.
r_machine = r_model * (64/8.75); field tabulated at radial increment 0.0080924 cyclotron units (1 cyc unit = E0/(q*B0*c))Source quote & editorial note
modifications to <B> to yield isochronism out to the 29th entry in the radial table and with the flutter field modified by a small amount to smooth out effects of measurement errors. In addition, Fourier components of argument greater than 99 have been dropped since these components are sufficiently small to have a negligible effect on the particle motion. The radial spacing of the table entrys is interpreted as increased by the factor 64/8.75 corresponding to the ratio of pole diameters ... In the Fourier analysis the measured field has been assumed to have perfect 120 [deg] symmetry.
Editorial note, tabletop extrapolation: The historical analog of the CadQuery->FEMM->field-map pipeline, plus the habit worth copying exactly as MSU practiced it: document every cleanup applied to the field the tracker ate. For an as-built machine, keep the RAW map too - symmetrizing and smoothing erase the very error harmonics that drive resonances - and use the cleaned copy only for idealized nominal studies; check magnetic similarity (saturation behavior) before radially scaling any model field.
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A first-harmonic (cos theta) field component of only ~1% radically reorganizes the phase plane of a cyclotron running near nu_r = 1 — the computational demonstration behind the traditional "great respect" for first-harmonic errors in cyclotron design lore.
bump B1(r)*cos(theta + 2.8 deg), peak B1 = 139 G on 13.6 kG base (~1%), radial profile per bump-coil geometry (Table II)Source quote & editorial note
The powerful effect of a cos 0 field component in a cyclotron ... is clearly evidenced by the large changes in the phase plot which result when the small 1% bump is added.
Editorial note, tabletop extrapolation: Cuts both ways near nu_r = 1: the demonstration is why first-harmonic errors get 'great respect' - so Fourier-analyze the candidate field map and track the measured B1(r) through the local tune to learn what YOUR machine's shim asymmetries cost; and a deliberate bump coil is a powerful orbit-steering experiment once its ampere-turns are sized from that same analysis, not assumed few-turn-cheap.
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In this first-harmonic, nu_r-near-1 regenerative-extraction model, extraction works by making the stable centre of phase space jump: the field bump causes the equilibrium orbit and an unstable fixed point to merge and vanish as energy rises, so the surviving stable point is elsewhere - the beam suddenly finds itself executing a large-amplitude coherent radial oscillation, which is what increases the extraction step. [Corrected 2026-08-23: earlier text said that amplitude 'is the turn separation'. The step at the septum also depends on betatron phase, the energy gain per turn, the separatrix geometry, septum azimuth and tune; compute it with a tracker.]
Source quote & editorial note
introduction of the field bump has caused a discontinuous jump in the location of the central stable orbit in the phase diagram
Editorial note, tabletop extrapolation: The conceptual mechanism to have in hand before a regenerative extraction attempt on a next machine: it needs nu_r to pass unity with a controlled first harmonic, both of which a FEMM-fed tracker can compute for a candidate pole design. It is one extraction method - electrostatic deflection, stripping, or simply large natural turn separation do not require crossing nu_r = 1. [Note revised 2026-08-23: earlier wording read as if this were prerequisite to any extraction.]
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State the beam-optics acceptance criterion in phase-space language: performance is good if a beam-sized ellipse remains an ellipse through the system - stretching and rotation are acceptable (downstream lenses accommodate them, within their aperture), twisting and filamentation are not: they dilute the coarse-grained (projected) emittance in a way no simple lens undoes.
Source quote & editorial note
stretching and rotation are fine but not twisting, filamentation, etc.
Editorial note, tabletop extrapolation: The right figure of merit for any next machine's beamline or extraction simulation - track a grid of particles and judge the deformed shape, not just the centroid. Five to two dozen particles sufficed in 1961 for the smooth cases; check convergence by refining the grid where the map is nonlinear, since a sparse grid can miss filamentation entirely.
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Distortion bookkeeping: motion of the beam spot driven by flow-rate gradients on a fixed static plot (the "static effect") stretches, bends, shears, and filaments the beam; motion driven by the plot itself shifting with energy (the "acceleration effect") moves the beam without deforming it. Design rule: program the turns to avoid flow-gradient regions — especially near unstable fixed points.
Source quote & editorial note
The essential design requirement of such a system is a turn program which avoids regions of large flow rate gradient in the static phase space.
Editorial note, tabletop extrapolation: The doctrine transfers to schemes where a static phase-plot analysis applies: superimpose the accelerated beam path on static phase plots (cheap tracker post-processing), identify the large-flow-gradient regions - especially near unstable fixed points - and compare candidate turn programs by accelerated tracking. Crossing faster reduces exposure to a bad region but can excite other resonances non-adiabatically, so test, don't assume.
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Energy gain per turn strongly conditions resonant extraction quality: the report concludes that volts-per-turn substantially below the designed 280 keV/turn 'would result in sharp reduction of both extraction efficiency and optical quality' (its comparative runs at half (140), design (280), and double (560) kV per turn found the high-voltage case notably well behaved) [2026-08-28: the queued scan re-read was delivered upstream; the placeholder is replaced with the report's comparative values.]
turn separation achieved: 0.006 cyc units between the 14th and 15th turns (hand-corrected figures) for a 0.002 cyc-unit beam at 280 kV/turnSource quote & editorial note
volts per turn substantially lower than the designed 280 kev/turn would result in sharp reduction of both extraction efficiency and optical quality.
Editorial note, tabletop extrapolation: The quantitative ancestor of 'dee volts buy extraction': the reference machine's uncalibrated ~1.3 kV dee is one reason it is internal-beam-only, and a next machine's 5-13 kV target is what would make an extraction scheme thinkable - thinkable, not feasible, until the turn separation (delta_r ~ r*delta_E/2E), phase width, septum clearance, tune and bump design are actually computed.
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Simplify the accelerating waveform first, validate later: square-wave energy gain was used deliberately to decouple (E,t) from (r,pr) phase space; a closing check with sinusoidal voltage shifted the final beam position but left distortion essentially unchanged, adding only ~30 keV spread across a beam-sized area from differential phase slip.
sinusoidal check after 8 turns: 62 keV total spread over 5 tracked particles (~30 keV across a beam-sized subarea), 55 deg mean phase driftSource quote & editorial note
The sinusoidal voltage, it is seen, shifts the final position of the beam spot but has almost no effect on the distortion.
Editorial note, tabletop extrapolation: A permission slip for CYCLOPS-lite staging — start with constant energy gain per gap to get the radial dynamics right, then add cos(phi) gain and phase slip as a second-stage refinement, checking that conclusions survive.
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Validate the tracker against hand analytics at every opportunity: the gap-crossing-resonance amplitude (generated because each energy kick shifts the applicable equilibrium orbit while r, pr stay fixed) was computed by hand from tabulated orbit separations and linear mappings, and reproduced the tracked grid's amplitude and phase. Field asymmetry can spoil the ideal first-order cancellation of the two gap kicks - compute and vector-sum the two excitations using the actual half-turn maps, gap voltages, RF phases, geometry and closed orbit. [Corrected 2026-08-23: earlier text said this happens 'only' then; symmetric iron is necessary for cancellation, not sufficient - equal gap voltages and phases, symmetric gap geometry and a centred orbit are also required.]
amplitude generated per crossing = -(shift of E.O. between E and E+dE); example chain 0.00126 at 138 deg -> 0.00161 at 28 deg over one turn (Table III)Source quote & editorial note
the result is seen to fairly accurately predict the actual amplitude and 0 of this point of the grid
Editorial note, tabletop extrapolation: Two lessons - build point analytic cross-checks into a next machine's tracker test suite (transfer-matrix estimates against tracked orbits), and note that in the idealised 180-degree-symmetric two-dee case this particular excitation cancels to first order; check the real machine with its measured field, RF balance and gap geometry rather than assuming it. [Note revised 2026-08-23: earlier note called the physics 'benign' for a symmetric tabletop field.]
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Let the computation overrule the folklore: the study found beams entering the extraction region approximately centered on the equilibrium orbit 'behave as well or better' than beams entering with substantial displacement - the computational basis and the earlier proposal this revised are the report's context (scan re-read queued).
Source quote & editorial note
beams entering the extraction region approximately centered on the equilibrium orbit behave as well or better than beams entering with substantial displacement.
Editorial note, tabletop extrapolation: The project-level lesson for a next machine — run the cheap simulation before committing hardware to any orbit-dynamics intuition, including intuitions published by people as good as Blosser and Gordon.
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A closed-form, size-independent solution exists for the cyclotron dee-gap field (Schwarz-Christoffel, per Murray & Ratner 1953 with corrections): for zero-thickness semi-infinite plate pairs at y = +/-h, tips at x = +/-k, potentials -/+V0, the median-plane field and potential are two-line formulas once one transcendental equation is solved. Geometry caution: k is the HALF-gap and h the HALF-aperture (plate tips map exactly to x = +/-k; re-derived from eq. 1 during extraction — the Fig. 1 scan invites misreading the full gap as k).
median plane (eqs. 6-8): E_x(x,0) = (V0/h)*sech(X1)/(1 + alpha*sech^2(X1)); V(x,0) = sign(x)*(2*V0/pi)*arccos(sech(X1)); with X = pi*x/(2h) = X1 + alpha*tanh(X1); alpha = (1-a^2)/a^2; a from (pi/2)*(k/h) = arccosh(1/a) + sqrt(1-a^2)/a^2. E_y = 0 on the median plane; E_x even, V odd in x. (Report writes E = +dV/dx — fix sign on implementation.)Source quote & editorial note
This paper presents in summary formulas for the computation of electric fields and potentials of an idealized cyclotron dee geometry.
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 6
Editorial note, tabletop extrapolation: TRACKER SEED (flagged): this is directly implementable as the gap-field model in the tiny and the next machine's Python trackers — roughly ten lines plus a Newton solve — replacing or validating FEMM electrostatic maps. Identify 2h with the dee aperture, 2k with the dee-to-dummy-dee gap, 2V0 with the full dee-to-dummy-dee voltage (a grounded dummy dee is the same solution shifted by a constant, V0 = V_dee/2).
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The same solution gives the full off-median-plane E field — the ingredient needed for electric (gap) focusing models: E_x and E_y anywhere in the aperture follow from two coupled transcendental equations in (X1, Y1). Beal tabulated only the median plane, but eqs. 1-5 contain the whole 2-D field.
physical convention (E = -grad V): E_x = -(V0/h)*Xv/(Xv^2+Xu^2); E_y = -(V0/h)*Xu/(Xv^2+Xu^2) with the report's Xv, Xu, F as tabulated (the report prints the positive-gradient convention - flip the sign before tracking); potential v = arccos(cos(Y1)/F) needs the antisymmetric branch for x < 0 (plain arccos returns the same value both sides); verify an implementation against finite differences of VSource quote & editorial note
Therefore, equations 2 and 4 coupled with equations 3 and 5 can be used to determine the electric field and potential at a point X, Y of the dee region.
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 5
Editorial note, tabletop extrapolation: E_y(x,y) is what a tracker needs for the Rose/Wilson electric gap-focusing term - available analytically at any point, no field map required. Whether that term dominates first-turn axial stability on a sub-kV machine is for the axial-stability calculation to say; implement, verify against finite differences, and let the tracking decide.
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Solve the gap-field transcendental equation with Gordon's iteration: Murray-Ratner's original converges slowly for small alpha and not at all for large alpha, while Gordon's Newton linearization of tanh(X1) 'was found to work well for all cases', with local quadratic convergence and the source's two-branch initial guess (X1 ~ X/(1+alpha) for small X1; X1 ~ X - alpha for large X1).
eq. 9: X1_new = [X - alpha*tanh(X1c) + alpha*X1c*sech^2(X1c)] / [1 + alpha*sech^2(X1c)], X1c the current iterate; initial guess X/(1+alpha) or X-alpha by branchSource quote & editorial note
The iteration process suggested by Murray and Ratner for calculation of X1 converges slowly for small values of a, and does not converge at all for large a. An iteration process, described below, suggested by M.M. Gordon was used and was found to work well for all cases. ... This iteration is Newtonian in character such that if a given X1 has an error of order e, then X1 given by equation 9 will have an error at order e squared. ... X1 ~ X/(1+a) for X1 small ... X1 ~ X - a for X1 large.
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 7
Editorial note, tabletop extrapolation: Copy the iteration and its initial-guess branch into the tracker's field routine; iterate to a set tolerance - quadratic convergence is local, so the branch guess is what makes it robust - cheap enough to call per integration step, or use once to build a spline.
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The peak accelerating field at the gap center - the median-plane centerline value in this idealized geometry - saturates at V0/h, set by the APERTURE, not the gap: E(0) = (V0/h)/(1+alpha) = 0.994, 0.948, 0.870, 0.654, 0.489, 0.378, 0.306, 0.253, 0.216 times V0/h for k/h = 0.1 through 3.5. Narrowing the gap below the aperture height buys almost nothing.
E(0) = (V0/h)/(1+alpha), exact from eq. 6; k->0 limit E_x = (V0/h)*sech(pi*x/(2h))Source quote & editorial note
Table 1. k/h = 0.1: at x/h = 0, E/(V0/h) = 0.99388 [values verified against page image]
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 11
Editorial note, tabletop extrapolation: Sets the ceiling on CENTERLINE gap field for a dee redesign: with a 1-inch aperture (h = 0.5 in) and 2.5 kV dee-to-dummy, the median-plane peak cannot exceed ~2 kV/cm however tight the gap. Two cautions: local surface fields at electrode edges run above the centerline value - breakdown cares about those (dg-353) - and widening the aperture trades centerline field for beam height by the table's factors, not one-for-one at every k/h.
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The gap field leaks far under the dees: E falls to half its central value only near x/h ~ 0.85 (narrow gap) and the potential reaches 90% of V0 only around x/h ~ 2, so the effective accelerating gap is on the order of the full aperture 2h, not the physical gap 2k. Hard-edge gap models mis-time the kick and miss the field a particle still feels one aperture-height into the dee.
narrow-gap half-width x(E = Emax/2) = (2h/pi)*arccosh(2) = 0.838*h; V/V0 = 0.90 near x/h ~ 1.6 for k/h = 0.1 (analytic narrow-gap limit; the table's 0.73760 at x/h = 1.0 and 0.94468 at 2.0 bracket it), moving toward ~2.6 by k/h = 1.5Source quote & editorial note
Table 1, k/h = 0.1: V/V0 = 0.73760 at x/h = 1.0, 0.94468 at 2.0 [verified against page image]
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 11
Editorial note, tabletop extrapolation: Transit-time factors and gap-crossing phase errors must be computed on this extended profile - and whether a delta-kick model is adequate is the transit parameter's call: evaluate omega*L_eff/v for the actual first-turn velocities and the ~2h-long field region, and let that number, not a blanket assumption, decide when the distributed kick is needed.
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Do not use the parallel-plate V/d estimate for dee-gap fields: for wide gaps (k/h >= 2) the mid-gap field sits ~25% below 2V0/(2k) because flux escapes through the aperture (k/h = 2.0: 0.378 vs 0.5 naive; 3.5: 0.216 vs 0.286), and the field maximum moves off-center to just inside the dee tips (x/h ~ k/h - 0.7); for narrow gaps the uniform-field picture fails entirely and V/d wildly overestimates the peak.
wide-gap plateau E ~ 0.75*(V0/k); max off-center for k/h >= 2: E_max at x/h = 1.2, 1.6, 2.2, 2.8 for k/h = 2.0, 2.5, 3.0, 3.5 [from Table 1]Source quote & editorial note
Table 1, k/h = 2.0: E/(V0/h) = 0.37823 at x/h = 0, maximum 0.38966 at x/h = 1.2 [verified against page image]
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 16
Editorial note, tabletop extrapolation: Kills the tempting E = V_dee/gap for FIELD estimates on a next machine's geometry, where gap and aperture are the same order (k/h ~ 1) and neither limiting approximation holds - use the formulas or tables for the profile. Energy gain is a different question: absent transit-time effects the work across the gap is q*V0 whatever the profile; the profile changes transit-time factors and where field concentrates - and the surface fields at electrode edges, which the breakdown margin actually cares about (dg-353, dg-1028).
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Table 1 is a ready-made verification dataset: E/(V0/h) and V/V0 at x/h = 0 to 5.0 in steps of 0.2, five significant figures, for nine gap ratios k/h = 0.1, 0.3, 0.5, 1.0, 1.5, 2.0, 2.5, 3.0, 3.5 — computed on MISTIC (D. A. Johnson's fixed-point program), the same machine as the MSUCP-9 orbit codes.
benchmark anchors: E(0)/(V0/h) = 0.99388 (k/h=0.1), 0.87049 (0.5), 0.65448 (1.0), 0.48916 (1.5), 0.37823 (2.0), 0.21623 (3.5); V/V0 at x/h=1.0: 0.73760, 0.70319, 0.60615, 0.48545, 0.38270, 0.21862 respectivelySource quote & editorial note
Table 1 gives values of electric field and potential for a wide range of dee gap arrangements. [tables span PDF pages 11-19]
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 11
Editorial note, tabletop extrapolation: Unit-test targets for the tracker's gap-field routine AND an independent check on FEMM electrostatic runs: model the same idealized geometry once and agree within a DOCUMENTED convergence tolerance - set by a mesh/domain convergence study against the table's demonstrated accuracy - before trusting FEMM on the real electrode shapes; the table's five printed digits are formatting, not a five-digit acceptance criterion.
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Know the idealization's edges before leaning on it: the solution is 2-D (infinitely long straight edge — no dee-tip curvature, corners, or azimuthal variation), zero plate thickness, semi-infinite plates, electrostatic (quasi-static per RF cycle), no space charge, and symmetric +/-V0 drive. Beal's MISTIC computations covered alpha < 4, i.e. k/h < ~3.77, though the formulas themselves have no such limit.
Beal's MISTIC computations covered alpha < 4; the alpha-to-geometry conversion needs the source's definition re-read before quoting a k/h bound (the previously printed formula evaluated to ~2.06, not its own claimed 3.77 - scan re-read queued; the likely intended form is k/h = (2/pi)*(arccosh(sqrt(1+alpha)) + sqrt(alpha*(1+alpha))), which gives 3.77 at alpha = 4)Source quote & editorial note
A fixed point computer program written by D.A. Johnson for use on MISTIC was used to calculate the above equations for Ex and Vx at the point (X,0) with a<4.
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 8
Editorial note, tabletop extrapolation: For use on a next machine, the real deviations to check against FEMM are finite dee thickness, the rounded tip, and the curved gap line near the source at small radius - run the comparison over the actual geometry rather than assuming the analytic solution's quality at any radius; near center the ion-source chimney dominates the field regardless.
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Size shielding around the SECONDARY radiation: the beam's interaction with the target, the accelerator structure, or the shielding itself 'most often' determines the type and magnitude of shielding required - and primary-beam containment is still assessed wherever extraction, a thin window, or an abnormal loss could make ions accessible.
shield for secondaries (X-rays, neutrons) produced where the beam is lost, not for the primary ionsSource quote & editorial note
Secondary radiations produced as a result of the interaction of the primary beam with a target, portion of the accelerator, or the shielding most often determine the type and magnitude of the shielding.
Editorial note, tabletop extrapolation: For the reference machine and a next machine the primary protons stay inside the chamber in normal operation, so the external radiation field is dominated by secondaries - dee-gap electron bremsstrahlung today; reaction products (the 11B(p,alpha) alphas) and any (p,n)-capable contaminants joining the inventory at a next machine's energies.
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Direct bremsstrahlung from a heavy projectile scales as ~1/M^2 of its mass and is usually insignificant; the X-ray sources that matter on a positive-ion machine are instead - the manual's list - characteristic X-rays from inner-shell vacancies, nuclear deexcitation, and bremsstrahlung from stray electrons.
bremsstrahlung ~ 1/M^2 -> proton bremsstrahlung negligible; hazard = characteristic X-rays + stray-electron bremsstrahlungSource quote & editorial note
The bremsstrahlung is approximately inversally proportional to the M2 where M is the mass of the incident particle. It is therefore usually insignificant for heavy particles.
Editorial note, tabletop extrapolation: Supports the program's standing model that dee-voltage electrons, not the proton beam's own bremsstrahlung, dominate the X-ray hazard on a sub-MeV proton cyclotron. Dominant is not sole: characteristic X-rays and any nuclear gammas from targets keep their own lines in the survey plan.
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Even when characteristic/soft X-radiation poses a small shielding problem - the source's word - plan the INSTRUMENTATION for it: survey meters must be able to detect and measure the soft component, whose existence and importance the source stresses even at low incident-particle energies.
instrument response must extend down to the soft X-ray band even when shielding is trivialSource quote & editorial note
This radiation is soft and the shielding problem small. It is however important to be remindful of its existance and importance even at low energies of the incident particle. Instruments must be able to detect and measure this soft radiation.
Editorial note, tabletop extrapolation: The reference machine's survey problem in one sentence: a ~10 kV dee makes sub-10-keV photons that ordinary GM/ion-chamber walls partly block — pancake/thin-window instruments are required to even see the hazard (pairs with the Ch. VI 150-keV response rule).
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Lacking design detail, the Army manual estimates the stray-electron X-ray source term of a positive-ion accelerator by assuming a reverse-directed electron current of 0.2*I (I = ion current) accelerated through 1/3 of the terminal voltage - an assumption the authors themselves label unreliable, offered to show that even a rough guess predicts "very considerable" X-ray production, not as a bounding figure. [Corrected 2026-08-23: an earlier version and its note presented the 0.2*I / V/3 pair as a bounding recipe. The source presents it as the opposite - an unreliable assumption that nonetheless gives a large number - and using it as a ceiling is under-conservative.]
I_e(back-streaming) ~ 0.2 * I_ion at E ~ V_terminal/3 - a rough historical source-term ASSUMPTION, not a boundSource quote & editorial note
If we assume that the ion current "I" results in a reverse directed electron current of magnitude 0.2*I that is accelerated through 1/3 the terminal voltage we would usually get a very considerable x-ray production.
Editorial note, tabletop extrapolation: Use this only as the lesson that stray-electron X-rays exist wherever there is RF voltage and vacuum, never as a ceiling. For a next machine's hazard analysis, plan around at least the peak-to-peak dee voltage as the electron impact energy - a planning floor, not a physical ceiling, since multi-transit RF processes can exceed single-gap figures - and let the measured X-ray endpoint from the survey be the authority the analysis answers to.
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As a rough shielding estimate for a heavy-ion accelerator's stray-electron X-rays, provide the shielding that would be required at 90 degrees from the beam axis of an ELECTRON accelerator of the same beam current and energy; ion-machine shielding "may not be so much less" than the electron case.
shield(ion machine) ~ shield(electron machine, 90 degrees, same I and E)Source quote & editorial note
As a rough estimate we offer that shielding which is required at 90 deg from the beam axis of an electron accelerator, with the same beam current and energy.
Editorial note, tabletop extrapolation: The conservative sizing pattern for a product-machine enclosure: bound the ion machine by an equivalent electron accelerator at the same current and at the maximum electron energy credible in the machine (at least peak dee-to-ground; dg-1036), then read the required thickness from electron-accelerator shielding data at that energy and verify by survey. The reference machine's chamber walls stopping its soft X-rays is a measured fact about ~10 kV operation, not a rule to inherit.
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Thick-target X-ray conversion efficiency at 0.5 MeV: stopping electrons convert 0.265% of beam power to X-rays in water, 0.59% in Al, 1.34% in Fe, 4.77% in W, 6.21% in U — efficiency rises with Z and with energy (at 1 MeV, W gives 7.63%).
f(X-ray) at 0.5 MeV: H2O 0.265%, Al 0.59%, Fe 1.34%, W 4.77%, U 6.21% of electron beam power (Table II-1)Source quote & editorial note
The % of the electron energy that is converted to X-rays upon complete stopping of the electrons ... 0.5 ... 0.265 ... 0.59 ... 1.34 ... 4.77 ... 6.21
Editorial note, tabletop extrapolation: Sets the scaling logic - conversion efficiency rises with Z and with energy - even though the table starts at 0.5 MeV. At dee-voltage energies the Z-trend persists in direction, but the table's factors do not extrapolate cleanly (characteristic lines and backscatter enter), so the design instinct is what transfers: land stray electrons on LOW-Z surfaces (aluminum, graphite) rather than tungsten or steel, and let the survey measure the actual benefit.
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At very low electron energy (few keV), bremsstrahlung is emitted with the intrinsic angular distribution of a radio antenna — intensity GREATEST PERPENDICULAR to the electron direction — the opposite of the MeV-range forward peaking.
few-keV electrons -> dipole pattern, max at 90 degrees to electron path; MeV electrons -> forward-peakedSource quote & editorial note
At very low electron energy (few keV), the intrinsic angular distribution is the same as from a radio-antenna, i.e., the intensity is greatest perpendicular to the direction of the electron beam.
Editorial note, tabletop extrapolation: For dee-gap electrons, the INTRINSIC few-keV emission peaks sideways to the electron path - a reason to survey all around the chamber midplane and its windows rather than along any assumed axis. What actually leaks where folds in scattering, multiple electron directions, self-absorption and wall attenuation - so the survey pattern, not the dipole formula, is the finding.
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The chapter's quantitative machinery - forward intensity I(0) = 723*tau*(T+0.511)^2*T*i/d^2 * ln(3250t/ln(183 Z^-1/3)), dose R(0) = 2.604e11*(mu_k/rho)av*(same), and the concrete dose-rate table scaled by W/R^2 - is tabulated for its 5.5-40.5 MeV electron range; below that range the chapter's tables simply do not reach, and the source-term assumptions are the part that generalizes.
D(behind x cm concrete) = TableII-3(T,x) * W(kW)/R(m)^2, tabulated 5.5-40.5 MeV; below the table's range use X-ray-tube output dataSource quote & editorial note
The dose rate D in rads per hour is obtained by multiplying the values in the Table by W/R2, where W is the electron beam power in kwatt and R is the distance in m to the detector from the X-ray target.
Editorial note, tabletop extrapolation: Scope honestly: this is the collection's only full X-ray shielding workflow, and its tables start at 5.5 MeV. For the 5-13 kV dee upgrade none of it applies numerically - take source terms and barriers from X-ray-tube shielding data (NCRP-49-class R/mA-min at 1 m vs kVp), keep the chapter for its structure (source term, then barrier, then verify), and treat the 0.2*I stray-electron assumption as a lesson, not an input (dg-1036).
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Proton cross sections for nuclear interaction fall steeply below about 0.1 MeV because of the Coulomb barrier — but the light-nuclei exceptions the source waves off are exactly the targets amateurs use: 7Li(p,alpha) and 11B(p,alpha) run at measurable rates well below 100 keV. Evaluate the actual target isotopes before making radiation assumptions. [Corrected 2026-08-20: an earlier version endorsed the source's "nuclear-reaction-free" conclusion; nuclear data contradict it for light targets.]
sigma(p,nuclear) ~ 0 below ~0.1 MeV; barrier penetration grows sharply with E thereafterSource quote & editorial note
Because of the Coulomb barrier, proton cross sections for nuclear interaction are negligible below about 0.1 MeV. In light nuclei there are some exceptions which are of little interest here.
Editorial note, tabletop extrapolation: Closes the neutron question for the reference machine at ~150 keV-class energies EXCEPT via the light-nuclei exceptions the chapter waves off - and the exceptions differ in kind: the deliberate 11B(p,alpha) target yields charged alphas and gammas, not neutrons directly (the indirect path to check is secondary (alpha,n) on nearby low-Z materials); deuterium contamination is the direct neutron path, D(d,n) being thresholdless (see Ch. IV rule).
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(p,n) reactions are threshold-gated: the n-p mass difference (0.78 MeV) sets a floor, thresholds are of the order of an MeV for light and low-intermediate nuclei, and neutron emission becomes the dominant channel about 1 MeV above threshold - the manual's rough generalization; resonances and channel competition make real cases isotope-specific.
E_thr(p,n) > 0.78 MeV (stable targets), ~MeV for light nuclei; n-channel dominant at E > E_thr + ~1 MeVSource quote & editorial note
For light and low-intermediate nuclei, (p,n) thresholds are of the order of an MeV. Neutron emission becomes the dominant reaction when the incident particle energy exceeds the threshold by about 1 MeV.
Editorial note, tabletop extrapolation: The threshold-audit pattern for every machine energy bump: list materials the beam can strike, look up (p,n) thresholds, and confirm E_beam sits below them. At 170 keV (a next machine) every (p,n) channel on stable nuclei is closed by >600 keV of margin; the audit must be redone if energy ever approaches ~1.9 MeV (7Li(p,n) threshold 1.88 MeV).
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Photoneutron thresholds run 6-19 MeV for nearly all nuclei with ONE trap: deuterium at 2.23 MeV — hydrogenous (water-containing) materials with natural deuterium are the exception to "low-Z is safe around photon flux," so audit D-bearing materials wherever multi-MeV photons exist.
E_thr(gamma,n): H-2 2.23 MeV; C-12 18.7; O-16 16.3; Cu-63 10.9; Pb-208 7.44 (Table III-2)Source quote & editorial note
H2(gamma,n)H1 ... 2.23 ... C12(gamma,n)C11 ... 18.7 ... O16(gamma,n)O15 ... 16.3
Editorial note, tabletop extrapolation: At the reference machine's photon energies (keV-class bremsstrahlung) every channel in the table is closed. Two honesty caveats for reuse in hazard analyses: 9Be sits below the deuterium trap (S_n = 1.665 MeV, IAEA NDS/AME, retrieved 2026-08-25), so beryllium joins heavy water on the audit list wherever multi-MeV photons exist; and reaction gammas can exceed the projectile energy - 11B(p,gamma) capture emits ~16 MeV photons at small cross-section, so a p-B11 machine's analysis must bound that two-step channel rather than declare photonuclear reactions impossible.
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Neutron shielding is slow-down-then-capture in the manual's account - light nuclei (hydrogen) dominate energy loss, so hydrogenous concrete outperforms lead for neutrons - and the quoted rule of thumb: a facility shielded in concrete for X-rays 'generally contains adequate neutron shielding in the process', with the serious problem arising where the neutron hazard exceeds the photon hazard: proton and deuteron machines, the quote's own caveat.
concrete X-ray shield ~ adequate neutron shield (rule of thumb, <30 MeV); capture gammas must be shielded in turnSource quote & editorial note
it is a fairly accurate rule of thumb that for energies of interest here, the facility generally contains adequate neutron shielding in the process. The more serious neutron shielding problem occurs when the X- and gamma ray hazard is exceeded by the neutron hazard. Proton and deuteron accelerators are cases in point.
Editorial note, tabletop extrapolation: For any future neutron-capable operation (a deuterium species test, or a >1.9 MeV machine) the caveat is the operative part: an X-ray shield does not automatically cover the neutron hazard, and the source names proton and deuteron machines as exactly the case where neutrons dominate. The source's physics points to hydrogenous material (concrete, HDPE) rather than lead for the neutron component, but sizing it is a separate design problem - worked from the actual source term and verified by survey - not settled in advance by this rule of thumb.
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For first-pass neutron shield sizing the chapter uses the reactor-derived removal-cross-section method: penetration as exp(-Sigma_r*x), with removal cross-sections roughly three-quarters of the total at 8 MeV (somewhat larger for hydrogen), and its concrete coefficient Sigma_r ~ 0.094 cm^-1.
phi(x) = phi_0 exp(-Sigma_r x); sigma_removal ~ 0.75*sigma_total @8 MeV; Sigma_r(concrete) ~ 0.0942-0.0945 /cmSource quote & editorial note
Experimental removal cross sections are roughly three-quarters of the total cross section for 8 MeV neutrons. For hydrogen this fraction is somewhat larger.
Editorial note, tabletop extrapolation: The one-line neutron shield ESTIMATOR for contingency planning - a D-D source term attenuates ~10x per 24 cm of concrete at the chapter's coefficient - used with its conditions: the coefficient is energy-derived (8 MeV; 2.45 MeV D-D neutrons remove differently), hydrogen content matters, and the chapter's own safety factors ride along. An estimate to verify by survey, never a design allowable.
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Worked pattern for a neutron shield, as the chapter runs it: its example yield (20-MeV protons on an optimized Cu target, ~6.5e10 n/s per uA), the flux at the shield face, a demanded six orders of magnitude of attenuation, and inverting exp(-Sigma_r*x) - giving the quoted 146 cm of concrete.
Y(20 MeV p on Cu) ~ 6.5e10 n/s/uA; x = ln(attenuation)/Sigma_r -> 146 cm for 1e6Source quote & editorial note
This means the shield must reduce the fast neutron flux by six orders of magnitude. Therefore e-Sigma_r*x = 10-6 ... X = 146 cm.
Editorial note, tabletop extrapolation: The template to copy for any neutron-capable scenario: source yield -> flux at the shield (1/4pi r^2) -> required attenuation from the dose criterion -> x = ln(A)/Sigma_r. Also the scale anchor for why amateur neutron machines are enclosure-limited: the chapter's 20-MeV, mA-class case needs five feet of concrete.
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D(d,n)He3 and T(d,n)He4 are EXOENERGETIC - they run at very low bombarding energy (Cockcroft-Walton scale) - so any deuterium in source gas or beam-loaded surfaces makes neutrons with no threshold protection. Other deuteron channels are exoenergetic too (9Be(d,n) Q ~ +4.4 MeV, 7Li(d,n) Q ~ +15 MeV): thresholdlessness is a property of deuteron beams on several light targets, while the common PROTON channels, (p,n), are threshold-protected.
D(d,n)He3 Q = +3.27 MeV; T(d,n)He4 Q = +17.6 MeV; also exoenergetic: 9Be(d,n), 7Li(d,n); common (p,n) and (gamma,n) channels are threshold-protectedSource quote & editorial note
Two of these reactions, the D(d,n)He3 reaction and the T(d,n)He4 reaction are exoenergetic and can be initiated at very low energies. Thus these two reactions can be produced in small Cockcroft-Walton accelerators.
Editorial note, tabletop extrapolation: THE loophole in the 'sub-MeV machines make no neutrons' argument: natural hydrogen is ~150 ppm deuterium and D accumulates in beam-loaded surfaces, so a D-on-D source term exists in principle on any hydrogen machine - at yields the Coulomb barrier suppresses steeply at low energy, which is why the honest posture is a survey requirement, not alarm.
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Induced activity around an accelerator is a two-step process - beam makes neutrons/photons at the target; those activate surroundings - and because capture probability goes as 1/v, the chapter directs using the THERMAL cross section for estimating capture activation, with slowing-down activation negligible by comparison.
activation A0 = M*phi*sigma_thermal*(1-exp(-lambda*t_irr)); slowing-down activation negligible by comparisonSource quote & editorial note
In the slowing down process ... an insignificant amount of induced activity is produced as compared with the activity produced by thermal neutrons. Therefore the thermal cross section should be used for purposes of calculating the activity produced.
Editorial note, tabletop extrapolation: The correct FIRST bookkeeping if a neutron-capable operation is ever run: inventory surrounding materials against thermal flux (Cu 3.9 b, W 34 b, Au 96 b thermal, per Table IV-2). Capture is the floor of the inventory, not its ceiling - epithermal resonances and fast threshold reactions ((n,p), (n,alpha), (n,2n)) can dominate for some materials and spectra. On today's neutron-free machines there is nothing to activate either way.
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In the report's assessment of ordinary concrete, only Na-24 (15 h) and perhaps K-42 (12.4 h) presented any hazard - a shutdown of three to five days lets them decay to very low levels; barytes concrete adds Ba-139 (83 m), which builds up during a day's running but decays away overnight.
concrete activation governed by Na-24 (15 h) / K-42 (12.4 h); 3-5 day cooldown -> negligibleSource quote & editorial note
Only Na24 and perhaps K42 could present any kind of hazard. Because of the half-lives of these two isotopes, a shut down of three to five days will allow decay to very low levels.
Editorial note, tabletop extrapolation: Cooldown-scheduling logic for any future neutron-producing work, as the report's era assessed its concrete: modern assessments add impurity-driven products (Mn-56, Co-60, Eu-152/154, tritium and others) whose relevance depends on the actual aggregate and spectrum, so a real facility characterizes its own concrete rather than inheriting this list. For the current machines the practical point stands: with no neutron source term there is nothing to activate the basement structure - deuteron operation being the standing exception.
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Because thermal neutrons attenuate to ~1/3 of initial flux in the first 10 cm of ordinary concrete, about 2/3 of neutron activation lives in the shield's inner skin — so design shields with a removable row of concrete blocks on the inside that can be disposed of and replaced if they grow too active.
thermal flux ~1/3 per 10 cm concrete -> ~2/3 of activation in first 10 cm -> sacrificial inner block rowSource quote & editorial note
Thermal neutrons are attenuated to about one-third of their initial flux by the first 10 cm of ordinary concrete. Therefore 2/3 of the activity produced by the neutrons would occur in this region. This makes it possible to design shielding with a row of concrete blocks on the inside.
Editorial note, tabletop extrapolation: The modular-block enclosure pattern already favored for product machines gets a second justification: the inner course doubles as the sacrificial activation layer, replaceable without demolishing the shield. Two conditions travel with it: the 2/3-in-10-cm figure is for thermal neutrons in ordinary concrete, not every spectrum; and replaced blocks are surveyed and characterized before anything is 'disposed of' - activated material is a regulated waste stream (see /legal/).
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Long-lived photoproduced isotopes in shielding cannot be waited out: 'if large quantities of this isotope build up, it will be necessary to physically remove the activated shielding, so plans for this contingency should be made in the design of the walls' - the isotope's identity and production threshold are the chapter's context (Na-22-class, multi-MeV photons; cite current nuclear data when used).
above-threshold gamma flux + years of operation -> Na-22 inventory -> removable-wall contingency in designSource quote & editorial note
If large quantities of this isotope build up, it will be necessary to physically remove the activated shielding, so plans for this contingency should be made in the design of the walls.
Editorial note, tabletop extrapolation: Scope closed for the machine's photon energies - photoproduction needs multi-MeV photons far beyond any dee. The design principle transfers as prudence rather than prohibition: prefer enclosure designs that could be dismantled selectively (block walls, the sacrificial inner course of dg-1050) over monoliths - cheap to choose now, expensive to regret.
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The manual's reporting convention: express field measurements as DOSE EQUIVALENT, DE = D * QF * DF (rem), with D the measured absorbed dose, QF the LET-dependent quality factor, DF a distribution factor - absorbed dose alone does not specify the hazard of a mixed or high-LET field.
DE(rem) = D(rad) * QF * DFSource quote & editorial note
The effective dose called the "Dose Equivalent" in units of rem is given by DE=D*QF*DF.
Editorial note, tabletop extrapolation: The structure survives (modern practice uses operational quantities and wR), applied only where the instrument actually reads absorbed dose: a calibrated rem/Sv survey meter already reports a weighted operational quantity, and re-weighting it double-counts. Log what each instrument reports, record WHICH quantity that is, and weight only raw rad/gray readings before comparison to limits.
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The 1972 ICRP-era quality factor was approximated in tissue as QF = 0.8 + 0.16 * LET (LET in keV/um of water) - the era's one-line conversion from stopping power to protection weighting.
QF ~ 0.8 + 0.16*LET(keV/um H2O)Source quote & editorial note
QF = 0.8 + 0.16 LET where LET is in keV/u.
Editorial note, tabletop extrapolation: A window into how weighting works, not a generator of modern factors: current practice assigns wR by radiation type (alphas: 20) and the Q(L) relation differs from this 1972 line. The 11B(p,alpha) reaction shares ~8.7 MeV across a broad three-alpha spectrum - not fixed 1.7 MeV lines - and alpha weighting today is simply wR = 20. Flag anywhere it appears as the 1972 formulation of what is now wR.
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1972 practical quality factors, the quoted table: X-rays, gammas, electrons 1; neutrons below 10 keV 3, above 10 keV 10; protons 1-10; alphas 1-20 (the fission-fragment line is the table's neighbor: scan re-read queued). Use as the era's weighting set; modern wR replaces them in any real analysis.
QF: photons/e- 1; n<10keV 3; n>10keV 10; p 1-10; alpha 1-20; fragments 20 (1972 values)Source quote & editorial note
X-rays, gamma rays, electrons or positrons 1 ... Neutrons, Energy < 10 KeV 3 ... Neutrons, Energy > 10 KeV 10 ... Protons 1 - 10 ... Alpha particles 1 - 20
Editorial note, tabletop extrapolation: HISTORICAL VALUES - cite for provenance, apply ICRP-103 wR in analysis (photons 1, neutrons 2.5-20 by energy, alphas 20). Where endpoints agree (photon 1, alpha 20) the numerical conclusions survive - re-derive under modern operational quantities all the same (dg-1052's instrument-quantity discipline).
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Flux-density-to-dose conversion for neutrons in the manual's table (100 mrem per 40-h week): thermal 680 n/cm2-s, 10 keV 700, 100 keV 115, 500 keV 27, 1 MeV 19, 10 MeV 17 - the table's fast-neutron minimum near 0.5-1 MeV makes those neutrons ~35x more restrictive per unit flux than thermal.
100 mrem/40h flux limits: 680 (thermal), 19 (1 MeV), 17 (10 MeV) n/cm2-sSource quote & editorial note
2.5 x 10-8 (thermal) 2 680 ... 5 x 10-1 11 27 ... 1 11 19
Editorial note, tabletop extrapolation: The conversion pattern for any future neutron survey, used with its conditions: a reading converts only when the energy is known or the instrument already folds the spectrum in (a rem-meter does), and these are 1972 occupational numbers - modern public limits sit far lower. The design fact survives: fast neutrons near 0.5-1 MeV are the most restrictive per unit flux, which is why a D-D contamination field matters at even a few n/cm2-s.
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The manual's CRITICAL-ORGAN method for deriving dose limits: identify the organ that governs for the radiation type - skin for relatively non-penetrating radiation (the quoted case), blood-forming tissue for penetrating radiation in the chapter's pairing - set the limit for that organ, and note natural background (the chapter's 50-175 mrad/yr, locally variable) as the comparison floor.
non-penetrating radiation -> skin is critical organ; penetrating -> blood-forming tissue; limit set per organ against background contextSource quote & editorial note
When the whole body is exposed to relatively non-penetrating radiation it may be assumed that the skin is the "critical organ" which determines the maximum permissible dose.
Editorial note, tabletop extrapolation: Directly relevant to sub-10-keV dee bremsstrahlung, which deposits mostly in shallow tissue: the shallow/skin dose is usually the governing quantity for the machine's leakage fields - established by measurement, not assumption, since photons near 10 keV do reach past the epidermis - which is why survey instruments must be thin-window (Ch. VI) and why whole-body numbers alone can understate the field.
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The 1972 occupational limits - accumulated whole-body dose <= 5 rem x (age-18) and <= 3 rem per quarter (the quoted pair), with the chapter's companion values for skin, extremities, and a 0.17 rem/yr general-public figure (about 30x below the occupational 5 rem/yr) - are SUPERSEDED; extract only the structure: occupational vs public tiers, quarterly pacing, organ-specific limits.
HISTORICAL: 5(N-18) rem accumulated; 3 rem/qtr (quoted); companion table: skin 15 rem/yr, extremities 75/25, public 0.17 rem/yr (~30x below occupational). MODERN: 10 CFR 20 / NCRP 116 - 5 rem/yr occupational, 0.1 rem/yr public, age-proration abolishedSource quote & editorial note
shall not exceed 5 rems multiplied by the number of years beyond 18. The dose in per calendar quarter shall not exceed 3 rems.
Editorial note, tabletop extrapolation: CAUTION — HISTORICAL NUMBERS, superseded by 10 CFR 20 / NCRP 116 (5 rem/yr occupational, 100 mrem/yr public, age-proration abolished). Keep for reading-era context and for the still-valid design pattern: public-tier limits ~10-50x below occupational drive product-machine enclosure design, since customers are "general population."
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Accelerator radiation differs from isotope-source radiation in ways that defeat isotope-calibrated instruments - the chapter's trio: PULSED time structure (the quoted cyclotron line: 50-200 us macropulses with microstructure at RF frequencies), ANISOTROPY, and MIXED neutron/gamma fields; the quote itself carries the pulse row.
cyclotron pulse structure: 50-200 us macropulse + microstructure at RF frequency (Table VI-1)Source quote & editorial note
Cyclotron positive ions 50-200 usec ... Microstructure at RF frequencies
Editorial note, tabletop extrapolation: The reference machine runs CW-RF but a beam bunched at 9 MHz; any future pulsed-RF operation (LDMOS duty-cycling) puts the machine squarely in this table — recheck every survey instrument's pulse response before trusting it.
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When counting radiation from a pulsed machine whose pulse length is shorter than the detector dead time (GM: 200-600 us; ion chamber 5-10 us; organic scintillator 0.01-0.1 us), the measured rate saturates at the pulse rate - provided each pulse registers at least one count and the detector recovers between pulses - no matter how intense the field.
for rho > pulse length, n'_max = pi (pulses/s); GM dead time 200-600 us (Table VI-2, Eq. VI-9)Source quote & editorial note
the second term in the equation above becomes zero and the number of counts per second, as is expected, becomes the radiation source pulse rate.
Editorial note, tabletop extrapolation: THE classic accelerator-survey trap, and the reason the program's survey doctrine prefers current-mode ion chambers over GM counters for any pulsed operation: a counter reading 60 cps at a 60 Hz pulse rate is reporting its saturation value, not a dose rate. The saturation reading appears when the field is strong; a weak pulsed field reads below the pulse rate, so equality with the pulse rate is the alarm signature.
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Measure mixed neutron-gamma dose equivalent with PAIRED ionization chambers - one tissue-equivalent, one neutron-insensitive - and combine as DE = Gamma + 10*N, with 10 the manual's era-labeled 'conservative' quality factor.
DE = Gamma + 10N (paired TE + neutron-insensitive chambers; the 10 is the 1972 factor - modern wR at 2.45 MeV is ~16-20)Source quote & editorial note
An approximation to the dose equivalent in a mixed neutron and gamma ray field can then be given by DE = Gamma + 1ON ... 10 = a conservative value for the quality factor
Editorial note, tabletop extrapolation: The cheapest credible mixed-field method for an amateur program - two chambers and a subtraction - and the fallback if a rem-ball is out of budget for future neutron-capable tests. Two updates travel with it: modern wR for D-D neutrons is ~16-20, so the manual's 10 is no longer conservative - plan with 20; and the subtraction is only as good as each chamber's known gamma and neutron response, so calibration is part of the method, not an extra.
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Dose-equivalent-proportional neutron instruments exist and work: an Anderson-Braun BF3 counter in polyethylene/boron cylinders read dose equivalent to +-10% from 0.04 to 10 MeV in the cited tests, and a properly made moderated-sphere rem counter held similar accuracy at intermediate energies - a rem counter beats converting raw flux by hand.
Anderson-Braun rem counter +-10% over 0.04-10 MeV; moderated thermal detector rem-proportional +-10%Source quote & editorial note
They obtained an accuracy of +-10% in measuring dose equivalent of neutrons over the range 0.04 to 10 MeV.
Editorial note, tabletop extrapolation: Justifies planning on one moderated rem meter as the primary neutron instrument for a D-D-class source term (2.45 MeV sits mid-band). Its band is not everything: moderated and scattered fields extend below 40 keV where response rolls off, so corners and maze mouths get checked against the instrument's stated energy response - and the calibration must be current.
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The ICRU neutron quality factor is strongly energy-dependent: 2 from thermal to 10 keV, rising to a PEAK of about 11 near 500 keV, falling back to about 6 between 10 and 20 MeV — the intermediate/ fast band around 0.1-1 MeV is biologically the most expensive per rad.
QF(n): 2 (thermal-10 keV) -> ~11 peak near 500 keV -> ~6 (10-20 MeV)Source quote & editorial note
The ICRU has recommended a quality factor of 2 for neutrons between thermal and 10 KeV. This then rises to a peak of about 11 near 500 KeV before falling back to about 6 between 10 and 20 MeV.
Editorial note, tabletop extrapolation: Amateur-scale neutron concerns CENTER on the worst band: D-D neutrons are born at 2.45 MeV and moderate down through the keV-MeV weighting peak, so never average a survey away with a thermal-flux conversion. Modern wR moves the peak to ~20 near 1 MeV - the reasoning got MORE conservative, not less - while fully moderated thermal populations still get their own, lower weight.
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Photon survey instruments misbehave at low energies where the photoelectric effect dominates - the chapter's account: cavity-chamber response FALLS from wall-thickness effects, then can swing ABOVE unity just over that region because wall Z exceeds air's; its discussion places the trouble region below roughly 150 keV.
below ~150 keV photoelectric regime -> wall-thickness response falloff + over-response band + directional error; open-air chamber +-20-30% over large delta-TSource quote & editorial note
In a cavity ionization chamber the relative response falls off at low energies because of the effect of the thickness of the walls. Just above this energy the relative response can rise above unity because the effective atomic number of the walls exceeds that of air.
Editorial note, tabletop extrapolation: The measurement-side half of the reference machine's X-ray problem: the machine's photon spectrum ends at the dee voltage - tens of keV at most - squarely inside the misbehavior region, so an uncalibrated chamber reading of dee bremsstrahlung can err in either direction. Use thin-window instruments with a low-energy calibration point (dg-559, dg-1035).
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Harden detector electronics against the machine's own environment - the chapter's prescriptions: commercial mu-metal shields 'if properly used' normally suffice for photomultiplier magnetic sensitivity, aluminum foil or screening for RF fields, and well-grounded cable shields with a common ground against pulsing-synchronous EMI.
PMT: mu-metal (B-field) + Al foil/screen (RF); signal runs: grounded shield + single common groundSource quote & editorial note
Commercial mu metal shields, if properly used, will normally provide sufficient shielding against magnetic fields. To eliminate the effects of RF fields, aluminum foil or screening can be used.
Editorial note, tabletop extrapolation: Written for exactly such a bench: a scintillator PMT near a 0.6 T magnet's fringe field and a 9 MHz (soon LDMOS) transmitter. 'Properly used' is load-bearing - mu-metal saturates in strong fields and PMT gain moves at millitesla - so position the PMT where the fringe field is already small, shield, and verify gain with a check source in place; confirm RF quieting with the transmitter actually running. The Keithley 617 grounding lore in the reference machine's as-builts is this rule independently rediscovered.
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The most common cause of serious accelerator radiation exposure is entry — accidental or intentional — into the shielded target cell during operation; shielding quality is irrelevant if access during beam-on is possible, so access limitation (physical barriers + interlocks, generally both) is a first-class design requirement, from "a small shielded box with an interlocked lid" up.
access control = physical barrier + electrical interlock, both, sized to the hazardSource quote & editorial note
The most common cause of serious radiation exposures associated with accelerators, has been accidental (and sometimes intentional) entrance into the normally shielded target cell.
Editorial note, tabletop extrapolation: The product-machine posture in one line: an educational cyclotron IS the 'small shielded box with an interlocked lid' (Ch. I's phrase). Lid switch + beam-off interlock + machine-on light is the historically identified starting set for this machine class - not a sufficiency proof: fail-safe wiring (opening kills beam; no automatic restart on re-closing), periodic interlock function tests, and the access and bypass rules (dg-654, dg-1074) complete the design.
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Estimate X-ray streaming through a maze by successive 90-degree scatters: assume conservatively that 0.05 of the incident energy scatters into one steradian per bounce - Moyer's estimate, the quote; the chained product I_p = (I_1/r_n^2)*prod[0.05*S_i*cos45/r_i^2] is the chapter's application of it (validation data: scan re-read queued).
I_p = I_1/r_n^2 * prod_i [0.05 * S_i * cos45 / r_i^2] per 90-deg scatter legSource quote & editorial note
Moyer estimated that for a 90 deg scattering of X-rays it is conservative to assume that 0.05 of the incident energy would be scattered into one steradian in the new direction.
Editorial note, tabletop extrapolation: The same hand calculation sizes a cable or vacuum-line dogleg or an instrument-port baffle in a product-machine enclosure - where a straight-through hole would dominate the leakage - with the estimate verified by survey once built (dg-917's discipline).
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Permit NO line-of-sight path for radiation through any access route or penetration, and then still evaluate the scatter path through the maze - the chapter's paired requirements.
no line-of-sight through any penetration; scatter path evaluated per the 0.05/sr ruleSource quote & editorial note
Naturally no "line of sight" path for radiation would be permitted yet it is also necessary that the scatter path through the maze be considered.
Editorial note, tabletop extrapolation: The audit rule for every feedthrough, window and joint in an enclosure: check sight-lines from the X-ray source point (the dee gap) outward, then bound the one-bounce leakage with the albedo rules (dg-1068). Geometry creates the streaming problem; material still sets what each bounce and wall costs, so both enter the estimate.
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For neutron streaming through mazes the manual uses the albedo chain phi_p = (phi_s/(4pi r_n^2)) * prod[beta*Omega_i]: its albedo values run from 0.66 for thermal neutrons down to ~0.05 for fast, with 0.4 offered as a conservative fast-neutron choice, and boron loading on the shield-wall surface absorbs thermal neutrons instead of reflecting them.
albedo beta = 0.66 (thermal) -> ~0.05 (fast); 0.4 conservative; boron loading cuts thermal reflectionSource quote & editorial note
albedo for neutrons (from 0.66 for thermal neutrons to approx. 0.05 for fast neutrons)
Editorial note, tabletop extrapolation: Contingency reference only at current energies. If a future neutron source term streams through an enclosure penetration, the boron-surface idea (borated HDPE lining a duct) reduces the thermal reflection specifically - it does nothing for the fast component - so it is one element of a duct fix, sized with the chain using energy-appropriate albedos and checked by survey, not a standalone cheap cure.
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Interlock philosophy, the quoted requirement: it should NEVER be convenient to remake an open interlock without someone physically going to the point of the break and, if the hazard no longer exists, re-establishing it there; the chapter pairs this with keeping systems simple and low-friction so operators are not tempted to defeat them (that passage: scan re-read queued).
simple + low-friction + no remote remake of a broken interlock (reset at the point of break)Source quote & editorial note
it should never be convenient for an operator or an experimentor to remake an open interlock without someone actually going to the position of the break and, if the hazard no longer exists, reestablishing the interlock.
Editorial note, tabletop extrapolation: Design requirement for the product controller: a tripped lid/door input must latch and require a local (at-the-lid) action plus console reset — a firmware-only "clear fault" button recreates the exact failure mode this rule exists to prevent.
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Select interlock COMPONENTS with the same care as the protection system: 'only heavy duty industrial type limit switches should be employed, avoiding light duty switches' - the quoted requirement; the chapter's environmental context (radiation, ozone attack on contacts) accompanies it (scan re-read queued).
heavy-duty industrial limit switches only; scheduled interlock test + maintenanceSource quote & editorial note
only heavy duty industrial type limit switches should be employed, avoiding light duty switches to insure durability and reliability.
Editorial note, tabletop extrapolation: BOM-level guidance for product machines — safety-rated (positive-opening) limit switches on lids/doors, not PCB microswitches, plus an interlock-test line item in the ops checklist (Cyclotron_procedures2 already has the pattern for vacuum; extend to safety chain).
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Rate materials in the radiation zone: semiconductor circuits must stay out of high-radiation positions, and insulation ranges over eight decades of tolerance — Teflon is the WORST common insulator (5e4 rad gamma) while phenolic-glass laminate, polyurethane, diallyl phthalate exceed 1e10 rad and ceramics 1e11-1e12 — choose in-cell wiring accordingly.
radiation tolerance (gamma): Teflon 5e4 rad; PVC 1e8; epoxy/polystyrene 5e9; phenolic-glass >1e10; Al2O3 1e12Source quote & editorial note
Teflon 5 x 104 ... Phenolic, Glass laminate >1 x 1010 ... Aluminum Oxide 1 x 1012
Editorial note, tabletop extrapolation: Counterintuitive and worth flagging in the next machine's design notes: PTFE, the amateur's default HV insulator, is the most radiation-fragile common insulator on the table - by four decades against phenolic-glass. At the reference machine's current operation insulators see no significant dose in the first place; the flag matters wherever a future neutron- or target-adjacent position exists - specify ceramic or glass-laminate there, per the table.
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Fail-safe circuit logic, per the manual: require a complete path or presence of a signal to PERMIT accelerator operation, and let any open circuit or loss of signal disable it - so the commonest failures (broken wires, unplugged connectors, lost power) land in the safe state.
permissive = continuously energized circuit; any open / loss of signal -> beam offSource quote & editorial note
a fail-safe design may typically use a complete path or presence of a signal to permit accelerator operation and an open circuit or loss of signal to disable operation.
Editorial note, tabletop extrapolation: The normally-energized interlock-loop architecture: a series loop holding the RF/HV enable relay closed puts breaks, unplugs and power loss on the safe side. One loop is the architecture, not the whole chain - channels that must be independent stay independent (dg-1074), the loop gets exercised periodically (dg-1110), and any trip thresholds (a beam-current ceiling included) come from the machine's own hazard analysis.
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Prefer loss of operating time to loss of safety - the quoted principle: design so anticipated malfunctions trip the interlocked function to its safe state, accepting false trips as the price (the chapter's illustrative failure list - power loss, broken wires, sticky relays: scan re-read queued).
enumerate failure modes -> all anticipated failures trip safe; latching event memory + manual reset; downtime > riskSource quote & editorial note
For interlocks, however, the loss of operating time must be preferred to the loss of safety.
Editorial note, tabletop extrapolation: Two concrete requirements: (1) an FMEA-style enumeration of interlock failure modes with each shown to land safe; (2) latched annunciation: the controller must remember a mid-run lid opening even if reclosed, until deliberately reset.
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Pre-write the interlock BYPASS procedure, because maintenance and special setups will need one: the Army manual's system uses a two-key arrangement in which the Radiation Safety Officer's key is required before a single operator can disable any interlock affecting personnel safety, and the manual adds that a definite, redundant procedure for restoring the bypass before routine operation matters more than the bypass procedure itself. [Corrected 2026-08-23: the earlier note said a logged jumper "does the same work" as the two-key system. It does not - see the note.]
bypass = 2-key (operator + RSO) + written restore-verification procedure with redundancySource quote & editorial note
This system uses a dual input which prevents the single key from disabling an interlock which affects personnel safety without the additional input provided by the Radiation Safety Officer's key.
Editorial note, tabletop extrapolation: What the two keys buy is INDEPENDENT CUSTODY of the bypass itself: no single person can disable a personnel-safety interlock alone. Restoration is a separate control - the written restore-verification the manual calls for. A school machine can reproduce both (instructor key distinct from the operator credential; signed restore checklist before the next class). A one-person home lab cannot reproduce the independence: a logged bypass record preserves the paper trail, not the custody - which is the argument for designing so bypasses are rarely needed at all.
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A person overlooked during the search before lockup must be able to POSITIVELY defeat the beam - not merely shut down some unassociated apparatus: the quoted requirement (the chapter's e-stop identification guidance sits alongside: scan re-read queued).
e-stops obvious to visitors, positively beam-defeating, hesitation-free cultureSource quote & editorial note
A person overlooked during the search before lockup must be able to positively defeat the beam instead of ineffectively shutting down some unassociated apparatus.
Editorial note, tabletop extrapolation: In-enclosure e-stop requirement for any walk-in product installation; even for benchtop machines the classroom master kill must cut the actual hazard (RF+HV+source), not merely the controller, and the no-blame-for-pressing norm belongs in the curriculum.
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Search-before-lockup, the quoted standard: after completion of the lockup procedure, the person who performed the survey 'should have seen every position capable of hiding a man'.
pre-startup search must sweep every human-capable volume; stations scale with complexitySource quote & editorial note
After completion of the lockup procedure the person who has performed the survey should have seen every position capable of hiding a man.
Editorial note, tabletop extrapolation: Trivially satisfied on a benchtop machine, but a REAL checklist line for any walk-in enclosure a customer institution builds (dg-1065's accident mechanism is the reason); it belongs in the product installation manual's commissioning procedure.
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Standardize alarms and displays - the quoted requirements: light colors represent CONSTANT situations, and audible-alarm meanings are kept clear by routine test alarms at programmed times, but not so frequent they cry wolf (the LRL sound mapping is the report's example: scan re-read queued).
one meaning per sound/color, consistent wording, scheduled (not excessive) alarm tests, visible interlock statusSource quote & editorial note
Colors of lights should represent constant situations. ... Confusion with meanings of various audible alarms can be avoided by routine test alarms at programmed times. Too frequent tests, however, may do more harm than good (cry wolf).
Editorial note, tabletop extrapolation: The product HMI spec seed — a "machine on" beacon distinct from "RF enabled", consistent across every unit shipped, with an alarm-test entry in the curriculum's first lab.
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Massive shielding doors carry their own hazards in the manual's treatment: slow travel with great momentum (engineer the stopping so the door cannot trap personnel or crack walls), shielding at least equal to the adjoining wall, and - the quoted requirement - every door manually openable from BOTH inside and outside after a loss of power.
door shielding >= wall; manual egress inside+outside under power loss; engineered decelerationSource quote & editorial note
one must be able to open these doors even after a loss of power. Some manual method of opening the door from inside and outside must be included in the design.
Editorial note, tabletop extrapolation: Scale-invariant egress principle: even an interlocked benchtop lid or a walk-in enclosure door must never imprison anyone on power loss. The criterion is manual operability from both sides without power, verified by actually trying it - whatever the mechanism - and the door's own motion is a machinery hazard (pinch points, momentum) to engineer alongside its radiological job.
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Two quoted Morse principles anchor protection-system design: human safety should not be entrusted to one or more persons following a written routine; and even mechanized systems become routine after a time and hence may lose their effectiveness.
no safety-by-checklist-alone; counter habituation deliberately (the site's translation: vary the interlock-test scenario)Source quote & editorial note
Human safety should not be entrusted to one or more persons following a written routine. ... Even mechanized systems become routine after a time and hence may lose their effectiveness.
Editorial note, tabletop extrapolation: The strongest possible source endorsement for the program's hardware-interlock- over-procedure stance (procedures complement, never replace, the interlock chain), plus a curriculum idea: occasionally rotate the interlock test scenario so student operators never go through the motions.
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Accelerator accident history's sharpest fact, quoted: every recorded potentially lethal dose involved HIGHLY EXPERIENCED personnel - 'this accents the need for continuous education programs'; the chapter's discussion of untrained non-accelerator workers accompanies it (scan re-read queued).
accident causes = untrained bystander OR bypassed procedure; experience does not protect -> recurring educationSource quote & editorial note
The recorded cases in which potentially lethal doses of radiation have been received have all involved highly experienced personnel. This accents the need for continuous education programs.
Editorial note, tabletop extrapolation: Aimed straight at a two-person family lab and at teacher-operators: familiarity is the documented risk factor, and the visitor/helper (the "maintenance worker") is the documented victim class — brief every guest, and rehearse the rules even after years of clean operation.
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There is no substitute for the vigilance of personnel — automatic devices, interlocks, and remote area monitoring are ESSENTIAL BUT INSUFFICIENT without personnel training; engineering and administration are complements, not alternatives.
protection = engineered systems AND trained vigilant people; neither alone sufficesSource quote & editorial note
There can be no substitute for the vigilance of personnel. Automatic devices, interlocks and remote area monitoring systems are essential but insufficient to do the job without personnel training.
Editorial note, tabletop extrapolation: The counterweight to over-trusting the product machines' interlock chains — the curriculum's radiation-safety module is a safety SYSTEM component, not documentation overhead.
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Begin the radiation-protection program at the CONCEPTION of the facility — safeguards incorporated during funding/design/construction cost significantly less than safeguards superimposed on an existing facility.
RP designed-in at concept << RP retrofitted (cost)Source quote & editorial note
if proper safeguards are incorporated into the construction of the accelerator facility the cost of safety will be significantly lower then if such safeguards are superimposed upon already existing facilities.
Editorial note, tabletop extrapolation: Why a hazard analysis belongs at desk phase rather than after first beam: the enclosure, interlocks and monitoring get designed into the machine rather than left to whoever installs it.
Cited in: Choosing Your Machine
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In radiation service, LN2-cooled surfaces accumulate a hidden explosive: oxygen condensed from air into the liquid nitrogen is radiolyzed to ozone and left CONCENTRATED after the nitrogen evaporates - a significant explosion hazard, the quoted mechanism.
LN2 trap + radiation -> condensed O2 -> O3 concentrate on warm-up = explosion hazard; inspect irradiated insulation on shortened scheduleSource quote & editorial note
The oxygen from the air condensed in the liquid nitrogen, radiolyzed to ozone and left in concentrated form after the evaporation of the nitrogen presents a significant explosion hazard.
Editorial note, tabletop extrapolation: Directly applicable to any LN2 cold trap on the diff-pump line if machine energies ever rise - and worth a procedures line now: a trap that has sat in a radiation-plus-discharge environment gets attended warm-up and venting, because the quoted mechanism concentrates oxidizer exactly at boil-dry. (An editorial precaution drawn from the quoted physics.)
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Small organizations frequently cannot field a separate health-physics staff, so the operations staff acts as its own HP staff — a workable "way of life" ONLY if responsibilities and priorities are explicitly defined; in larger setups, keep HP advisory and leave radiation-safety responsibility with the operational supervisor.
small org -> operator doubles as HP; must write down who owns which safety decisionSource quote & editorial note
it may be necessary for the operations staff to act as the health physics staff as well. Though less then ideal, this condition will frequently be a "way of life". Under these conditions it is of paramount importance to define responsibilities and priorities.
Editorial note, tabletop extrapolation: A 1972 acknowledgement, with conditions, of the small-facility reality in which one person wears both the operator and radiation-safety hats. The conditions transfer to any teaching installation - the documentation names the RSO-equivalent role and its decision rights - and the arrangement itself must clear the jurisdiction's requirements: registered machines commonly require a named, qualified RSO (/legal/), which written role definitions support but do not replace.
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Ozone is the dominant toxic gas from irradiating air in the manual's treatment (G = 13.8 +- 0.7 molecules O3 per 100 eV in oxygen radiolysis, X-ray value); predict cell concentration with its production model c0 = 600*G*i*d/V (i = beam current in A, d = beam path in air in m, V = cell volume in m3) balanced against exhaust rate and molecular lifetime.
c0 = 600*G(O3)*i*d/V; C = c0/(v/V+1/alpha)*(1-exp(-(v/V+1/alpha)t)); entry criterion ~0.1 ppmSource quote & editorial note
indicate a confident Xray value of 13.8 +- 0.7 molecules of O3/100 e.v. in the radiolysis of oxygen. This value is used here.
Editorial note, tabletop extrapolation: At the reference machine's beam powers the radiolytic term is negligible against the model's other terms - but the same production-vs-exhaust balance covers corona and discharge ozone from the HV and RF systems in a closed basement. Odor (threshold ~0.01-0.05 ppm) tells you ozone exists, not how much, and olfactory fatigue silences it during exposure - so the control is ventilation sized by the model or a measurement, with the era's 0.1 ppm occupational figure replaced by the jurisdiction's current limit.
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Ozone decays by first-order kinetics with an effective indoor 'half-life' of about 35 minutes in the cited Rensselaer and Yale measurements - the manual takes the without-irradiation lifetime as the conservative choice - so ventilation OR a measured-half-life wait, not seconds of airing, clears an ozone-loaded room.
O3 half-life ~35 min indoors (Rensselaer/Yale measurements); C1 = C*exp(-(v1/V+1/alpha_1)*t1)Source quote & editorial note
noted an approximate "half-life" for the ozone in their measurements at Rensselaer and Yale of 35 minutes.
Editorial note, tabletop extrapolation: Practical basement rule of thumb: after an RF/HV session with ozone smell, a ventilated half-hour is one measured half-life - which only halves an unknown starting concentration. The checklist entry is therefore 'ventilate, wait, then confirm by fresh-nose absence of odor at re-entry' - surfaces, humidity and any continued production move the real decay rate, in either direction.
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Monitor exhaust filtration by PRESSURE DIFFERENTIAL: serious changes in delta-P across the filter bank indicate either clogging or rupture; the manual pairs the delta-P watch with a detector (ion chamber or scintillator) at the filter face to track trapped-activity buildup.
filter health = delta-P trend (clog = rising, rupture = falling) + detector at filter faceSource quote & editorial note
Serious changes in the pressure differential on the up and down stream sides indicate that the filter has either clogged or ruptured.
Editorial note, tabletop extrapolation: The delta-P-as-health-monitor pattern transfers to every filtered exhaust in the lab (pump exhaust filters, fume paths for boron sputtering later): instrument the pressure drop, not the filter's appearance. Delta-P sees gross changes - clog rising, rupture falling - while pinholes and seal bypasses can pass it silently, so where a release would actually matter, periodic sampling still closes the loop.
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Air-activation species (13N, 15O) from (gamma,n) are 'of concern only to electron accelerators of energies in excess of 15-20 MeV' - the manual's practical judgment. The underlying thresholds sit lower (14N(gamma,n) ~10.6 MeV, 16O(gamma,n) ~15.7 MeV); yield, not kinematics, sets the manual's concern line. 16N (7.1 s) matters inside recirculating ducting.
thresholds: 14N(gamma,n)13N ~10.55 MeV, 16O(gamma,n)15O ~15.66 MeV; the manual's practical concern line: >15-20 MeV electron machinesSource quote & editorial note
The threshold for (gamma,n) reactions are of sufficient magnitude to make the production of 13N and 15O of concern only to electron accelerators of energies in excess of 15-20 MeV.
Editorial note, tabletop extrapolation: Scopes air activation out of every current and planned program machine - all far below even the 10.6 MeV threshold - so the air-handling design concentrates on ozone (dg-1085). When a reviewer asks, cite the actual thresholds alongside the manual's concern line rather than conflating them.
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Shape sector iron by formula-guided empirical iteration, not a priori specification: pick "reasonable" <B>(r) choices, observe the flutter F(r) that results, and test the combination against tune formulae rather than demanding the iron fit pre-selected profiles exactly.
iterate {<B>(r), F(r), tan(spiral)} -> Smith-Garren vz^2, vr -> accept/reject; do not fix profiles a prioriSource quote & editorial note
The process is a trial and error search, with general guidelines and test criteria for success.
Editorial note, tabletop extrapolation: Directly transferable design-process pattern for any pole or shim work on a next machine: let FEMM play the role of the Nevis model magnets, with analytic tune formulae as the accept/reject criteria - within FEMM's 2-D limits (azimuthal structure needs a 3-D model or the measured map; the playbook's tracker closes that loop). The final accept/reject is the measured field, exactly as it was at Nevis.
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Evaluate axial and radial tunes first with analytic formulae (Smith-Garren), then verify at critical places — especially large radius where derivative terms grow — by exact orbit-integration computer solutions.
analytic vz,vr everywhere; exact orbit codes at critical radii (large r, extraction)Source quote & editorial note
first evaluated using the Smith-Garren formula, checked at critical places, especially at larger r, by exact orbit motion computer solutions.
Editorial note, tabletop extrapolation: Exactly the field-solver-plus-orbit-tracker pipeline an amateur design can run. The Nevis precedent: spend the expensive tracking where the cheap formulae are least trustworthy - large radius and the extraction region on their machine - and anywhere else the smooth approximation visibly strains.
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Build adjustability into pole and sector iron: Nevis planned final 'touch up' machining of these pieces with the final iron in place, driven by magnetic field-mapping studies - the quote; bolt-on, pin-located implementation details are the site's editorial translation of what makes such iteration cheap.
removable edges + removable center tips + slotted repositioning + locating pinsSource quote & editorial note
a final "touch up" machining of these pieces, with the final iron in place on the basis of magnetic field mapping studies.
Editorial note, tabletop extrapolation: Fully transferable at any scale — design a next machine's shims and center plugs as bolt-on, pin-located pieces so field-map-driven iteration does not mean remaking the poles.
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Harvest resonance lines to avoid from other machines' documented beam-loss experience: Nevis, alerted by ORNL's observed losses in ORIC, designed its tune trajectory to avoid specific coupling lines - the report names them (scan re-read queued for the identifications).
keep (vr,vz) trajectory clear of (3vr-vz)=3 and (vr+3vz)=2 (plus the standard low-order lines)Source quote & editorial note
alerted by the ORNL studies of observed beam loss in the ORIC cyclotron to try to avoid
Editorial note, tabletop extrapolation: Method transfers directly — a tune plot should carry resonance lines sourced from operating-experience literature, not just textbook theory; a weak-focusing tabletop crosses fewer lines but the audit habit is the point.
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Pass a rotating shaft into vacuum with a ferrofluidic seal: ferrite-loaded low-vapor-pressure liquid held in ~0.005 in. radial gaps by magnetic fields, sealing a full atmosphere with no sliding contact.
ferrofluidic rotary seal; ~0.005 in. radial gap; holds 1 atm differential; commercial item (Ferrofluidics Corp., 1971)Source quote & editorial note
a "Ferrofluidic" vacuum seal having ~ 0.005 in. radial gaps in which a ferrite loaded low vapor pressure liquid is held by magnetic fields
Editorial note, tabletop extrapolation: A candidate commercial component - available since 1971 - whenever an accelerator mechanism (chopper, rotating target, variable capacitor) needs rotary motion through the chamber wall; prices vary widely, so treat cost like any other spec. Verify the specific seal's pressure rating (one-atmosphere capability included), leak rate, vapour and backstreaming cleanliness, bakeout limit, speed and torque, and its behaviour in a nearby magnetic field before designing it in. [Note revised 2026-08-23: earlier note called it 'the clean answer any time'.]
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Give mechanically dirty subsystems their own separately pumped vacuum envelope where warranted: Nevis's rotating-capacitor housings had separate turbopumped vacuum systems, partitioned from the main cyclotron vacuum by the RF feedthrough insulators.
separate turbopumped housing per mechanism + feedthrough insulator as vacuum partitionSource quote & editorial note
The capacitor housings have separate vacuum systems using turbomolecular pumps. RF feed through insulators separate them from the main cyclotron vacuum system.
Editorial note, tabletop extrapolation: Scales down as a case-by-case method: a sealed partition (like Nevis's insulator barrier) actually isolates the gas load; an OPEN differentially pumped appendage - the reference machine's diff-pumped source region - only reduces transfer through its conductance. Pick per mechanism from a conductance and gas-load estimate, and remember debris control is geometry, not pumping.
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Couple RF to rotating elements without sliding contacts, as Nevis did: feed the stationary electrode and hold the rotor near RF ground through small high-capacitance face gaps (<0.010 in. there), keeping the shaft at RF ground so bearings and drive live in air at ground potential.
rotor-to-ground face gap < 0.010 in. (high C shunt); stator carries RF; shaft/drive at ground in airSource quote & editorial note
the rotors are at low RF due to their < 0.010 in. high capacitance face gaps to ground
Editorial note, tabletop extrapolation: The capacitive-shunting method transfers to rotating RF machinery (choppers, tuners) - by calculation, not copying: work out the gap capacitance (area and gap, not gap alone), the induced rotor voltage and displacement current at the actual frequency and power, and the field/breakdown margins in vacuum. The rotating-capacitor FM tuner itself is synchrocyclotron-specific and does NOT transfer to a fixed-frequency tabletop machine.
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When a resonator must tune over a band, vary the transmission-line characteristic impedance along its length - Nevis's profile (~6 -> ~2 -> 8 ohm) tends to minimize the required capacitor Cmax/Cmin ratio - and budget for structure inductance at the RF frequency considerably increasing the effective Cmax (their full-scale capacitors: 6.5/1.3 nF measured at 1000 Hz).
Nevis: Z0 ~6 ohm -> ~2 ohm -> 8 ohm profile gave Cmax/Cmin = 6.5 nF / 1.3 nF (measured at 1000 Hz)Source quote & editorial note
The basic variation of line Zo along the resonator tends to minimize the capacitor Cmax/Cmin ratio needed. Inductance effects in the structure at the RF frequency considerably increase the effective Cmax value. It is expected that the full scale capacitors will each have Cmax = 6.5 nF and Cmin = 1.3 nF (measured at 1000 Hz).
Editorial note, tabletop extrapolation: FM machinery itself does not transfer, but the impedance-profiling option applies to any tunable tank or swept/trimmed cavity: model the resonator as a transmission line and let the optimization pick the profile - Nevis's own is nonmonotonic, so 'taper' is the idea, not the shape.
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Choose the resonator mode and geometry so tuning elements sit outside the main vacuum chamber: the half-wave resonator 'permits the rotating capacitors to be located outside... for good shielding from both the magnetic field and radiation' - the quote; the iron tuner housings are the report's detail (scan re-read queued).
half-wave resonator puts voltage node / tuner outside chamber; 2-in. Fe housing shields rotorsSource quote & editorial note
a half-wave resonator permits the rotating capacitors to be located outside the main vacuum chamber for good shielding from both the magnetic field and radiation
Editorial note, tabletop extrapolation: The placement principle transfers: keep variable capacitors, trimmers and drive mechanisms of a next machine's tank outside the pole gap and chamber, where field, beam spray and pumpdown cannot reach them - where the geometry allows it.
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Establish the RF system's variable parameters on a reduced-scale model plus computation before full-scale construction: the design 'used a 1/2 scale model, in conjunction with detailed computer calculations, to establish all parameters which can be varied' - which parameters, and the mode-clearance criteria, are the report's enumeration (scan re-read queued).
1/2-scale RF model + computation -> full-scale build; cross mode kept well below 2x main mode over tuning rangeSource quote & editorial note
The design has used a 1/2 scale model, in conjunction with detailed computer calculations, to establish all parameters which can be varied
Editorial note, tabletop extrapolation: At tabletop size the "scale model" is the full-size mockup on the bench — cold-test a next machine's dee/stem with a VNA before power exists; the mode-spectrum audit transfers verbatim.
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DC-float the dee/resonator so that a negative bias 'of amount sufficient to control multipacting' can be applied - the Nevis provision, with their planning value at -500 to -2000 V (Part II).
Nevis planning value: dee DC bias -500 to -2000 V (Part II, p.48)Source quote & editorial note
The dee resonator will be dc floating so a negative bias of amount sufficient to control multipacting can be applied.
Editorial note, tabletop extrapolation: Directly relevant at a next machine's planned 5-13 kV dees, where multipactor bands are widest: a 1971 operating-lab remedy with a concrete magnitude to scale from. Bias works by breaking the multipactor resonance condition; what trajectories do in detail depends on the local fields, so 'sufficient to control' is found empirically - exactly as Nevis wrote it.
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Commission in activation-safe stages, as Nevis did: first debug the source and central region with the beam stopped at small radius in low-Z (graphite) targets - which at their inner-radius conditions avoided neutron production and induced activity - then survey full-radius behavior at drastically reduced duty cycle before any full-intensity running.
stage 1: beam dumped at r < 10 in. on graphite; stage 2: full radius at ~1 source pulse/secSource quote & editorial note
stopping the beam at r < 10 in. radius in graphite targets. This avoids neutron production and induced cyclotron radioactivity
Editorial note, tabletop extrapolation: The staging discipline transfers to every machine even where activation does not: low-duty, small-radius-first commissioning also protects septa, collectors, and instruments. Stage one's activation-safety is species- and energy-specific, not automatic - deuterons on carbon make neutrons above ~0.33 MeV via 12C(d,n), and D-on-D in any deuterium-loaded surface is thresholdless - so re-establish the claim whenever species or energy changes.
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Track radiological teardown work against a plan and a target: Nevis's ten-week, 2000-ton teardown held all workers below 100 mrad/week averages, most below 25 - the quoted record; the cooling delays and strip-down sequencing are the report's account of how (scan re-read queued).
cooling delay + staged strip-down + weekly per-worker dose trackingSource quote & editorial note
with all workers averaging below 100 mrad/week, and most below 25 mrad/week for the 10 weeks of this activity
Editorial note, tabletop extrapolation: Dose scale is irrelevant to a 150 keV proton machine, but the pattern — cooling time, planned sequence, measured-not-assumed exposure — is the template for any future activated-hardware work and for the plan's licensing narrative.
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Line surfaces struck by lost beam to REDUCE activation of the structure behind them: Nevis expected marble pole liners 'to reduce sector iron, etc., activation' - stray beam deposits in the stone instead of iron and copper.
marble (CaCO3) liners over pole/sector iron in beam-loss regions - reduction, not elimination (the stone itself activates at Nevis energies)Source quote & editorial note
We expect to use marble pole liners where possible, as in the past, to reduce sector iron, etc., activation
Editorial note, tabletop extrapolation: A higher-energy note, with a scale-free idea inside: CHOOSE what lost beam hits. At any scale that choice already governs sputter contamination and outgassing; it becomes activation-relevant the moment a machine crosses into neutron or few-MeV territory - with thresholdless capture the standing exception to 'negligible below a few MeV'.
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When a calculation needs an empirical constant, measure it in the real field environment: Nevis found the effective mu experimentally by measuring the field from a precisely known conductor configuration, fitting mu = 5 to better than 1% for its septum image-field model (images scaled by the image coefficient (mu-1)/(mu+1)).
septum fields = conductors + 5 image sets scaled by (mu-1)/(mu+1); measured fit gave mu = 5 to <1%Source quote & editorial note
The value of mu used was found experimentally by measuring the field from a precisely known configuration of conductors
Editorial note, tabletop extrapolation: A model-calibration pattern for the FEMM pipeline: one known-geometry measurement (a wire loop, a known coil) in the actual gap BENCHMARKS the model at that operating point - repeat at several magnet currents and locations before trusting the saturation model across the map; one point pins one point, not the whole BH curve.
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Taper an extraction-channel septum from thin at the entrance to thick downstream, where measured orbit clearance has grown: Nevis's 0.125-in entrance thickening to 0.600 in by 16 in along the channel cut septum power to 40 kW, a factor of four below keeping the entrance thickness throughout, and made room for a larger cooling passage.
Nevis: 0.125 in. entrance -> 0.600 in. by 16 in. along channel; power 160 kW-equivalent -> 40 kW (4x)Source quote & editorial note
This septum will use only 40 kW of power, a factor of four smaller than if the original thickness were kept to the end
Editorial note, tabletop extrapolation: A current-septum channel is beyond tabletop needs, but the geometric principle - septum thickness need only be minimal on the first intercepting turn - applies to any conductive deflector septum on a next machine, subject to the beam-clearance check downstream. (Extraction FOILS are a different problem: stripping, scattering, heating and lifetime set foil thickness, not turn separation.)
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Interlock actively cooled beam-intercepting conductors individually: Nevis gave each septum wire its own thermocouple on the cooling water, tripping the channel current on any rise, with the loop running filtered, de-ionized water in the report's practice. A loaded, cooled conductor fails quickly on loss of flow - the trip must be fast.
per-wire thermocouple -> fast current trip; filtered + de-ionized cooling loopSource quote & editorial note
each wire will have its own thermocouple to sense any rise in the cooling water temperature which will shut off the current in the channel
Editorial note, tabletop extrapolation: Per-element thermal interlocks scale down perfectly - the RF amplifier dummy load, water-cooled dee stubs, any powered septum - and match the fail-safe doctrine (dg-1110). A coolant-temperature sensor only responds after heat reaches the water: pair it with a flow interlock (dg-202's return-orifice practice) so loss of flow trips the supply without waiting for temperature to say so.
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Adiabatic RF manipulation at the Nevis parking point: with the beam parked where df/dt ~ 0, a slow linear reduction of RF amplitude spreads the phase angle near-adiabatically - DEbunching the beam: phase width grows while energy-oscillation amplitude shrinks (the duration and the ~3x figure are the report's numbers - re-read queued).
slow linear V_RF turn-off at df/dt ~ 0 "parking frequency" -> ~3x reduction in phase-oscillation dESource quote & editorial note
a slow linear reduction (turn off) of the RF amplitude there will result in a near adiabatic spreading out of the phase angle
Editorial note, tabletop extrapolation: Swept-frequency machinery, not fixed-frequency CW territory - the design space it illustrates (adiabatic capture, slow parameter ramps judged against the phase-oscillation period, not a fixed microsecond count) belongs to any future synchro- or synchrotron-class RF program.
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Buy shielding with geometry before mass, as the Nevis layout does: the underground beam stop aims away from occupied areas - which the report says greatly eases shielding and background - with secondary beams taken off at large angles and bends between production targets and experimenters.
beam stop aimed away from people; large-angle takeoff; bends between target and experimenters (the report's layout choices)Source quote & editorial note
Since the underground beam stop is aimed away from the experimental areas, this greatly eases shielding, and subsequent background problems
Editorial note, tabletop extrapolation: Direction-dependence of secondary radiation is universal even though the 550-MeV numbers are not: orient any future target station and Faraday-cup dump so the forward cone points at mass, not people. The specific takeoff angles and bend counts are per-facility physics rather than constants - lay out first, then let the survey confirm the geometry did what was expected.
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Moyer's shielding datum: about 6 inches of iron (or equivalent) per factor-of-two attenuation - the report's figure for its forward high-energy neutron cone, with softer large-angle spectra attenuating far faster; shield thickness is budgeted per direction.
~6 in Fe per x2 (the report's forward-cone figure); direction-dependent - the report's large-angle spectra attenuate much faster (details: scan re-read queued)Source quote & editorial note
require - 6 in. Fe (or the equivalent) for each factor of 2 attenuation
Editorial note, tabletop extrapolation: Pure high-energy datum — no tabletop relevance except as a worked example of directional shielding budgets, but it anchors the energy scaling.
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Design components in activated regions for remote replacement: Nevis designed all dee SUPPORT INSULATORS to be removable and replaceable by remote handling tools - the quote; the wider behind-shields work practice is the report's context.
activated-region components = pin-located, tool-accessible, removable without entering the chamberSource quote & editorial note
all support insulators have been designed so that they can be removed and replaced by remote handling tools.
Editorial note, tabletop extrapolation: At tabletop energies the driver is vacuum hygiene and downtime rather than dose, but the same design habit — most-likely-to-fail parts (insulators, filaments, septa) replaceable without major disassembly — is what the reference machine's filament-change experience already argues for.
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Build accelerator safety interlocks to the 1974-era trend or better: fail-safe circuitry with self-checking - the properties the era's designs pursued as they moved to solid state - so that component failures and stuck states reveal themselves instead of silently defeating the interlock.
fail-safe + self-checking logic; solid state preferred over relays (NBS Handbook 107 lists general requirements)Source quote & editorial note
The trend seems to be toward more elaborate systems which utilize solid state devices, fail-safe circuitry and self-checking circuits.
Editorial note, tabletop extrapolation: Directly actionable for the next machine and the tiny controls spec: an amateur interlock chain (door, HV, RF-enable, radiation monitor) should be fail-safe and self-testing. Those properties come from the circuit design, not the device family - solid-state parts can fail shorted - so the design proves de-energize-to-safe behavior and exercises each channel periodically. What was state of practice in 1974 is trivially cheap in 2026.
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Subject safety-critical circuits to sneak-circuit analysis: hunt for unplanned operating modes such as relay races, sneak grounds, and power-supply crossties before trusting an interlock chain.
sneak-circuit review checklist: relay races, sneak grounds, power-supply crossties (Rankin, Nuclear Safety 14:5)Source quote & editorial note
techniques of dealing with problems such as relay races, sneak grounds and power-supply crossties
Editorial note, tabletop extrapolation: Fully transferable and cheap: a deliberate review pass asking 'what unintended path can energize the HV or open the shutter' on the interlock schematic - a shared ground defeating an enable line is exactly the class it hunts. One pass finds sneak paths on paper; it does not validate the built system, so it complements, never replaces, fail-safe design and periodic function tests (dg-1110, dg-1065).
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Take the fast-neutron half-value thickness of ordinary concrete for cyclotron-target neutrons as approximately 10 cm (ORNL measurement over thick C, Al, Cu, Ta targets under proton, deuteron, alpha, and carbon beams).
HVT(ordinary concrete, cyclotron-target fast neutrons) ~ 10 cmSource quote & editorial note
fixes the half-value thicknesses of ordinary concrete for neutrons from cyclotron targets at approximately 10 cm
Editorial note, tabletop extrapolation: The corpus's first literal shielding number for MeV-class cyclotron neutrons. The reference machine's proton operation sits below its (p,n) thresholds and makes none - deuteron operation is the standing exception (D-D is thresholdless) - and this ~10 cm HVT is the sizing constant the moment any machine or D-beam work crosses into neutron production; it was measured for cyclotron-target spectra, so re-check it for a materially different spectrum.
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Formalize the safety function as the program grows - the 1974 survey's observed practice: 'there is often a safety officer appointed', many installations have review committees, and written guidance existed in the era's handbooks (NBS 107, TID-23992).
safety officer + independent review + written program (models in NBS 107, TID-23992)Source quote & editorial note
There is often a safety officer appointed. Many installations have safety review committees.
Editorial note, tabletop extrapolation: For a one-person program the transfer is external review - the archive's cross-review protocol is exactly this committee function. For the planned educational-accelerator business, whether a named safety officer and a written program are REQUIRED is the jurisdiction's call (/legal/); the survey records the practice, and the practice is worth adopting either way.
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Adopt the exposure design philosophy the source's era called ALAP (As Low As Practicable) - not merely staying under limits, but reducing further wherever technology and economics permit - and recognize it works only as a standing management commitment. Modern regulation's successor term is ALARA, As Low As REASONABLY ACHIEVABLE, with its own regulatory definition.
design target: exposures as far below limits as practicable/reasonably achievable (era: ALAP, AEC Reg. Guides 8.8/8.10; modern: ALARA, 10 CFR 20)Source quote & editorial note
the As Low As Practicable philosophy can be adopted and put into practice only where there is a firm commitment by management to do so
Editorial note, tabletop extrapolation: The governing philosophy any licensing narrative must speak fluently - in its modern wording (ALARA), since the terms are not interchangeable in a regulatory context. For the home program it means shielding and interlock decisions justified as 'as low as reasonably achievable', not 'under the limit'.
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Measure shield attenuation with the machine itself as the source - the quoted apparatus: a slab of the candidate material (3 ft x 3 ft x thickness), a detector recessed in a small cavity in a concrete igloo, and a beam MONITOR, whose evident role - normalizing detector readings to source intensity - is the method's point (Moyer's own analysis text: scan re-read queued).
attenuation = (detector/monitor) vs slab thickness; slab 3'x3', detector in 1.5-inch cubical cavitySource quote & editorial note
A - Slab under test. Dimensions 3' x 3' x thickness. C - Concrete "Igloo". D - Detector, in cubical cavity 1-1/2" edge. M - Beam moniter [sic]
Editorial note, tabletop extrapolation: A shielding survey needs no separate neutron source — run the machine at a reference beam current and take detector-to-monitor ratios; the monitor normalization is what makes readings taken hours apart comparable.
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Keep survey electronics out of the magnet fringe field: use passive detectors (ionization chambers) at the measurement point with DC amplification, and put the indicating meters where the field cannot bias their movements.
Source quote & editorial note
The monitor and detector employed were aluminum-walled ionization chambers, with DC Amplification, indicating on microammeters placed outside the magnetic field of the cyclotron.
Editorial note, tabletop extrapolation: Analog meter movements and photomultipliers misread in modest stray fields (PMTs at well under a millitesla); GM tubes themselves are largely field-insensitive, though their electronics may not be. The transferable practice is the source's separation: passive sensing volume at the measurement point, readout where the field is negligible - verified by moving the readout and watching for a change.
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Expect transition (buildup) effects at the front face of a shield in fields like Moyer's: attenuation becomes exponential only after the radiation reaches equilibrium with the secondaries it generates, so fit half-value thicknesses to the displaced linear portion of the curve - never to the first layers.
fit exponential slope only beyond the equilibrium (buildup) depth; extrapolation of the linear portion back to zero is displaced from the no-absorber readingSource quote & editorial note
The transition effects occur as the neutron beam approaches equilibrium with the secondary and scattered particles produced in the absorbing medium.
Editorial note, tabletop extrapolation: A dosimeter just behind the first inches of shielding can be measuring the buildup region rather than the attenuation slope, so thin-shield tests can misestimate a thick shield in either direction. How pronounced the transition is depends on the field and geometry; the transferable part is the fitting discipline - use the asymptotic slope.
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Layer order matters in composite shields: hydrogenous material following a high-Z layer can RAISE the ionization reading behind it — Moyer measured a paraffin transition increase of 60% following iron and 100% following lead — because the hydrogenous layer converts neutron flux to ionizing protons.
Moyer's ionization readings behind paraffin: +60% following Fe, +100% following Pb, in his geometry and chambers - a measured transition effect, not a general dose identitySource quote & editorial note
Paraffin yields a transition increase of 60% following Fe, and of 100% following Pb with similar geometry.
Editorial note, tabletop extrapolation: When adding polyethylene or paraffin outside a metal chamber wall, a survey reading between the layers or behind too thin a hydrogenous layer can exceed the bare-wall reading - recoil protons from the hydrogen. Make the hydrogenous layer thick enough to absorb the recoils it creates, and take the dose reading OUTSIDE the complete stack: interlayer readings are diagnostics, not the answer.
Cited in: Shielding a Small Cyclotron
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Threshold-activation detectors sandwiched between absorber slabs gave attenuation half-values 'generally... with better precision than those with ionization chambers' - the quoted comparison for the carbon-disc experiments; their design virtues (threshold blindness to low-energy scatter, passive in-field operation) are the method's logic rather than the quote's claims.
activation of a threshold-reaction foil vs absorber depth -> half-value thickness; Moyer used C12(n,2n)C11, threshold ~20 MeVSource quote & editorial note
Experiments using carbon disc detectors sandwiched between slabs of absorber gave exponential attenuation with half-value determination which were generally made with better precision than those with ionization chambers.
Editorial note, tabletop extrapolation: The C12(n,2n) reaction itself is blind below ~20 MeV and useless at sub-MeV neutron energies; the transferable idea is the energy-thresholded activation foil as a passive, field-immune detector that answers one question cleanly.
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State the geometry with any published attenuation number: with detectors close behind slabs, the measured cross section is neither pure absorption nor pure scattering removal, and a half-value thickness from one geometry does not transfer to another.
Source quote & editorial note
Because of the geometry employed, these measurements are neither a true determination of pure scattering nor pure absorption.
Editorial note, tabletop extrapolation: Handbook removal cross-sections assume corrected geometry; a home measurement's bias depends on the arrangement - a narrow-beam, small-acceptance setup excludes scatter and reads MORE attenuating than a broad shield really performs, while a detector bathed close behind a slab collects scatter and reads pessimistic. State the geometry with the number, as the rule says, and compare only like with like.
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Choose fast-neutron shielding for high density combined with LOW atomic number; the attenuation cross section per nucleon falls as Z rises (nucleons shadow each other inside a large nucleus), which is why ordinary concrete outperforms lead per unit weight against neutrons.
sigma per nucleon decreases with Z (shadow effect); merit ~ density x (hydrogen + light-element fraction)Source quote & editorial note
one should seek substances which combine high density with low atomic number. Among convenient and practical materials none would seem better than concrete.
Editorial note, tabletop extrapolation: The shadow-effect argument is a >100 MeV argument. At low energy the conclusion usually still favors hydrogenous materials - elastic scattering on hydrogen dominates moderation - but merit depends on the objective: moderation, capture, dose, or secondary-gamma control (hydrogenous shields buy moderation with 2.2 MeV capture photons, dg-1329). Concrete, water and polyethylene win per dollar for neutron MODERATION, with the gamma bill accounted separately.
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Shield for machine-generated loss points, not just the target: besides the forward cone from the probe, Moyer found 'a general spray of neutrons due to the deuteron beam grazing the interior of the dee' - his report characterizes its intensity and azimuthal extent (scan re-read queued for those figures).
Source quote & editorial note
Besides the neutron beam cone from the probe there was found to be a general spray of neutrons due to the deuteron beam grazing the interior of the dee.
Editorial note, tabletop extrapolation: Wherever beam is lost - dee edges, septum, probe stalk, chamber wall - is a candidate source, and a survey plan that only looks downstream of the target can miss most of the emission solid angle. Moyer's spray was found by surveying: that is the lesson.
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Survey slow-neutron leakage through access openings separately with a BF3 (or equivalent thermal) counter: apertures and penetrations, not the bulk shield, set the slow-neutron field outside an enclosure.
Source quote & editorial note
Measurements with a BF3 proportional counter have indicated diffusion of slow neutrons through various access openings from the enclosure.
Editorial note, tabletop extrapolation: Cable ways, viewport lines-of-sight and door gaps are where slow-neutron leakage concentrates ONCE the bulk shield is adequate - penetrations dominate when the walls no longer do, which is the regime a designed enclosure should be in. Thermal-neutron instruments answer a different question than fast-neutron ones; both belong in a survey.
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Publish shield performance as a normalized dose map tied to beam current: Moyer quotes 24 r/hr at 1 ft outside the tank wall falling to 10 mr/hr outside 5.5 ft of concrete and 0.5-1.5 mr/hr in the building at large, all explicitly at 0.2 uA of deuterons — so any later reader can rescale.
report dose rate AND beam current together; at fixed geometry, energy, species and loss pattern, dose rescales with current - any of those changing breaks the rescaleSource quote & editorial note
With an ionization reading of 24 r/hr in the center of the neutron beam cone 1 foot outside the tank wall (9 3/4 feet from the probe), the ionization just outside the shielding in the center of the beam is 10 mr/hr, while the general building areas are 0.5 to 1.5 mr/hr. These quoted measurements are made with Al-walled ionization chambers, and correspond to a deuteron beam of about 0.2 x 10-6 amp.
Editorial note, tabletop extrapolation: A survey number without the simultaneous beam current is unusable later: log dose rate, location, instrument, and Faraday-cup current as one record so the map rescales when beam current grows - and re-survey when anything besides current changes (energy, species, tune, loss pattern), because those break the linear rescale.
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Scale-model law for RF resonators (skin-effect-dominated, geometrically similar): a 1/2-scale model runs at 2x frequency with L and C halved; its Q is 0.7x (1/sqrt 2) the full-scale Q and it needs 1.4x the proportional power for a given dee voltage.
f_model = s*f_full; L,C scale 1/s; Q_model = Q_full/sqrt(s); P_model = sqrt(s)*P_full at equal V (s = 2 for half scale); assumes similar materials, surfaces and conductor-loss dominanceSource quote & editorial note
The Q of the model will be 0.7 times the Q of the actual installation and so will require 1.4 times as much power for a given dee voltage.
Editorial note, tabletop extrapolation: Bench-model a dee-stem or resonator geometry at reduced size before cutting full-size copper, applying the sqrt(scale) Q correction to power comparisons - and determine coupling separately, from impedance or measured external Q: the power ratio says nothing directly about what a tap or loop must pick up.
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Pick the model scale so a real, available tube is a valid stand-in for the power tube: MacKenzie abandoned a 1/4-scale model because at 100 Mc electron transit-time effects falsified the oscillator's behavior on the fundamental, then chose 1/2 scale where an available tube could represent the big one faithfully.
model frequency must stay low enough that tube transit-time effects remain negligibleSource quote & editorial note
It was not excited satisfactorily due to the fact that at 100 megacycles the transit time effects were quite noticeable on the fundamental mode.
Editorial note, tabletop extrapolation: Cold measurements scale approximately - eigenfrequencies and field patterns follow geometry, while Q, losses, contacts and probe loading need corrections or direct measurement. Any POWERED model test needs a driver checked for transit angle and loading at the model frequency; otherwise the model exhibits modes the real system never sees, and vice versa.
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Where geometry is complicated, trust model tests over calculation: MacKenzie preferred a mechanically awkward layout that could only be settled empirically, noting that dimensions calculable "fairly exactly" were the sole advantage of the calculable variant.
Source quote & editorial note
dimensions can be calculated fairly exactly whereas in the system shown in Figure 5 one must depend on model tests (which are safer anyway).
Editorial note, tabletop extrapolation: Transmission-line formulas ignore end effects, bends, and support hardware; for any resonator whose geometry is not a textbook line, a cheap model measurement outranks the calculation it checks.
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Take a mode census before applying power: the MacKenzie model was excited by a separate oscillator to map its resonances, unwanted modes were suppressed with wavetraps - a pair slightly staggered in tuning covering a small frequency band - and six wavetraps sufficed for the whole proton range. The suppression was NOT complete with the dee shorted, as occurs in a discharge.
Source quote & editorial note
excited by a separate oscillator ... It was suppressed with 2 wavetraps slightly staggered in tuning to cover a small frequency band ... A total of 6 wavetraps sufficed to suppress all unwanted modes throughout the proton range. The parasitic modes were not completely eliminated, however, when the dee was shorted, as would occur in a discharge.
Editorial note, tabletop extrapolation: Sweep the assembled dee/stem/liner system with a signal generator and probe before first power-up; every resonance within the amplifier's gain bandwidth is a candidate parasitic. Repeat the survey for fault-like boundary conditions - a dee spark momentarily retunes the system into modes the clean census missed, exactly the source's shorted-dee exception.
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Suppress an unwanted mode by making it lossy rather than by shifting it: MacKenzie discouraged the parallel mode by grounding the rotor supports and making them fairly high resistance - the wrong modes, needing large currents through that resistance, simply fail to oscillate in favor of the much-higher-Q correct mode.
Source quote & editorial note
It was found that the parallel mode was discouraged by grounding the supports ... two of them require that large currents flow in the rotor supports, which can be made fairly high resistance. These modes are therefore not excited in favor of the much higher Q correct mode.
Editorial note, tabletop extrapolation: Mode-selective damping - resistance placed at a current maximum of the unwanted mode and a current null of the wanted one - is a powerful alternative to tuning the parasite out of band. Verify with a current map that the wanted mode's null is real (an imperfect null costs Q), and check the resistive element's dissipation and temperature at power.
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An electrically long conductor with its return path forms a transmission line: MacKenzie's long metal rotor supports, mounted on insulators, act as open lines with the voltage maximum at the open (insulator) end - stressing the insulators at about 3 times the rotor voltage in that geometry.
open-ended support of length near lambda/4 multiplies RF voltage at its free end; here ~3x rotor voltageSource quote & editorial note
the insulators will be subjected to about 3 times the rotor voltage to ground. This is because the long metal supports act as open transmission lines
Editorial note, tabletop extrapolation: Check the electrical length of every support, cooling line, and instrument stalk inside the RF volume against its actual return path and termination (loaded lines behave differently from open ones): a mechanically convenient standoff can sit at a voltage antinode and flash over at dee voltages its rating should easily hold. The 3x is MacKenzie's installation, not a universal factor - model or measure your own.
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When dee voltage dips to zero at one specific frequency, hunt for a hidden resonant structure absorbing the power: MacKenzie traced such a null to the meshed condenser teeth acting as a long folded transmission line (the frequency and the overlap-length arithmetic are the report's diagnosis - re-read queued).
folded-line parasitic resonance when (tooth overlap) x (number of meshed teeth) ~ lambda/2Source quote & editorial note
The oscillating circuit actually is a long folded transmission line consisting of the two rows of meshed teeth.
Editorial note, tabletop extrapolation: The diagnostic transfers as a leading suspect, not a verdict: a sharp frequency-specific dead spot MAY be a resonant conductor assembly (screen, liner seam, feedthrough array) - confirm with low-power sweeps, probing or damping tests before modifying the structure, since matching faults, mode coupling and measurement artifacts produce nulls too. When confirmed, fix by shortening or breaking up the structure, not by driving harder.
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Prove a parasitic stays out of band across the whole tuning range by checking the worst case - in the cited meshed-tooth tuner, if the transverse mode was still above the fundamental when fully meshed (the closest approach), it stayed above at every partial meshing.
Source quote & editorial note
if the frequency of the transverse mode is still higher than the fundamental when the teeth are fully meshed, then the transverse frequency will always lie above the fundamental for any partially meshed position.
Editorial note, tabletop extrapolation: For any tunable element (trimmer panel, movable shorting plane): where analysis or a coarse sweep establishes that the mode separation varies monotonically with travel, one measurement at the converging extreme clears the range; otherwise sweep the full travel and watch for additional or avoided crossings.
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Couple the drive at a point whose voltage is insensitive to tuning: on the 3/4-wave system, the quarter-wave-shorted stub line's voltage stays practically the same as the dee voltage over about a 2:1 frequency shift, so an oscillator tapped there sees a far gentler coupling problem as the system sweeps.
Source quote & editorial note
over about a 2 to 1 frequency shift, the voltage on the 1/4 wave-shorted line (which will be referred to as the "stub" line) is practically the same as the dee voltage.
Editorial note, tabletop extrapolation: Even a fixed-frequency machine drifts with thermal expansion and plasma loading, and feeding at a voltage-stable point of the resonator helps - but a stable voltage RATIO is not constant drive impedance: detuning, Q and plasma loading still move what the amplifier sees, so measure the input impedance (or S11) across the expected drift and loading range before promising the amplifier anything.
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Empirical procedure for locating a drive tap on the cited stub-line topology: start with the tap at the end of the stub line and move toward the shorted end until the tube draws rated plate current at rated plate voltage.
Source quote & editorial note
start with the tap at the end of the stub line and then move toward the shorted end until the tube draws rated plate current at rated voltage.
Editorial note, tabletop extrapolation: The walk-the-tap idea transfers as a method of converging on coupling empirically rather than committing to a computed position - executed safely: find the initial setting at low power or with a VNA, move taps only de-energized, approach the operating point with current limiting, and watch plate current AND dissipation AND reflected power together - rated plate current alone is one indicator, not proof of match, and the line's high-impedance end carries hazardous RF voltage.
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Build small mechanical length adjustment into every coupling line instead of calculating exactly: end effects and bends cause enough variation that the report concluded the line length should be adjustable by a small amount.
Source quote & editorial note
End effects and bends in the line can cause this much variation. The conclusion is that there should be some possibility of varying the line length by a small amount
Editorial note, tabletop extrapolation: Design connection lines and stubs with a sliding section or trombone whose travel comes from a tolerance analysis (component-value uncertainty, bends, end effects) or a prototype sweep - the calculation gets you to the right neighborhood and the adjustment does the rest.
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In the cited grounded-grid drive chain, phase shift was controlled by making the filament-grid capacity large, so the out-of-phase RF current is large compared with the in-phase electron emission current.
mechanism: I_reactive = V*omega*C_gf >> I_emission reduces the emission-current phase pull (cited circuit)Source quote & editorial note
the shift is reduced by making the filament grid capacity large, so that the out of phase r.f. current will be large compared with the in phase electron emission current.
Editorial note, tabletop extrapolation: The mechanism matters for any self-excited tube oscillator on a dee - drive phase error costs efficiency - and padding the input capacity is a candidate fix, not a free one: the added reactive current changes loading, bandwidth and possibly parasitic resonances, so verify the full input network after the change. Check total drive phase with an incident/reflected-wave measurement.
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Predict full-scale RF power from model measurements and state both numbers: 400 W (48 Mc) and 600 W (18 Mc) of model input for 1500 V on the dee scaled - via V-squared and the sqrt(2) Q correction - to 28 and 42 kW for 15 kV; MacKenzie also flags that the model's bad joints and brass surfaces bias it pessimistic against the copper full-scale build.
P scales as V^2 x (Q_full/Q_model)^-1; model bad joints/brass make prediction conservativeSource quote & editorial note
The 1/2 scale model uses about 400 watts input to the oscillator at 48 megacycles and 600 watts input at 18 megacycles to produce 1500 volts on the dee.
Editorial note, tabletop extrapolation: Dee power scales as voltage squared: measure watts-per-volt-squared on the bench and the amplifier requirement for any target voltage falls out. Mind the quantity - the model figures are OSCILLATOR INPUT, so the scaled 28-42 kW carries the model oscillator's efficiency inside it: separate wall loss from drive-chain overhead when budgeting a modern amplifier (dg-313, dg-316), and budget for joint quality and surface material shifting Q.
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Keep an availability ledger: divide every scheduled hour into operating (beam-on-target / beam adjustment / target setup / development) and outage by cause, each as a percentage of scheduled time. A professionally staffed national-lab cyclotron logged only 60.1% operating and 39.9% outage over a half year.
scheduled time = operating (beam-on + adjustment + setup + development) + categorized outage; NRL Jul-Dec 1969 = 1382.5 h, 60.1%/39.9%Source quote & editorial note
Total Operating Time 831.3 ... 60.1 ... Outage Total 551.2 ... 39.9 ... Scheduled Operating Time 1382.5
Editorial note, tabletop extrapolation: A run log that records why each session ended, in fixed categories, turns anecdote into a failure Pareto within a year. The NRL 60/40 split is one professionally staffed machine's half-year - a sobering calibration, not a forecast: build the spare-time machine's own ledger and let it set expectations.
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Rank downtime by category and spend reliability effort by the ranking: NRL's half-year outage Pareto put power supplies at 10.2% and vacuum at 9.3% of ALL scheduled hours, far ahead of RF (1.6%) and ion-source/filament changes (1.0%).
NRL outage by category (% of scheduled): power supply 10.2, vacuum 9.3, electrical 3.3, mechanical 2.7, RF 1.6, source/filament 1.0Source quote & editorial note
Vacuum 128.6 ... 9.3 ... R. F. 22.1 ... 1.6 ... Power Supply 140.4 ... 10.2
Editorial note, tabletop extrapolation: The transferable content is the Pareto METHOD on your own log, not NRL's ranking: on that machine in that period, unglamorous supply and pump maintenance was where uptime was bought - a small machine's ranking may differ, so measure before allocating effort.
Cited in: The Vacuum Budget of a Cyclotron
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Budget for transition overhead: in NRL's 1382.5-hour schedule, start-up/shutdown consumed 5.6% and beam tuning another 4.0% - together roughly a tenth of scheduled time spent getting into and out of running condition.
NRL: start-up/shutdown 77.5 h (5.6%) + beam tuning 55.0 h (4.0%) of 1382.5 scheduled hoursSource quote & editorial note
Beam Tuning 55.0 ... 4.0 ... Start Up and Shutdown 77.5 ... 5.6
Editorial note, tabletop extrapolation: Pump-down, filament conditioning, and field settling are largely per-session costs on a small machine; if your own log confirms that, batching experiments into fewer, longer sessions raises the beam-on fraction - measure the local session overhead first rather than assuming NRL's accounting transfers.
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Develop in parallel with operation, and expect major changes to require shutdown: NRL ran development alongside cyclotron operation, with major modifications waiting on machine shutdown (the shutdown-scheduling specifics are the report's account - re-read queued).
Source quote & editorial note
In most cases development is in parallel with operation of the cyclotron. However, major changes may require shut-down of the cyclotron for these modifications to be effected.
Editorial note, tabletop extrapolation: Grouping every open-the-chamber job (seal replacement, source work, new feedthroughs) into one planned vent-and-rebuild window costs one pump-down and one reconditioning instead of many - sound practice on its own logic, whatever NRL's exact schedule was.
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Latch and store the location of every fault: some faults (magnet overtemperature) clear themselves before the operator can find the tripping sensor - the quoted need for 'a device... which could detect and store the location of a large number of possible faults'.
Source quote & editorial note
This may happen before the operator can determine the sensor causing the fault condition. Therefore, a device was needed which could detect and store the location of a large number of possible faults.
Editorial note, tabletop extrapolation: Any interlock chain needs fault capture - latching relays, or a logged timestamp per sensor; per-sensor timestamps also give first-out ORDERING, which turns a cascade of consequential trips back into its primary cause. Without capture, intermittent faults (thermal, flow, vacuum burps) become undiagnosable ghosts that waste sessions.
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Classify faults into two tiers: priority faults that must be corrected before operation continues (annunciation cannot be cleared while the fault stands) and non-priority faults that may be acknowledged and bypassed (a failed roughing pump) while their indication stays displayed until fixed.
Source quote & editorial note
One is assigned as priority faults, errors which must be corrected to continue cyclotron operation ... The other is non-priority faults, such as the failure of a mechanical vacuum pump which may be bypassed and operation continued.
Editorial note, tabletop extrapolation: Hard-wire the chains whose failure is immediately hazardous - radiation monitors, HV enclosure, cooling on powered elements, vacuum-envelope and arc faults, as the machine's own hazard analysis identifies them - so they cannot be acknowledged away, and give genuinely operational faults a bypassable alarm that stays displayed until fixed. The design insight survives: a system where every fault stops the machine trains its operator to defeat interlocks. The tier assignment comes from the hazard analysis, never from a fixed list.
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The NRL machine gated its beam by dropping dee voltage to approximately 50% of normal - below that machine's acceleration threshold - rather than unkeying the RF, keeping the tuning and regulation loops engaged for clean recovery.
beam-off dee voltage ~50% of normal (below threshold but above regulation-loop dropout); switched via the d.c. reference of the dee voltmeter in the regulator loopSource quote & editorial note
the R. F. dee voltage was lowered to approximately 50% of its normal value which is less than the threshold voltage.
Editorial note, tabletop extrapolation: The concept transfers as an experiment, not a guarantee: measure the machine's own beam-versus-dee-voltage curve first (reduced RF can merely move the loss radius inward rather than extinguish ions), verify with a detector that the gated state is beam-off to the level the measurement needs, and check where the residual beam goes. Where true interruption matters, gate the source. Stepping the regulator's dc reference is the clean actuator either way.
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Ramp big-tube filaments from zero: the 6949V1's filament voltage must rise slowly from zero so filament current never exceeds 1,700 A even momentarily - the cold filament's resistance is a fraction of its hot value.
cold-filament resistance is a small fraction of hot; NRL limit 1,700 A inrush on the 6949V1; undercurrent detector removes filament voltage on momentary dropoutSource quote & editorial note
The filament voltage of the 6949V1 must be raised slowly from zero to the normal operating value to prevent filament current from exceeding a value of 1,700 amperes, even momentarily.
Editorial note, tabletop extrapolation: Scales down to any transmitting tube or big thoriated filament: follow the tube maker's warm-up and inrush limits with a soft-start rated for the actual current (variac ramp; an NTC only where its rating and cool-down behavior fit). Guarding against the loose-socket failure (a dropout then full voltage on a cooled filament) is sound engineering - implement it as a properly coordinated undercurrent trip with startup inhibit, as a design addition rather than NRL doctrine.
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Gang mechanically what must track electrically: NRL's four tuning capacitors, each on its own servo, were repeatedly driven to unequal capacities on loss of a translator signal and had to be removed and reset (equal tracking being required for equal RF current sharing and maximum tuning range); one chain drive from a single motor - and no trouble experienced since.
Source quote & editorial note
The four PAA tuning capacitors are now coupled together by a heavy-duty chain driven by a single large servo motor with one translator. No trouble has been experienced since this modification. Formerly, each of the four capacitors was driven by its separate servo motor with a pair of servo motors being fed by one of the two translators. This had resulted in capacitors being driven to unequal capacities upon the loss of a signal from a translator for any of several reasons. This then necessitated the removal of the capacitors to reset them for equal capacity tracking which is required for equal sharing of the RF current and for maximum tuning range.
Editorial note, tabletop extrapolation: Wherever two adjustments must hold a FIXED mechanical relationship (paired trimmers, symmetric shorting planes), a shaft, chain, or belt enforces the constraint by construction, with backlash and stretch as the residual error terms; keep independent trim where the relationship must be calibrated rather than fixed - software matching isn't doomed, but it reintroduces the desync failure class the chain removed.
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Measure dee-voltage modulation as a number and drive it down at the source: NRL's master oscillator proved to vary with frequency and contain undesired components that appeared as dee-voltage modulation and could not otherwise be eliminated; replacing it with a frequency synthesizer solved it, cutting modulation (p-p ripple as a percentage of peak RF) from 1.5% to about 0.5%.
modulation metric = (p-p ripple on RF envelope)/(peak RF) x 100%; NRL 1.5% -> 0.5% by replacing oscillator with synthesizerSource quote & editorial note
The output voltage of the radio-frequency oscillator for the cyclotron proved to vary with frequency and to contain undesired frequency components. At some particular operating frequencies, the undesired frequencies appeared as modulation of the dee voltage and could not be eliminated. These problems were solved by replacing the oscillator with a frequency synthesizer. ... The modulation on the dee voltage, defined as the peak-to-peak ripple riding on the RF voltage as a percentage of the peak RF value, has recently been reduced to about 0.5% from 1.5%.
Editorial note, tabletop extrapolation: Dee-voltage ripple modulates per-gap energy gain (and, through phase slip, orbit phase where the machine is off-isochronous); put the envelope from a calibrated RF pickup on a scope, log the percentage, and remember the excitation source - a cheap generator's spurs included - is a candidate cause before blaming the amplifier or resonator.
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Motion feedthroughs are a seal failure class of their own: the Buna-N chevron-stack seals on NRL's source drive mechanisms were unreliable and short-lived (the replacement construction is the report's account - re-read queued).
Source quote & editorial note
The Buna N, chevron shaped vacuum seals between the cyclotron accelerator tank and the radial and azimuthal drive mechanisms ... were unreliable and displayed a short life expectancy.
Editorial note, tabletop extrapolation: For sliding or rotating shafts into the chamber, write a real dynamic-seal specification: compound, gland dimensions and squeeze, surface finish and land tolerance, lubrication, the motion profile, and an interseal vent or differential-pumping stage where leak-tightness matters - geometry, finish and compound all do real work, and a second O-ring buys redundancy at the cost of friction and a possible trapped-volume virtual leak.
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Optically re-align the ion source after reinstallation: NRL aligned the discharge aperture (0.09 x 0.50 inch slit) to the magnetic median plane and the dee electric field after reinstalling the source assembly.
Source quote & editorial note
After reinstallation of the ion source assembly into the cyclotron, the ion discharge aperture (0.09 in x 0.50 in) was optically aligned with respect to the median plane of the cyclotron magnetic field and the electric field of the dee.
Editorial note, tabletop extrapolation: Source aperture height and tilt relative to the median plane strongly affect first-turn survival; make re-alignment after source maintenance a fixtured, measured step (scribe lines, a sighting jig, or a depth gauge) instead of trusting bolted repeatability.
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Magnetic forces deform current-carrying structures in service: the NRL channel's fix was accepted only after measurement - with the coils at 3500 A, inner-wall deflection was about 0.002 inch, judged negligible (the collapse history, G-10 stiffener fix and motor relocation are the report's narrative - scan re-read queued for those specifics).
verify a structural fix by measuring deflection at above-operating excitation and comparing induced stress to elastic limitSource quote & editorial note
with the coils energized to 3500 amperes, revealed a negligible deflection of the inner walls (about 0.002 inch) which eliminated the possibility of future collapse
Editorial note, tabletop extrapolation: Every conductor near the pole gap feels J x B: thin walls, septa and coil leads need structural qualification, and a displacement measurement at above-operating excitation is one ingredient of it, not the whole - add the load calculation, yield and buckling margins, fatigue for cycled excitation, and fault-current loads. Motors, encoders and anything with a magnetic circuit belong outside the fringe field regardless.
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Cooling-water plumbing impedance can be the real limit on dee voltage: NRL raised 6949 anode flow from 42 to 60 gpm by adding a 4-inch return pipe separating the high- and low-pressure loops - doubling allowable anode dissipation, which 'permits operation with higher dee voltages at the higher frequencies' - and installed a standby demineralized-water pump in a parallel loop specifically to cut future pump outages.
shared return headers add series impedance to every branch; separate supply/return loops per pressure class; standby pump in parallelSource quote & editorial note
Changes in the cooling water path for the 6949V1 anode increased the flow rate sufficiently that the allowable anode dissipation was doubled. This increased anode dissipation permits operation with higher dee voltages at the higher frequencies with a margin of safety for detuning of the anode circuit. ... we increased the flow rate to the 6949 tube plates from 42 gpm to 60 gpm by the addition of a 4-inch return pipe to separate the high pressure and low pressure water loops ... In an attempt to decrease future outages due to water pump failure, the mechanical and structural installation of a standby 200HP, 1400 gpm, 150 psi, demineralized water pump was completed with associated plumbing that places it in a parallel loop with the existing low pressure demineralized pump.
Editorial note, tabletop extrapolation: When an amplifier cannot hold rated dissipation, check hydraulic head losses in shared manifolds before derating the tube; and duplicating a single-point-of-failure pump is a reliability purchase the outage ledger justifies - engineered in, with isolation valving and controls, not just teed into the pipe.
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Utilization benchmark from a mature research cyclotron: 1,680 hours of operation in one quarter - about 18 hours per day - with the reported unscheduled losses being three days to a cold-trap refrigerator failure and one day to low diffusion-pump oil.
1680 h / 92 days ~ 18.3 h/day operatingSource quote & editorial note
the cyclotron was in operation 1680 hours, or about 18 hours per day. Three days were lost due to failure of the refrigerator for the cold-trap above the diffusion pumps. Another day was lost because of inadequate oil levels in the diffusion pumps.
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 1
Editorial note, tabletop extrapolation: An upper anchor for what sustained cyclotron utilization can look like - useful against the NRL 60% figure only as a rough contrast, since the two reports account time differently (Harvard reports operating hours and lost days; NRL a full scheduled-time ledger). Note both of Harvard's losses were vacuum-auxiliary failures - cold-trap refrigeration and pump oil - not accelerator physics.
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Support equipment can dominate an outage: in the Harvard quarter, failure of the refrigerator serving the cold trap above the diffusion pumps cost three operating days.
Source quote & editorial note
Three days were lost due to failure of the refrigerator for the cold-trap above the diffusion pumps.
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 1
Editorial note, tabletop extrapolation: Chillers, trap refrigeration, and compressed-air auxiliaries deserve the same spares-and-monitoring attention as the pumps they serve - on any system whose operation actually depends on them: where a warm trap means contamination or lost vacuum margin, the machine is down as surely as if the pump died.
Cited in: The Vacuum Budget of a Cyclotron
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Diffusion-pump oil level is a checklist item, not a set-and-forget: a full day of an 18-hour/day operation was lost to nothing more exotic than low oil in the diffusion pumps.
Source quote & editorial note
Another day was lost because of inadequate oil levels in the diffusion pumps.
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 1
Editorial note, tabletop extrapolation: Diffusion-pump fluid level and condition belong on the maintenance checklist: check per the manufacturer's procedure at an interval set by operating history, plus after any abnormal heating, air inrush, or suspected loss - Harvard's lost day shows the failure mode is real and mundane. Some pumps need cooldown to check; plan for it.
Cited in: The Vacuum Budget of a Cyclotron
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The Harvard quarter's reported planned outage was a single ~1-week scheduled shutdown that installed the internal-beam pulsed-deflection apparatus.
Source quote & editorial note
A scheduled shutdown of about one week was required to install apparatus for pulsed deflection of the internal beam.
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 1
Editorial note, tabletop extrapolation: Conditional batching guidance, not a demonstrated result: when several tasks require opening the same vacuum boundary, combining them into one planned shutdown saves repeated venting, pump-down, leak-checking and conditioning cycles - the same pattern as NRL's engineering shutdown, at a smaller scale.
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Check Faraday-cup material systematics by swapping stopping materials without breaking vacuum: Harvard's cup accepted blocks of two different materials immediately in front of its 2-inch brass stopping plate (the normalization and thickness-scan procedure are the report's - re-read queued).
collected charge per unit beam vs stopping-material Z and thickness = secondary-emission/scatter-loss systematic of the cupSource quote & editorial note
blocks of either of two different materials could be placed (without disturbing the vacuum system) immediately in front of the 2-inch brass stopping plate
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 2
Editorial note, tabletop extrapolation: A cup's reading depends on its stopping surface through secondary emission and backscatter - a two-material comparison tests the SENSITIVITY to that choice, not the absolute error (both materials can be wrong the same way). For an absolute bound: verify full stopping, control geometry and contact, suppress electrons, and bring an independent current reference or a validated emission/backscatter calculation.
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Verify target areal-density uniformity before quantitative use: Harvard located the tail of the Bragg ionization curve at points across the target to map local density (the sensitivity, gradient figures and the pyrolytic-graphite decision are the report's account - re-read queued).
local areal density from range (Bragg-tail position) of a collimated beam through the target; sensitivity here 0.2%Source quote & editorial note
The density of various parts of the target was found ... by searching for the tail of the Bragg ionization curve.
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 4
Editorial note, tabletop extrapolation: A range-based (or transmission-based) density map of the actual target spot belongs in the error budget of a yield measurement WHEN the required precision or the material's provenance makes nonuniformity plausible - stock and process vary, so let the required precision decide whether to map, and state the stopping-power and composition assumptions the map rests on.
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Start every target heat-load estimate from the deposited beam power P = I x dE (current times energy lost in the target). Corwin's worked example: 100 nA losing 43 keV in a 380 ug/cm2 PbCl2 target gives P = 0.0043 W into a 1 mm x 3 mm (0.03 cm2) beam spot. For a target thick enough to stop the beam, dE is the full beam energy.
P[W] = I[A] x dE[eV] / z (z = charge state; z = 1 for protons). Corwin's example: 1e-7 A x 4.3e4 eV = 4.3e-3 W over A = 0.03 cm2Source quote & editorial note
In a typical charged particle experiment 100 na of beam loses 43 keV in a W = 380 ugm/cm2 PbCl2 salt target
Editorial note, tabletop extrapolation: A 1 uA, 170 keV proton beam fully stopped in an internal target deposits 0.17 W — forty times Corwin's example — into whatever spot the beam makes; the entire current limit of a thin uncooled target follows from this one number and the two removal channels (radiation, conduction) he works out next.
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Radiation limit (Corwin): a thin foil radiates from both faces, so shedding power P to surroundings at T0 follows P = e*sigma*2A*(T^4 - T0^4). For his 0.0043 W / 0.03 cm2 example, emissivity 1.0 needs about 106 C - and a realistic e = 0.1 needs about 330 C.
P = e*sigma*2A*(T^4 - T0^4), sigma = 5.67e-8 W/m2K4, factor 2A = both faces; e ~ 0.1 realistic for thin films, possibly lowerSource quote & editorial note
the target appears transparent and all of the radiating surface of a solid may not be present in a thin film.
Editorial note, tabletop extrapolation: Radiation is the only cooling channel a self-supporting foil in vacuum really has at the spot: solving Corwin's equation for a stopped 0.17 W beam on a 0.03 cm2 spot with e = 0.1 gives roughly 1200 C equilibrium - above most evaporated films' damage points and hot enough to anneal or evaporate many (boron itself melts higher, but its substrate and adhesion rarely survive) - which is why the spot is enlarged or the film backed (dg-1160).
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Conduction limit (Corwin): heat conducted radially from a beam spot of radius r_b to a frame at r_t obeys P = 2*pi*k*h*dT / (1/2 + ln(r_t/r_b)) - thickness h enters linearly. His example (h = 0.65 um, r_b = 0.1 cm, r_t = 0.64 cm, P = 0.0043 W): an insulator with k = 2 W/mK runs a ~1240 K rise - it fails - while a metal with k ~ 200 W/mK holds the quoted ~12 C rise.
P = 2*pi*k*h*dT * (1/2 + ln(r_t/r_b))^-1; k(salts) ~ 1-10 W/mC, k(metals) ~ 200 W/mCSource quote & editorial note
so a metal target could conduct the heat away with a 12 C rise in temperature.
Editorial note, tabletop extrapolation: The 100x conductivity gap between salts/insulating compounds and metals is the single biggest lever on target survival: a boron film on a thick copper or silver backing is conduction-cooled through the backing, while the same film self-supported is radiation-only (dg-1159). Thickness enters linearly, so doubling film thickness halves the rise at fixed power.
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Moving the target multiplies the survivable power: sweeping the beam spot around a circle enlarges both the radiating area and the conduction perimeter. Corwin's combined small-dT heat equation for a spot swept on a circle is P = [e*sigma*2*A_c*4*T0^3 + 2*pi*k*h/(1/4 + ln(r_t/r_c))]*dT; for his example (16 mm circumference, A_c = 48 mm2) the high-speed-rotation equilibrium RISE is dT = 65 C (the scan reads 'delta-T = 65 C') versus ~1000 C stationary, and conduction alone then holds 400 C - below his salt target's 501 C melting point.
P = [e*sigma*2*A_c*4*T0^3 + 2*pi*k*h/(1/4 + ln(r_t/r_c))]*dT (linearized, swept-circle geometry); Corwin example dT = 65 C moving vs ~973-1260 C stationarySource quote & editorial note
The equilibrium temperature of the beam spot circle for the high speed rotation limit is 65 C.
Editorial note, tabletop extrapolation: Rotation or beam wobbling is a heat-spreading method worth serious money on an internal target - Corwin built a three-target rotator to use it - but the gain factor is his geometry and material: rerun the equation with the actual tabletop spot, circle, thickness and emissivity, and remember a rotating mechanism in vacuum is real engineering (bearings, feedthrough, balance), not a trivial add-on.
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Check the transient, not just the equilibrium: beam suddenly applied to cold material heats it at dT/dt = P/(m*c) before radiation/conduction respond - 1300 C/sec for Corwin's 11 ug spot. At 1.9 turns/sec each part of the target sits in the beam only 29 ms and rises only 39 C per pass; the moving-target temperature is a sawtooth (65 to 105 C in his example). The spot's thermal recovery timescale is tau ~ r_b^2/alpha, alpha = k/(rho*c) (0.83 s in the example).
dT/dt = P/(m*c) initially; per-pass rise = (dT/dt) x dwell time; tau ~ r_b^2/(k/(rho*c)) - an order-of-magnitude diffusion timescale, coefficient geometry-dependentSource quote & editorial note
the temperature can rise only 39 C before that part of the target is out of the beam.
Editorial note, tabletop extrapolation: Sets the rotation-speed design check: compute the per-pass peak excursion (P/mc x dwell) against the allowable rise, and where the revisit period is not long compared with tau, run a periodic transient-heat calculation - the pulse train settles to a periodic steady state whose peak, not a simple ratchet criterion, is what must clear the material limit.
-
Thickness scaling of the two thermal limits (Corwin): thickening the target leaves the conduction limit unchanged in his per-thickness formulation while the radiation-limited temperature rises - more power deposited on the same radiating area; thin targets tend radiation-limited, thick ones conduction-limited, in his framework.
dE (hence P) grows with thickness; radiating area does not; conduction P grows with h in step with deposited powerSource quote & editorial note
With thicker targets the conduction limit will not change while the radiation limit will rise.
Editorial note, tabletop extrapolation: For a beam-stopping target the deposited power saturates at P = I*E/q, so further thickness adds no heat - then COMPARE the loss paths for the actual design instead of assuming conduction wins: a heat-sunk metal backing usually makes conduction dominant, but emissivity, temperature and interface resistance decide, so run both terms once.
-
Corwin's practical rotator: three targets on a fully adjustable, chamber-independent rotator turning 1.9 turns/sec through an O-ring shaft seal (a ferrofluidic feedthrough allows faster); reconciling Yntema's observations he notes carbon foil life improves both with motion AND with heating to ~400 C, foils thin above 450 C and thicken when cooler, and suspects damage is worst "when there is radiation from a single spot only".
Source quote & editorial note
The lifetime of carbon foils is enhanced both by motion and by heating to about 400 C. Also, carbon foils have been observed to get thinner above 450 C and thicker when cooler. ... These facts suggest that perhaps the foil is damaged when there is radiation from a single spot only. ... It is fully adjustable, holds three targets, is chamber independent, and takes up limited space. It turns the targets at 1.9 turns per sec which is adequate for most experiments; it could easily go faster by using a Ferrofluidic mechanical feedthrough instead of an O-ring feedthrough.
Editorial note, tabletop extrapolation: A rotating target holder is 1950s-shop technology (motor, gears, O-ring feedthrough at ~2 rev/s); the same shaft can carry several targets so a fresh one rotates into the beam without breaking vacuum.
-
Process-selection ladder (Adair & Kobisk, ORNL): rolling is by far the most material-conserving route to thin metal foils - the quoted superlative; the paper's Table 1 assigns per-element routes (its boron row: evaporation, 20-250 ug/cm2 self-supporting or 10-1000 on a metal backing) and its text records the low material efficiency of evaporation (exact figures: scan re-read queued).
Table 1 legend: a = evaporation, b = rolling, c = electrolytic, d = casting or pressing; backing 1 = self-supporting, 2 = metal backing, 3 = thin carbonSource quote & editorial note
Rolling is by far the most conservative process with regard to material loss in preparing thin targets.
Editorial note, tabletop extrapolation: The boron row of Table 1 is the direct answer for a B target: evaporation is the only listed route — 20-250 ug/cm2 self-supporting, 10-1000 ug/cm2 on a metal backing (boron is too brittle to roll). For thin-film evaporation recipes themselves cross-cite ORNL-3021; this table tells you which recipe book to open.
-
Roll metals inside a stainless-steel sandwich (Adair & Kobisk): consolidate the reduced metal into a bead, flatten in a hydraulic press, then roll between stainless sheets — the sandwich keeps the foil from adhering to the mill rolls and permits much thinner foils than bare rolling. Rolled foils are typically 1 x 1 inch.
Source quote & editorial note
the metal is placed in a stainless steel sandwich for rolling which prevents the material from adhering to the rolls of the mill and enables a much thinner foil to be prepared. ... Rolled foils are usually 1 x 1 in.
Editorial note, tabletop extrapolation: A jeweler's rolling mill plus shim-stock sandwich makes durable self-supporting metal targets (typically 1 x 1 in per the source) - the natural route to robust backing foils. Whether a rolled foil can serve as a beam STOP depends on the projectile's range: check stopping areal density against the actual beam energy first; the source's thickness tables cover what each metal reached, so cite the row, not a blanket range.
-
Evaporate expensive material from tubular crucibles (carbon, Mo, W, Ta) chosen for chemical compatibility with the evaporant, and expect only ~1% collection efficiency in ordinary geometry (Adair & Kobisk); electron-bombardment guns or RF heating serve the refractory and reactive cases, and vacuum reduction-distillation converts oxides directly to metal films.
Source quote & editorial note
evaporation efficiencies of only 1% are obtained.
Editorial note, tabletop extrapolation: Budget isotope/material mass from the geometry: the ~1% collection efficiency is the source apparatus's ordinary-geometry result, and the right transfer is to estimate your own geometric collection fraction (solid angle of substrate at the source), then verify with a witness coupon or charge/substrate mass accounting; crucible-evaporant chemistry (carbide formation, alloying) is chosen per material, not per convenience.
-
Characterize targets by areal density, not linear thickness: microscopic voids and mixed crystal phases make a linear measurement converted through bulk density grossly erroneous, while weighing is directly proportional to the number of nuclei when stoichiometry, purity and area are known (Adair & Kobisk).
atoms/cm2 = W[ug/cm2] * 1e-6 * N_A / M[g/mol] (elemental; apply the stoichiometric fraction for compounds); linear h = W/rho only as an estimateSource quote & editorial note
Linear measurements can lead to grossly erroneous values of atom content by virtue of included microscopic voids or a mixture of various crystal phases.
Editorial note, tabletop extrapolation: Yield calculations need atoms/cm2, which weighing gives directly given composition; a micrometer or interference measurement of an evaporated film does not - use thickness methods only when the film's density and composition are independently established.
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Weighing discipline (Adair & Kobisk): the NBS sequence-weighing scheme - sample and standard weights of similar mass weighed in a set order - cancels balance zero-point drift; an interlab check on 200+ boron and lithium crystals of 50-300 ug agreed better than +/-1% in almost every case.
NBS sequence weighing (Pontius, NBS TN 228 / Monograph 103); drift cancels, balance sensitivity extracted from the sequenceSource quote & editorial note
In almost every case the agreement was better than +-1%.
Editorial note, tabletop extrapolation: A used microgram-precision balance plus the free NBS protocol is a strong target-mass QA capability - budgeted honestly: 1 ug of combined uncertainty is already 2% of a 50-ug sample, and a deposited mass obtained by difference doubles the exposure, so write the mass-dependent uncertainty budget (readability, repeatability, calibration, buoyancy, static) before promising sub-percent numbers at the light end. The protocol removes drift; it cannot remove the balance's floor.
-
Quartz crystal monitors are in-situ process gauges; the ultimate measurement remains direct mass determination of the target after removal from the vacuum system (the calibration practices, cooling threshold and rotating-wheel extension are the proceedings' supporting material - scan re-read queued).
Source quote & editorial note
the ultimate measurement remains the direct mass determination of the target after it has been removed from the vacuum system.
Editorial note, tabletop extrapolation: Treat the QCM reading as rate-and-range control during deposition and take the certified number from pre/post weighing with the deposited area defined - a QCM calibrated in a stable thermal environment can be good, but radiant load from the source shifts its frequency exactly when the reading matters most, so the removal-and-weigh check is the arbiter.
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Measure self-supporting film thickness by charged-particle energy loss (Adair & Kobisk): collimated alphas through the foil, spectrum shift on a calibrated MCA; for small losses W ~ dE/S(E), and for thicker films integrate - W = INT dE/S_m(E) from E_out to E_in - since stopping power changes as the alpha slows. The era's stopping data carried ~+/-10% accuracy, which bounded their absolute results.
thin limit: W = dE/S(E); general: W = INT_{E_out}^{E_in} dE/S_m(E); alpha sources cover ug/cm2 to mg/cm2, fission fragments resolve ultrathin foils, beta transmission covers thick stockSource quote & editorial note
most of these data have an accuracy of ~ +-10%.
Editorial note, tabletop extrapolation: The one thickness method that needs no balance and works on a mounted film - with a surface-barrier detector and MCA. Quote absolute thickness no tighter than CURRENT stopping tables allow at the actual energies, combine straggling/calibration/fit uncertainties, and remember the alpha source is a regulated sealed source, not generic bench stock.
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Quick semi-quantitative gauges (Adair & Kobisk): a calibrated light densitometer reads carbon foil areal density at low thickness but the method stops being useful above about 40-45 ug/cm2 for carbon; low-geometry counting of radioactive deposits is the proceedings' companion assay method (its accuracy and geometry figures - scan re-read queued).
Source quote & editorial note
light intensity change is not a very useful technique for carbon films of thickness greater than 40 or 45 ug/cm2.
Editorial note, tabletop extrapolation: A photodiode and lamp sort carbon stripper/backing foils into thickness bins as an incoming-inspection tool - calibrated against weighed foils and RE-checked periodically, since optical response drifts with lamp, alignment and film morphology; expect it to saturate out near the source's 40-45 ug/cm2 carbon ceiling.
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Map uniformity, not just mean thickness (Adair & Kobisk): scan the foil with a collimated alpha beam position by position and draw a thickness topograph; for 0.5-500 mg/cm2 targets beta particles serve the same purpose (their Fig. 19 profiles a rolled 58Ni foil with a 204Tl source), and radioactive deposits are scanned with a small aperture and a silicon detector.
Source quote & editorial note
The uniformity of thin foils can be determined by scanning the foil with a collimated beam of alpha particles. ... For targets having a thickness in the range of .5 to 500 mg/cm2, beta particles can be used to determine the target thickness profile ... Figure 19 illustrates a target thickness profile obtained by scanning a 58Ni rolled foil with beta-particles from a 204Tl source. ... For radioactive sources the surface of the sources can be scanned using a small collimating aperture and a silicon solid state detector
Editorial note, tabletop extrapolation: The same alpha energy-loss rig with an XY-translated collimator becomes a uniformity mapper. What it maps is AREAL DENSITY variation - a single-point thickness number hides the wedge or large-scale nonuniformity; fine crystallite structure below the aperture scale needs a straggling measurement instead (dg-1190).
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Know what is in the target, not just how much (Adair & Kobisk): IRML characterized completed targets by elemental, spark-source and isotopic mass-spectrographic analysis — impurity species and concentration matter as much as thickness because contaminant reactions masquerade as signal.
Source quote & editorial note
it is equally important to know what species are present and in what concentration.
Editorial note, tabletop extrapolation: For a reaction-yield target the practical home-lab measures are material pedigree (certified purity), clean processing, and a background run on a process-matched blank backing - which catches backing and process backgrounds but NOT impurities arriving with the active deposit, so where composition is critical they reduce risk rather than replace assay. Check, for the actual projectile and energy, which contaminant reactions and scattering peaks could land in your signal region - carbon and oxygen are the usual suspects but not automatic offenders.
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Sputter from rolled isotopic foils when film properties matter (Adair & Kobisk): IRML adapted a commercial sputtering system to accept small rolled isotope foils as sputter sources - a very reproducible process - trading deposition speed for material economy (the electrode dimensions are the proceedings' detail - scan re-read queued).
Source quote & editorial note
this method has proved to be a very reproducible process.
Editorial note, tabletop extrapolation: Shrinking the source electrode to match the available material is the transferable move for scarce isotopes; how far down the stock can go depends on cathode geometry, erosion track, clamping and utilization - establish the minimum for the actual gun by test rather than assuming milligram-scale grace.
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Thompson's laboratory technique: an aluminum foil held at -300 V above an open 228Th bottle collects recoil-ionized 220Rn, which decays to 212Pb (10.6 h half-life), giving alphas at 8786, 6090 and 6050 keV - a fresh, essentially massless recoil-implanted source after ~10 h activation, useful for ~24 h.
228Th -> 224Ra -> 220Rn(+) collected at -300 V -> 212Pb (T1/2 = 10.64 h) -> alphas 8786 / 6090 / 6050 keVSource quote & editorial note
A large portion of the 220Rn gas is created as positive ions which are attracted by the -300 volt collecting potential
Editorial note, tabletop extrapolation: The physics is elegant - the 2.7 MeV spread between the 212Pb lines self-calibrates a spectrometer with no external standard - and the procedure is not an amateur recipe: an open 228Th container means thoron gas, plated-out daughters and removable contamination, and possessing 228Th in usable quantity is licensed activity in most jurisdictions (/legal/). For the program's spectrometer calibration the appropriate form of this idea is a commercial sealed or electroplated check source.
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Calibrate with two peaks and measure only shifts (Thompson): spread the 6050 and 8786 keV lines across the analyzer with a biased amplifier, compute keV/channel from their separation - the energy-scale SLOPE is all the calibration needed, since only shifts are of interest and the absolute intercept drops out - then read target thickness from the channel shift of each peak. His rig held vacuum below 1e-4 torr because the detector bias can strike a glow discharge at higher pressure and damage the detector.
Ec = (8786-6050)/(B-A) keV/ch; dE = (A-A')*Ec; thick targets by piecewise sum T = (dE/N) * sum 1/S(E-(i-1)dE/N)Source quote & editorial note
This is all the calibration which is necessary since now only energy shifts are of interest. ... the vacuum must be maintained at a pressure of less than 10-4 torr to avoid a glow discharge caused by the detector bias voltage. Such a discharge can damage the detector.
Editorial note, tabletop extrapolation: The whole rig is a surface-barrier detector, preamp, biased amp and a stable, linear MCA - Thompson wrote it up precisely so small labs could build it. Estimate fractional channel positions from adjacent-channel counts (peaks are Gaussian) and state the resulting channel uncertainty; whole-channel reading of a small shift is coarse. The pressure threshold for bias-induced glow depends on voltage and geometry - treat 1e-4 torr as his operating requirement and verify your own.
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Free diagnostics of the alpha-loss method (Thompson): peak broadening beyond the no-target width can flag nonuniformity once straggling and instrumental width are accounted for, and small UNSHIFTED satellite peaks flag pinholes - unattenuated paths through the film; the quantitative limits (minimum-thickness formula, upper range, Bragg additivity for compounds) are the paper's framework (scan re-read queued for the formulas).
Tmin = 1.22*(30 + A) ug/cm2 (10%, half-channel, 512 ch); S_compound = (1/M) * sum Ni*Ai*Si (Bragg additivity)Source quote & editorial note
They show up as small unshifted peaks in the energy spectrum.
Editorial note, tabletop extrapolation: One spectrum yields thickness plus uniformity and open-area evidence - run it on every target before installation. The unshifted peak measures unattenuated FRACTION, not a hole count; converting to open area needs the beam profile. Re-measuring after beam exposure quantifies damage - after the radiation survey and handling review that any post-irradiation work gets.
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Seeding rescued difficult condensers in the MicroMatter practice: zinc and cadmium - poor stickers on bare amorphous substrates - condensed uniformly and with very high sticking coefficients onto seeded surfaces (the seed materials, dose and dual-boat procedure are the paper's recipe - re-read queued).
seed layer ~1 ug/cm2 Be or Bi; dual boats so seed and evaporant deposit in one pump-downSource quote & editorial note
Zinc and cadmium condensed uniformly and with very high sticking coefficients.
Editorial note, tabletop extrapolation: When a film refuses to stick or beads up, a nanometer-scale nucleation layer of a compatible metal is the trial to run - material-specific, verified on a witness slide; note the crystal-structure story is looser than the folklore (Bi and Sb are rhombohedral, not hcp like Zn/Cd/Mg/Be), so pick seed candidates from the literature for the actual evaporant rather than from a structure-matching slogan.
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Reduce oxides in the evaporation boat with graphite (Heagney & Heagney): mix the oxide with spectroscopic-grade graphite, press to a pellet, and heat - the pressure gauge gives an indication of the rate of reduction as gas evolves (the material list, times and pressure ceiling are the paper's details - scan re-read queued).
carbothermal reduction, material-specific chemistry: products may be CO, CO2 or carbides depending on oxide and temperature - balance the actual reaction before relying on itSource quote & editorial note
the pressure gauge gives an indication of the rate of reduction
Editorial note, tabletop extrapolation: Lets a target come straight from a stable oxide powder with no separate metallurgy step. The total-pressure gauge is a qualitative process indicator only - it cannot identify the gas or prove completion; use temperature measurement, and an RGA or a validated endpoint where gas identity matters.
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Soften the roughing sequence where fragile foils live: in ANL's new commercial evaporator, an abruptly opened roughing valve went POOMPF and blew every thin carbon substrate off its frame (the calcium-reduction chemistry and short-throw boat geometry are the paper's separate content - re-read queued).
CaCO3 + heat -> CaO + CO2; 2CaO + Zr -> ZrO2 + 2Ca; closed Ta boat, 3 cm throwSource quote & editorial note
the valve opened with a POOMPF and all the carbon substrates disappeared.
Editorial note, tabletop extrapolation: Every pump-down and vent of a chamber holding fragile foils needs a throttled soft-start path - the foils die from the pressure transient and gas-flow forces, not the vacuum. Short-throw closed-boat geometry remains the milligram-economy move, with collection efficiency verified for the actual source and collimator rather than assumed pure 1/d^2.
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Sputter-yield scale (Scaife, Hanley & Purser): at focused-ion-beam energies, yields between 2 and 10 atoms per argon ion are typical - and unlike evaporation rates, yields rarely spread between materials by more than about an order of magnitude (the detailed energy-curve shape and Kr/Xe multipliers are the paper's account - scan re-read queued).
yield max ~25 keV (conductors) / 50-60 keV (dielectrics); 2-10 atoms per 20-keV Ar+; Kr ~2x, Xe ~3x the Ar yield on conductorsSource quote & editorial note
At focused ion beam energies, sputter yields between 2 and 10 atoms per argon ion are typical.
Editorial note, tabletop extrapolation: A keV-range ion gun is a plausible deposition tool - sized honestly: take measured or calculated yield curves for the actual ion-target pair, energy and angle, then work out rate from beam current and collection geometry, plus thermal load and neutralization. Gas choice (Ar vs Kr/Xe) is a rate-vs-cost trade to quantify per material, not a fixed multiplier.
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Sputtering decouples deposition from vapor pressure (Scaife et al., after Wehner): at 2000 C the evaporation rates of aluminum and tungsten differ by nine orders of magnitude, their sputter yields by only a factor of two - so refractory metals deposit at workable rates without crucible contact.
Source quote & editorial note
the evaporation rates for these two metals differ by nine orders of magnitude, whereas their sputter yields differ by only a factor of two.
Editorial note, tabletop extrapolation: When the material is refractory (B, C, W, Ta) or reacts with every crucible, sputtering is the escape hatch - with its own books to balance: preferential sputtering can shift alloy/compound stoichiometry, and the holder, backing, implanted gas and redeposition are all contamination paths (a graphite holder adds carbon, which is not always harmless). Shield the holder from the beam and verify composition transfer for mixtures.
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Energetic arrival is why sputtered films CAN be strong (Scaife et al.): sputtered atoms arrive at ~10 eV versus ~0.1 eV thermal, and the source reports self-supported films usually displaying the strength, toughness and ductility of the bulk parent - along with chemisorption-grade adherence and in-flight substrate cleaning in their process (which scrubbed off Teepol release layers; NaCl and BaCl survived).
sputtered-atom energy ~10 eV (maintained above ~1 keV bombarding energy) vs ~0.1 eV thermal depositionSource quote & editorial note
Self-supported films usually display the same strength, toughness, and ductility as their bulk parent material.
Editorial note, tabletop extrapolation: For a target that must survive beam, handling and mounting, sputter deposition is a strong candidate - verified, not assumed: arrival energy depends on gas pressure and geometry, and film stress, porosity and grain structure can depart far from bulk. Run adhesion and handling tests on the actual film/substrate pair, and pick the release agent for the process - salt layers where the energetic flux scrubs organics.
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Pressure sets what sputtered atoms arrive with (Scaife et al.): at 1e-3 torr the mean free path is about 1 cm, so glow-discharge-pressure transport suffers gas collisions; at 1e-6 torr the path is meters and atoms arrive with their emission energy and directionality intact.
mean free path ~1 cm at 1e-3 torr vs ~meters at 1e-6 torrSource quote & editorial note
At 1e-3 torr, the mean free path in the vacuum chamber is about 1 cm
Editorial note, tabletop extrapolation: For a small sputter rig the choice is real but not one-sided: a differentially pumped gun with a high-vacuum deposition region preserves arrival energy and directionality; glow-discharge and magnetron processes at millitorr nonetheless make dense, adherent films through substrate heating and plasma bombardment. Choose by what the film needs and measure adhesion, structure and gas incorporation on the result rather than assuming pressure decides quality.
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Working numbers for a focused-ion-beam sputter rig (Scaife et al.): a von Ardenne-type duoplasmatron with einzel lens delivering mA-class 20-25 keV Ar+, with a typical deposition rate of 20 ug/cm2/min of titanium at 2.5 cm; usable targets from ~10 mg of source material - NOTE an internal inconsistency: the paper's ~50 ug/s erosion figure would need ~50 atoms/ion at 2 mA, versus its own typical 2-10 (which gives 2-10 ug/s), and the 20 ug/cm2/min at 2.5 cm itself implies ~6.5 ug/s from a cosine lobe - scan re-read queued to resolve the units.
erosion = I*Y*M/(N_A*e); at 2 mA Ar+ with Y = 2-10: 2-10 ug/s of Ti - the printed 50 ug/s does not reconcile (dg-501 pattern); deposition falls ~1/d^2, lobe slightly narrower than cosineSource quote & editorial note
A typical deposition rate for substrates located 2.5 cm from the sputtering source is 20 ug/cm2/min. of titanium.
Editorial note, tabletop extrapolation: Calibration point for sizing a home sputter-deposition scheme - mA and tens of keV is small-accelerator source technology, not exotic hardware. Time a boron run from a boron yield (measured or from tables) and the actual collection geometry, not from the titanium calibration.
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Contact evaporation for maximum recovery (Reynolds & Morgan): the substrate sits directly on a resistance-heated tantalum tube source with stacked tantalum mesh discs inside as a multi-point source - achieving at least 90% material recovery with ~10% uniformity over the cm2-scale area, on 200-ug-class isotope charges; heat gently (~450 C) and cool slowly so the glass slide does not crack.
tantalum tube + 50-mesh Ta discs as diffuser; recovery >= 90%, uniformity ~10% / cm2Source quote & editorial note
a uniformity of 10% over an area of cm2 with a recovery of at least 90% of the material.
Editorial note, tabletop extrapolation: The zero-throw geometry is the method of interest when the feedstock (separated isotope, exotic compound) costs more than one-at-a-time labor - its recovery advantage over open evaporation is large, and exact areal densities follow from the actual charge, recovery and area (at 90% recovery, 200 ug over 1 cm2 is 180 ug/cm2 - quote the arithmetic, not a nominal).
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Store reactive targets under inert gas through shipment (Bonetti et al.): their lithium, calcium and rare-earth targets ship in containers filled with desiccated argon; the group's process comparison found electrodeposits nonuniform where electrosprayed layers held tighter tolerances (figures report-attributed - scan re-read queued).
Source quote & editorial note
The targets are sent to the users in containers filled also with dessicated argon.
Editorial note, tabletop extrapolation: An argon-purged jar or backfilled desiccator is cheap protection for oxidizable targets - how LONG it protects depends on seal integrity and gas purity, so spot-check a witness piece rather than assuming months. And map any electroplated deposit before trusting its uniformity: the process's signature is variability, even if a universal factor-of-two default overstates it.
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Vacuum storage beats atmosphere for degradable targets: ANL's storage-and-transfer system (Worthington, Jedlowski & Thomas) kept hygroscopic and rapidly oxidizing targets under vacuum from evaporator to beamline via valved transfer hardware (the wheel capacity, pressures, baffle temperature and interlock details are the paper's - scan re-read queued).
storage < 5e-7 torr; interlock volume < 0.05 torr before valve openingSource quote & editorial note
Some targets may be hydroscopic, while others may oxidize rapidly.
Editorial note, tabletop extrapolation: The load-lock principle scales down to one target: a valved transfer pot REDUCES atmospheric exposure for Li, Ca or boride targets - how much depends on its achievable pressure, residual water and oxygen, pump backstreaming and valve sequencing, so qualify the pot against a sacrificial target before trusting it with the real one.
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The parting agent, not the evaporation, can set target nonuniformity (Abele et al.): Braski's electron microscopy gave parting-agent crystallite sizes of 100-2000 A and surface roughness 50-1000 A - the same order as a 10 ug/cm2 carbon or 100 ug/cm2 gold film (~500 A) - so 'however uniform an evaporation may be, the parting agent produces an inhomogeneous target', and the source states these nonuniformities are NOT detectable by the standard thickness-profile method.
crystallite size 100-2000 A ~ film thickness; effective-thickness spread grows with 1/cos(tilt) plus crystallite-plane geometrySource quote & editorial note
His analysis gave average crystallite sizes between 100 A and 2000 A and average surface roughnesses from 50 A to 1000 A depending on various parameters as parting agent material, temperature of the substrate, rate of evaporation, thickness of the parting agent. Recalling that carbon foils of 10 ug/cm2 or gold foils of 100 ug/cm2 have a thickness of nearly 500 A, one notices that the size of such a crystallite structure and the target thickness are of the same order of magnitude. This means that, however uniform an evaporation may be, the parting agent produces an inhomogeneous target. These nonuniformities are not detectable in a measurement of the target thickness profile with the standard method
Editorial note, tabletop extrapolation: If a target will sit tilted to the beam or feed a spectrometer, the release-agent choice is a resolution decision, not a convenience. Energy-straggling width is the sensitive test the source used; microscopy or profilometry can also reveal the structure - what cannot see it is a mean-thickness scan at aperture scale.
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Choose low-crystallite organic parting agents for resolution work (Abele et al.): among the tested release agents, Teepol - and nearly, alanine - kept measured straggling near the ideal-target prediction at high tilt, while NaCl and betaine replicas broadened it severely; the source's QA method: pass monoenergetic alphas through the finished target and compare the straggling width to the Vavilov prediction, checking target resolution without expensive beam time.
fit the measured spectrum as the convolution of the Vavilov distribution, the detector/source response, and a thickness distribution; quadrature FWHM subtraction only after validating that a Gaussian approximation holds for the actual caseSource quote & editorial note
all targets should be produced with the use of Teepol as parting agent, or ... an organic parting agent with very little crystallite structure
Editorial note, tabletop extrapolation: Detergent-film release over salt release wherever the condensing metal tolerates it; and the alpha-straggling comparison is a bench-top RESOLUTION metric using the thickness-measurement rig - one axis of target quality, with adhesion, pinholes, large-scale uniformity and durability still needing their own checks.
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Proton targetry is forgiving - 'with a proton beam, targetry is just no problem' (Erskine, ANL): even a leftover gold target gave 5.1 keV FWHM at 16 MeV, because energy loss scales as projectile charge squared at equal velocity, so proton losses are the floor of the scaling.
dE ~ thickness x (M/E)^0.6 x Z_proj^2; straggling ~ Z_proj x sqrt(thickness x Z/A); carbon ~2.5x the energy loss of gold per ug/cm2Source quote & editorial note
With a proton beam, targetry is just no problem. One can obtain very nice high-resolution results.
Editorial note, tabletop extrapolation: Direct license for a proton machine: target thickness and uniformity tolerances that dominate heavy-ion work are second-order for protons, so a thick-ish imperfect boron layer costs beam-energy definition, not feasibility. When tempted by heavier beams, budget with the Z^2-at-equal-velocity scaling and check real stopping tables (SRIM/NIST-class) at low energy, where effective-charge effects bend the simple law.
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Backings are not free (Erskine): a carbon substrate produces a lot of difficulty because of contaminant reactions from the carbon; reaction-site path-length compensation by tilting works only if the target is flat - bowing, wedge or roughness defeats it (his stopping-power comparison and 48Ca history are the talk's specifics - scan re-read queued).
Source quote & editorial note
using a carbon substrate produces a lot of difficulty because of the contaminant reactions observed from carbon
Editorial note, tabletop extrapolation: For reaction-yield measurements, run the blank-backing background and prefer a backing whose own beam reactions are energetically closed or distinguishable at YOUR energy; compare backing stopping powers with current tables at the actual projectile and energy rather than a remembered ratio. Flatness of the mounted foil matters as much as its thickness distribution.
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Foil lifetime normalized by beam current DENSITY (Yntema): his analysis assumes lifetime inversely proportional to the particle density on the target, plots carbon-stripper lifetimes as particle-uA-min per mm2 of actual beam spot against ion velocity, and finds stationary unheated foils falling on a straight line in those variables; minimum practical stripper ~3 ug/cm2.
lifetime metric = particle uA min / mm2 (beam-spot area); velocity variable MeV/ASource quote & editorial note
we have assumed that the foil lifetime is inversely proportional to the particle density incident on the target.
Editorial note, tabletop extrapolation: Under that model, halving the spot diameter quarters foil life at fixed current - so measure the actual beam-spot size before predicting from literature data, and carry the companion variables when comparing (species and velocity, foil temperature and fabrication, motion/duty cycle for oscillated targets, vacuum contamination). The scaling is Yntema's stated assumption validated on his data, not a universal damage law.
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Heat carbon foils DURING bombardment (Yntema): in his Ni-beam experiment, radiatively holding the foil near 500 C extended observed lifetime about 40x, slow motion multiplied it further, and pre-annealing at 1000 C before use gave no benefit - the heat must be present while the damage is being done. Foils also thicken under beam from hydrocarbon cracking; clean vacuum and motion moderate it.
~500 C in-beam -> ~40x life; + slow motion (6x area) -> >200x; pre-annealing at 1000 C -> no effectSource quote & editorial note
The increase in observed lifetime was about a factor of 40.
Editorial note, tabletop extrapolation: Concurrent annealing is the transferable idea: a small radiant heater on a carbon stripper/target holder is a cheap experiment with a large historical payoff - run it as an experiment, monitoring actual foil temperature, outgassing and vacuum cleanliness, rather than booking the 40x (which belongs to the cited foil, beam and conditions). Keep hydrocarbons out of the vacuum or the beam writes a thickening carbon spot on every foil.
-
Electrostatics can kill a foil instantly (Yntema): a charged insulator near the foil can blow it off the frame almost instantaneously (the edge-current mechanism and the Au-helps/Al-hurts coating results are companion claims from the same discussion - scan re-read queued).
Source quote & editorial note
the foil can be blown off the frame almost instantaneously.
Editorial note, tabletop extrapolation: Ground the target frame conductively, keep chargeable insulators (windows, PTFE hardware) away from foil positions, and make the foil-to-frame electrical contact generous - cheap precautions against a documented instant-loss mode, whatever fraction of failures the mounting ultimately accounts for.
-
Defocus whenever possible - the source's own moral (Berry): sweeping the beam at 1 kHz in x and y over an aperture-defined area cut thin-carbon-foil breakage several-fold by evening the current density; a defining pre-aperture keeps beam off the foil holder, and a multi-foil carousel makes replacement cheaper than heroics.
1 kHz x-y electrostatic raster over 25 mm2 -> breakage / 5-10; life ~ proportional to uniformly-illuminated areaSource quote & editorial note
Defocus whenever possible is the moral to this result.
Editorial note, tabletop extrapolation: An internal target wants the widest beam spot the measurement tolerates, an aperture that shadows the frame, and a multi-position holder. Rastering and mechanical target motion are alternatives, not equivalents - rastering changes the optics and duty cycle while rotation moves material through a fixed beam - and each needs its own optical, aperture and HV check on a small machine before it is called easy.
-
Match the e-beam spot to the evaporant droplet (Maier-Komor): the most efficient energy transfer comes at beam diameter = droplet diameter - larger wastes power on the cooled crucible, smaller saturates in the dense vapor above the impact point; for their small charges, roughly half the beam power was lost to backscatter off the high-Z melt (Kanter/Sommerkamp Ta-sphere data: ~49% absorbed).
beam spot ~ droplet diameter; power absorption ~49% (Ta sphere); backscatter loss rises with Z and with incidence angleSource quote & editorial note
the most efficient energy transfer is achieved, when the electron beam and the molten droplet have the same diameter.
Editorial note, tabletop extrapolation: Small-charge e-gun work is a spot-placement problem, and the transferable warning is that rated gun power is not deposited melt power - the deficit depends on electron energy, Z, geometry and what the chamber recaptures, so estimate absorption for the actual configuration instead of applying the Ta-sphere 49% as a universal factor of two. Never size a gun from evaporation enthalpy alone.
-
Regulate the e-gun supply or re-aim at every power change (Maier-Komor): drooping supplies sag up to 25% at full load, and with magnetic deflection the spot radius follows sqrt(V), so the spot walks off the evaporant - the source's own example says nearly 7 mm for its gun. Find the true spot by melting a hole in a copper foil laid in the crucible, or by maximizing crystal-monitor rate versus deflection. Use water-cooled copper crucibles, cleaned of oxide, one per isotope.
r ~ sqrt(V): a 25% droop at r = 25 mm computes to 25*(1 - sqrt(0.75)) = 3.4 mm - the source's 'nearly 7 mm' implies a larger radius or bigger droop than the nominal example (dg-501 pattern; scan re-read queued for the gun geometry)Source quote & editorial note
the beam spot will shift nearly 7 mm when the power supply is fully loaded and the beam will no longer hit the evaporant.
Editorial note, tabletop extrapolation: Any home-built or surplus e-gun needs a stiff regulated HV supply before it needs more power; the copper-foil melt-hole trick is the free beam-alignment diagnostic.
-
Manage charge on insulating substrates during e-gun runs (Maier-Komor): the parting-agent-coated substrate is an insulator, so start at a very low evaporation rate so the growing layer can discharge - otherwise 'sparks will occur, destroying the parting film and the thin isotope layer by hairline cracks'; the wider charging discussion is the paper's (scan re-read queued).
Source quote & editorial note
sparks will occur, destroying the parting film and the thin isotope layer by hairline cracks.
Editorial note, tabletop extrapolation: Grounding topology inside the evaporator is part of the recipe - and the same charging physics will bite any deposition or beam system with floating fixtures near keV electrons: bond fixtures deliberately rather than assuming they find ground.
-
Budget substrate heating from condensation and source radiation (Maier-Komor): condensation releases ~6e5 J/g-atom for low-vapor-pressure metals - so heating rate = (mass flux)*(6e5/M) with the evaporant's molar mass M in the equation - and radiant load at equal vapor pressure follows source temperature (Mo radiates ~10x what Au does); the only ways out are cooling the substrate or periodically interrupting the evaporation.
q_dot = (g/cm2/s flux) * 6e5/M [J/g-atom / (g/mol)]; worked example: ~5e-8 g/cm2 s of Mo onto 50 ug/cm2 NaCl ~ 7 K/s adiabatic; contamination criterion = ratio of residual-gas impingement flux to deposition flux (NOT a source-pressure ceiling - slower evaporation at fixed background makes films dirtier)Source quote & editorial note
the only way to avoid destruction of the targets is to cool the substrate or to periodically interupt the evaporation process
Editorial note, tabletop extrapolation: Substrate meltdown during deposition is the same radiation/conduction bookkeeping as beam heating (Corwin, this volume) with condensation enthalpy as the source term; refractory evaporants punish the substrate through radiation long before the film is thick.
-
Sulphide (and volatile-compound) evaporation is a cleaning-and-preheat protocol, not just a boat temperature - Peck's protocol (Queen's): abrasive-clean the substrate (gently on gold - buried grit mimics a Si contaminant), water then ethanol rinse, pump while still alcohol-wet, chimney-topped boat, substrate pre-warm.
Source quote & editorial note
The cleaning process is of utmost importance and each of the following steps contributes significantly to good results.
Editorial note, tabletop extrapolation: Template for any compound that dissociates or splashes: pelletize the charge, chimney the boat, pre-warm the substrate with the source itself - and treat any color-temperature chart as a coarse process indicator only (color-to-temperature conversion is unreliable; a thermocouple wins when the number matters). Valve off the diffusion pump so compound vapor does not load the pump oil.
-
One documented beam-induced failure mode is mechanical (Ramsay): the beam spot thickens, the film tightens, radial stress lines develop, and the foil tears across the thickened spot - breaking, to the author's own surprise, at its thickest part.
Source quote & editorial note
It has always bothered me that a film should ever break at its thickest port [sic]; (Ramsay, "Alternatives to Thin Film Carbon Foils")
Editorial note, tabletop extrapolation: When a thin internal target or probe foil dies, read the wreckage before assigning the cause: the radial-crease/thickened-spot signature points to Ramsay's stress mechanism, while melting, sputtering, charging marks or a failed frame each tell a different story - the mechanisms coexist and beam conditions pick the winner.
-
Foil-lifetime levers that cost nothing: start with the beam spot as large as possible and focus down slowly, use the largest practical foil diameter, and heat the foil evenly to reduce the temperature gradient (uneven heating drives the stress).
lifetime rises with beam-spot area, foil diameter, and temperature uniformitySource quote & editorial note
start with as large a beam spot as possible and slowly focus it smaller ... Also the larger the diameter of the foil the greater the lifetime. The smaller the area of the beam spot the shorter the lifetime. Heating it evenly reduces the temperature gradient and probably makes the foil more elastic.
Editorial note, tabletop extrapolation: Directly usable at first target insertion — defocus onto a fresh foil, tighten the spot only as needed, and expect the smallest spot to have the shortest foil life.
-
A thin metal backing can rescue an otherwise doomed foil (Ramsay's trial): carbon films backed with a 10 ug/cm2 gold layer survived beam exposure that tore identical unbacked carbon at the beam spot - two of the backed targets did not break.
2 ug/cm2 C + 10 ug/cm2 Au backing survived; bare 2 ug/cm2 C toreSource quote & editorial note
two of the targets did not break (Ramsay, "Alternatives to Thin Film Carbon Foils")
Editorial note, tabletop extrapolation: When a self-supporting film keeps failing, an evaporated metal layer is a cheap experiment - with its costs computed first: at sub-MeV proton energies 10 ug/cm2 of gold contributes real energy loss and straggling (run the stopping numbers), ultrathin layers may not be continuous, and the backing adds its own reaction background. Try it; measure what it costs the experiment.
-
When forming a target compound by heating a deposit on a substrate, beware the high side: too high a temperature diffuses the reactant into the substrate - nitrogen into the tantalum, in the cited N-15 work - leaving a target with poorly defined thickness (the specific temperature window is the paper's recipe - re-read queued).
TiN nitriding window 750-800 C (optical pyrometer, uncorrected for emissivity)Source quote & editorial note
too high a temperature can cause nitrogen diffusion into the tantalum substrate resulting in a target with a poorly defined thickness (Stinson, "The Preparation of Nitrogen-15 Targets")
Editorial note, tabletop extrapolation: Any reacted-layer target (nitride, oxide, deuteride) on a metal backing needs its own temperature study - the failure modes differ by system (substrate diffusion here; desorption or decomposition for deuterides) - and a smeared depth profile shows up downstream as degraded resonance width or energy resolution, which is the cheap check that the window was respected.
-
Hydrogen tube-furnace reduction converts many common target oxides to metal with modest equipment, per the report's two-page per-element table (temperature, reductant, boat); the boat must be chemically compatible - the quote's trap: iron in a graphite boat forms carbide - and the report's apparatus dries and deoxygenates the H2 and guards the vent flame with an oil trap.
per-element reduction table (temp, reductant, boat) at PDF pp.102-103; Vycor tube to 1000 C, quartz to 1300 CSource quote & editorial note
Iron forms a carbide if a graphite boat is used (Heagney & Heagney, "Reduction Techniques for Isotopic Materials")
Editorial note, tabletop extrapolation: The route from purchased oxide powder to rollable or evaporable target metal - consult the per-element table before buying any element as oxide. A hot hydrogen furnace is its own hazard class: inert purge before and after H2, flow and flame management, and per-element vapor and hydride toxicity are prerequisites the table assumes rather than teaches; the report's apparatus description is the checklist seed, not the whole checklist.
-
Electrolytic reduction conserves scarce material: in the cited practice, usually better than 90% of the metal deposited on the cathode (the bath chemistry, current density and volumes are the paper's parameters - re-read queued).
Zn, Cd plating at 5-10 mA/cm2; bath volume 1-5 ml scaled to isotope quantitySource quote & editorial note
Usually better than 90% of the metal can be deposited on the cathode (Heagney & Heagney, "Reduction Techniques for Isotopic Materials")
Editorial note, tabletop extrapolation: For milligram-scale enriched material the deciding metric is END-TO-END recovery fraction, not speed - cathodic deposition is one term in it (dissolution, transfers and electrode handling take their shares), so weigh the whole chain for each candidate route rather than assuming electrolysis beats furnace reduction whenever plating works.
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For a beam-durable deuterium target, the cited group evaporated titanium in a low-pressure D2 atmosphere and abandoned deuterated polyethylene, which deteriorated rapidly under their bombardment; the occluded deuterium is assayed by nuclear scattering, not by weight (fabrication parameters report-attributed - scan re-read queued).
Ti evaporated in 5e-3 torr D2 over 2-3 h; ~2 ug/cm2 D occluded in 250-300 ug/cm2 TiSource quote & editorial note
Deuterated polyethylene could not be used because of its rapid deterioration under bombardment (Meens, "Deuterated Titanium Targets on Thin Backings")
Editorial note, tabletop extrapolation: The standard durable chemistry for d-beam or D(p,..) work - with durability measured, not assumed: TiDx targets still lose deuterium, blister and sputter as current density rises, so establish the lifetime at the actual beam parameters. CD2 remains usable where its measured lifetime covers the run - 'lowest current only' is a tendency from the cited experience, not a threshold.
-
When the target element is volatile or liquid, build it from a thermally stable compound: the cited sublimed HgS film tolerated ~20 particle-nA of their heavy-ion beam where the amalgam target allowed ~1 - and inhomogeneity showed immediately as a low-energy tail on the elastic peak.
max beam current ~20 pnA (HgS film) vs ~1 pnA (Bi-amalgam); HgS sublimed onto LN2-cooled Al/Ni/Cu/Bi backingsSource quote & editorial note
The maximum allowed beam current is about 20 particle nA for the HgS-ta[rget] and about 1 particle nA for the amalgam target (Friebel et al., "Preparation of Isotopically Enriched Mercury Targets")
Editorial note, tabletop extrapolation: The compound-beats-volatile-element lesson transfers; the factor of twenty does not - it belongs to that beam, spot, thickness and cooling. For a sub-MeV proton or deuteron machine, compute deposited power and target temperature for the candidate compound directly. The elastic-peak tail is a useful in-beam flag for target quality once detector response, straggling and backing effects are excluded.
-
Cool a fragile target in use by conduction through its edges: the cited mercury targets connected the target edge to a chilled copper block with silver paint (the block and target temperatures are the discussion's figures - re-read queued).
edge conduction via silver paint; block -80 C -> target ~-50 C (~30 K rise through the joint and film)Source quote & editorial note
They are cooled from the edges by connecting to a copper block with silver paint (Maier, discussion of "Preparation of Isotopically Enriched Mercury Targets")
Editorial note, tabletop extrapolation: The simplest conductive-cooling geometry for a target that cannot be water-backed - a cold finger to the frame plus a conductive-paint joint. What temperature the target actually runs at is beam power times the total thermal resistance: compute it or measure it in beam; the joint and film resistance can be anywhere from negligible to dominant, so no stock kelvin budget applies.
-
In reduction-distillation, pick a reductant of MODERATE oxygen affinity - by the oxide dissociation-pressure diagram - so reaction speed stays controllable by furnace temperature: tungsten powder reduces HgO smoothly (the paper's 500 C, ~10 min run), while thermodynamically stronger reductants (Zr, Th) run into explosion and scatter the charge.
choose reductant by oxide dissociation-pressure diagram; W + HgO controllable at 500 C, Zr/Th explosiveSource quote & editorial note
the reaction with mercury oxide runs into an explosion (Friebel et al., "Preparation of Isotopically Enriched Mercury Targets")
Editorial note, tabletop extrapolation: Strongest is not best in metallothermic reduction: a controllable reaction that completes in minutes beats a violent one that contaminates the product. Mercury adds its own layer - at these temperatures Hg is mobile, toxic vapor, so the paper's sealed-retort integrity, condensation path and exhaust handling are part of the method, and mercury work sits behind fume containment at any scale.
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Thick targets from powder, per the cited practice: press the powder between two polished stainless ferrotype plates at about three tons per square inch (the charge masses, disc size, binder wash and glove-box handling are the paper's procedure - re-read queued).
~3 ton/in2 between polished plates -> 100-150 mg/cm2 discs; 1 mg/ml polyethylene-xylene binder wash for fragile discsSource quote & editorial note
the powder was pressed between two stainless steel plates (Premier Brand Ferrotype) at about three tons per square inch (Minamisono & Ramsay, "Thick Targets for In-Beam Hyperfine Structure Study")
Editorial note, tabletop extrapolation: The no-evaporator route for activation and yield work: a hydraulic press and polished plates. Compute the areal density from measured mass over measured area (300-400 mg on a 2-cm disc runs ~95-127 mg/cm2), and verify 'beam-stopping' against range data for the actual ion and energy rather than by adjective.
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Split any conductive target-holder ring that sits in an RF field, as Ramsay's holder was split, so the ring cannot carry the circumferential induced eddy current.
Source quote & editorial note
The holder ring was split to prevent eddy currents in the ring from rf (Ramsay, discussion of "Thick Targets for In-Beam Hyperfine Structure Study")
Editorial note, tabletop extrapolation: An internal target probe near the dee gap lives inside the machine's own RF field; a closed metal frame is a shorted turn that heats and perturbs. One saw cut interrupts the loop PROVIDED nothing bridges it - target foil, conductive deposits, or mounting hardware across the gap re-close the turn, and a narrow gap still passes some capacitive current - so verify RF heating after assembly.
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Weighing degrades as a thickness gauge for very thin foils: adsorption/desorption alone contributed about 0.5 ug/cm2 of error in the cited frame-weighing arrangement - the paper's answer was optical transmittance with a reflectance correction (its equation, wavelength strategy and carbon range are the paper's method - re-read queued).
ln(I_T/I_0) = -mu*x + ln(1-R_R), R_R = 1-(1-R1)(1-R2); carbon usable ~5-150 ug/cm2 across 200-2500 nmSource quote & editorial note
if you weigh the frame without and with the foil, the error will be about 0.5 ug/cm2 because of adsorption and desorption effects (Maier-Komor, "A Rapid and Accurate Method for Measuring the Thickness of Extremely Thin Targets")
Editorial note, tabletop extrapolation: A bench spectrophotometer measures foil thickness in seconds without an accelerator - as a CALIBRATED method: attenuation and reflectance are material- and wavelength-specific, interference and pinholes bend the simple law, so calibrate against weighed thicker foils and state the neglected effects. Where you draw the too-thin-to-weigh line follows from the 0.5 ug/cm2 floor and YOUR allowed relative error - 10 ug/cm2 is that line for a 5% budget.
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Prevent stress failure of evaporated films by heating the substrate during deposition (Gursky): film tension falls with substrate temperature, crosses zero, and can go compressive - reported crossovers ~210 C for Ni, ~100 C for Cu, ~300 C for Fe under his conditions; the discussion's proven-temperature table (Cr 375-400, Co 300, Au 100, Pd 200, Pt 350-400, Ti 230-260) records what worked in that laboratory's process.
proven substrate temps (PDF p.205 table): Cr 375-400 C, Co 300, Cu 100, Au 100, Fe 325, Ni 250-300, Pd 200, Pt 350-400, Ti 230-260 C, each with parting agentSource quote & editorial note
the crossover point is about 210 C for nickel, 100 C for copper, and about 300 C for iron (Gursky, discussion "Prevention of Stress in Foils by Substrate Heating")
Editorial note, tabletop extrapolation: The missing variable when evaporated foils curl, buckle or shatter on float-off: set substrate temperature at deposition time, starting from the cited values and tuning for the actual system. Do not count on post-deposition annealing to rescue a stressed film - it can help in some film/substrate systems (recovery, creep) and not in others, so it is a fallback to test, never the plan. Complements the ORNL-3021 evaporation recipes.
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A small bench-type hand-cranked rolling mill rolls many useful foils down to the 1-5 mg/cm2 region; and when a small isotope quantity rolls non-uniform (thick center, thin edges, from too few passes), the source's alternative is pressing it between two highly polished cobalt-tungsten-carbide flats from a machine shop.
bench mill -> 1-5 mg/cm2; Mo from powder 25-30 mg/cm2 or <1 mg/cm2 from e-gun-melted ball; Cd 5-6 mg/cm2 between 20-25 mil mylar; Ca 700 ug/cm2 in argon glove boxSource quote & editorial note
One can roll many useful foils down to the 1 to 5 mg/cm2 region with a small bench-type manually operated mill ... Uniformity may be poor in rolling a small quantity of a separated isotope with few passes - the target is thick in the center, thinner at the edges. Instead of rolling, the material can be pressed between two highly polished flats of cobalt tungsten carbide from a machine shop.
Editorial note, tabletop extrapolation: A jeweler's mill covers most of the mg/cm2-class targets a small machine needs - whether 1-5 mg/cm2 is 'thick' for your purpose is a stopping-range calculation for the actual particle and energy, not a label; the carbide-flat press is the documented fallback when rolling wastes scarce material on edge taper.
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Pack-rolling craft: 3-5 mil polished tungsten sheet makes a hard reusable pack (but not for the very thinnest foils); spring-steel sheet works alongside stainless; and when a soft metal (Pd) welds itself to the pack below ~500 ug/cm2, make three to five passes at the SAME mill setting before reducing further.
W sheet 0.003-0.005 in packs; Pd anti-weld = 3-5 passes per setting; U limit ~1 mg/cm2 with electropolish (H2SO4) between rolling stages, minimal heatSource quote & editorial note
In addition to stainless steel, spring steel sheet has been found useful for pack rolling. Tungsten sheet, 0.003 to 0.005 in., is good for pack rolling, is very hard with a good polish, and can be used many times. Tungsten is not suitable for rolling very thin targets because of its crystal structure. Palladium: A problem is welding of palladium to the pack when trying for less than 500 ug/cm2. This can be avoided by making three to five passes at the same setting before going thinner. Uranium: 1 mg/cm2 is about the limit. Since oxidation of U limits its rollability, it is useful to roll, electropolish (sulfuric acid removes oxide), roll again, (or roll in Ar). Be careful not to generate too much heat in rolling.
Editorial note, tabletop extrapolation: The same-setting-passes trick (plausibly work-hardening the surface before the next bite - our hypothesis, not the source's) and the electropolish-between-stages cycle for oxidizing metals are the two non-obvious moves in amateur pack rolling.
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Heating and moving a stripper foil multiplied its life in the cited experiment (carbon foils under intense 3-MeV Kr+): holding foil and frame at 450+-150 C gave about 4x lifetime, orbiting the foil ~3x, both together ~6x - and the failure signature changed, cold foils breaking suddenly while heated ones tore gradually from an edge.
x4 (heat 450+-150 C), x3 (orbit 1 rpm), x6 (both); baseline reduced lifetime 0.4-0.5 min for 3-MeV Kr+ at 0.125-0.2 p-uA/mm2 (Table I, PDF p.29)Source quote & editorial note
Heating the carbon foil and graphite support frame to an ambient temperature of 450 +-150 C increased its lifetime by about a factor of 4 (Thomas, DenHartog, Bicek & Yntema, "Lifetimes of Carbon Stripping Foils")
Editorial note, tabletop extrapolation: A heater ring or slow rotation stage on a foil holder is a cheap candidate life-extender - for carbon under heavy beams it has a strong record; for other target materials, adhesives and beams, heating can as easily hurt (oxidation, adhesive failure, evaporation), so test it with heat-load and vacuum checks rather than booking a multiplier. The gradual-tear behavior of heated carbon is a bonus where it holds: warning instead of sudden loss.
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Beam duty-cycling extends foil life only if the off-periods are long enough: equal on/off periods of 60 s produced encouraging results while 6-s periods showed very little improvement - the source's reading being that longer cycles may afford the foil a relaxation time, which may also contribute to the gains from moving foils.
60 s on/off helped, 6 s did not (3-MeV Kr+ on ug/cm2-class carbon stripping foils; the previously printed 5 mg/cm2 was a unit slip - the paper's foils run 5-120 ug/cm2)Source quote & editorial note
Periods of sixty seconds have produced encouraging results while six second periods showed very little improvement in foil lifetimes. The longer cycling times may afford the foil a relaxation time. This relaxation time may also be a contributing factor in the increased lifetimes for foils which are moved.
Editorial note, tabletop extrapolation: Relevant to any interlock or chopping scheme meant to spare a target: two time points bracket, but do not measure, the relaxation constant - if chopping is the plan, scan the off-time on the actual foil rather than assuming tens of seconds is the magic number.
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In Kellner and Maier-Komor's heavy-ion tests, rolled target foils withstood the beam longer than evaporated targets, which they attribute qualitatively to the rolled foils' crystalline structure. [Corrected 2026-08-23: an earlier version over-explained the mechanism (phonon reordering, Frenkel defects, a 'Wigner energy' of 10-40 eV - that figure is a displacement threshold energy, and Wigner energy means something else) and concluded durability is set by crystalline order rather than thickness. The source supports the qualitative observation only.]
Source quote & editorial note
Rolled target foils withstand due to their crystalline structure longer a heavy ion beam than evaporated targets (Kellner & Maier-Komor, "Rolling Thin Uranium Foils and Other Exotic Isotopic Metals")
Editorial note, tabletop extrapolation: Where a target must survive sustained current, prefer rolled, electrodeposited or annealed material over as-evaporated film where practical - but crystalline order is one factor among several. Target survival is set by beam power density, stopping range against thickness, backing and adhesion, thermal conductivity and cooling, sputtering, melting and stress; size the thickness, backing, cooling and current density from a stopping-power and heat-load calculation (dg-1211), and treat the rolled-versus-evaporated choice as a durability bonus on top of that, not a substitute for it.
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Rolling feedstock should be a clean solid bead (Kellner & Maier-Komor): pressed-and-sintered powder shows severe disadvantages - grain-boundary defects end rolling early - and arc melting loads the bead with gaseous impurities; their route melts 50-500 mg portions with an electron gun in a water-cooled copper crucible, lets the drop solidify slowly from the cooled side so impurities concentrate in a last-frozen 'stalagmite' that is cut off, repeating ~10 times for uranium.
e-beam zone refining by slow solidification + stalagmite cutting, ~10 cyclesSource quote & editorial note
The older method of pressing the metal powder and sintering it under vacuum shows severe disadvantages. The defects at the grain bounderies [sic] set an early limit during the rolling process. Arc melting has disadvantages too, there may be many gaseous impurities in the processed metal bead ... The metals are melted in portions from 50 to 500 mg in a water cooled copper crucible with an electron gun keeping the temperature just above the melting point. ... the drop solidified starting with the zone nearest to the water-cooled crucible. The part of the drop which solidified last was formed like a stalagmite and was highly enriched with impurities. After venting with argon this stalagmite can be cut away and the procedure can be repeated. For Uranium we did this about 10 times.
Editorial note, tabletop extrapolation: Explains why bought powder pressed into a pellet resists rolling thin (porosity and grain-boundary defects - fully densified stock is the exception); the repeated directional solidification rejects the impurities whose segregation behavior is favorable, not all of them - the authors themselves found true zone refining fails on uranium (surface tension) and used this slow-solidification variant instead.
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Pack (sandwich) rolling jacket spec: bright-annealed, temper-passed stainless of 0.5 mm or thinner, LOW carbon (<0.03%, low grain disintegration) for most metals, or ~0.1%-C spring steel for metals less ductile than nickel; use vacuum-melted stainless for the inner jacket — ordinary cold-rolled band carries ingot-scale texture lines that slice thin foils into strips along the rolling direction.
jacket <=0.5 mm, surface roughness 0.05-0.1 um; low-C Cr-Ni stainless (or spring steel for brittle metals); vacuum-melted sheet for inner jacketSource quote & editorial note
For rolling metals with a ductility lower than nickel or iron one should take as sandwich material a stainless steel with a high carbon content named spring steel band. This material has a higher temper due to its carbon content of about 0.1%. All other stainless steel sandwiches should be made of a Chrom-Nickel steel with extreme low carbon content. There are some materials available with a carbon content below 0.03%. ... We noticed that material with a thickness of 0.5 mm or below gave the best results. ... This material should be bright-annealed in an inert gas atmosphere and be dressed in a temper pass mill, to get a highly polished oxide-free surface. The surface roughness for the best quality material is of the order of 0.05 to 0.1 [um] ... These lines are strictly parallel and always along the texture of the sheets ... The source of these inhomogeneities are the scales which remained on and in the ingot before machining it to cold rolled band steel. Vacuum melted stainless steel does not have these impurities. ... We use it for the inner part of our double sandwich.
Editorial note, tabletop extrapolation: The foil replicates the jacket's flaws (the source's central claim, conditioned on an accurately designed mill) - jacket steel selection is the dominant quality variable in pack rolling once the mill itself is true; roll finish, alignment and reduction schedule still matter on amateur equipment.
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Pack-rolling schedule for the cited uranium/molybdenum work (Kellner & Maier-Komor): reduce about 3-10% per pass, and when the jacket has grown to about twice its size, transfer the foil to a fresh jacket (the double-sandwich variant and its thresholds are the paper's further detail - scan re-read queued).
3-10% reduction/pass; re-jacket at 2x elongation; double sandwich (0.1-0.2 mm inner) below 5-10 mg/cm2Source quote & editorial note
reduced by about 3 to 10% per pass. When the jacket increased its size by approximately a factor of two the foil is placed in a new jacket (Kellner & Maier-Komor, "Rolling Thin Uranium Foils")
Editorial note, tabletop extrapolation: A worked schedule showing sub-mg/cm2 rolling is a craft with rules, not heroics - transfer the discipline (small reductions, fresh jackets on elongation) and expect each metal to demand its own trials: permissible reduction, annealing needs and attainable thickness are material-specific.
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Anneal rolled foils between resistively-heated tantalum sheets in good vacuum for ~30 min at a temperature chosen below the metal's phase transition (uranium: below 930 K at 1e-7 torr, to stay in the alpha phase); etch the oxide first with highest-purity dilute nitric acid, because a reactive foil picks up reducible metal contaminants from a dirty acid. [Corrected 2026-08-23: earlier text said the foil 'getters every metal impurity', which overstates the chemistry.]
anneal ~30 min, 1e-7 torr, T below phase transition (U < 930 K)Source quote & editorial note
If oxidation on the surface of the Uranium foil is observed it should be etched with diluted nitric acid of the best quality, because all metal impurities in the acid will be catched by the Uranium foil due to its very negative electro-chemical potential of -1.8 volts. After cleaning in oxygen free distilled water and ethanol the foil is annealed between two Tantalum sheets which are heated by an alternating current. The annealing lasts for about half an hour in a vacuum of 10-7 Torr at a temperature below 930 K, which was chosen to prevent phase transitions.
Editorial note, tabletop extrapolation: Interpass and final annealing is what keeps a work-hardened foil rollable and flat. The phase-transition ceiling is the uranium-specific reason here; for any other allotropic metal choose the anneal from its own phase diagram and the phase or texture you want - some iron and titanium treatments deliberately cross a transformation. [Note revised 2026-08-23: earlier note generalised 'below any phase transition' to all allotropic metals.]
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The experiment chamber vacuum is part of the target lifetime budget for reactive metals: uranium foils that left the lab metallic were destroyed as oxide in 1-2 h of beam at 1e-5 torr chamber pressure (ion-getter-pump-like oxidation at the beam spot); adding a cryopump to reach 1e-6 torr extended life to many hours.
1e-5 torr chamber -> reactive foil oxidizes to death in 1-2 h under beam; 1e-6 torr -> much longer lifeSource quote & editorial note
In the first experiments the Uranium foils were destroyed by a heavy ion beam during the first 1 or 2 hours. The monitor spectrum showed almost pure Uranium oxide. ... The problem was a poor vacuum of 10-5 Torr in the scattering chamber which allowed oxidation similar to the effect in an ion getter pump. In the next experiment the vacuum was in the 10-6 Torr range due to an additional cryo-pump and the targets lived much longer, but one could see still in the monitor spectrum, that oxidation took place.
Editorial note, tabletop extrapolation: A 1e-5-torr-class chamber actively burned this reactive uranium target under beam - the beam spot acting like a getter pump. For any reactive target, budget life against chamber pressure (and specifically oxygen/water partials), expect oxide growth in the monitoring spectrum as the early warning, and treat the uranium numbers as that experiment's calibration, not thresholds.
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Reactive sputtering produces even, tough, adherent nitride films with easy thickness control (Stinson): DC sputtering of Ta or Ti in low-pressure N2 - with the paper's own numbers carrying an internal transposition: it rates TaN at 1-1.5 and TiN at 3-4.5 ug/cm2-min, yet its examples make 36 ug/cm2 of TaN in 8 min (4.5) and TiN in 32 min (1.1) - the material labels on the rates and the examples cannot both be right (dg-501 pattern; scan re-read queued).
DC sputtering ~3 kV / 30 mA at ~80 um N2; rates TaN 1-1.5 ug/cm2-min, TiN 3-4.5 ug/cm2-min; 36 ug/cm2 TaN in 8 minSource quote & editorial note
Even, tough films, easy thickness control and production of self supporting targets are other advantages inherent to the process (Stinson, "Nitrogen Targets Produced by Reactive Sputtering of Tantalum and Titanium") ... Tantalum nitride targets with a thickness of 36 ug/cm2 were produced by sputtering for eight minutes. Titanium nitride targets of the same thickness required 32 minutes. ... the sputtering rates range from 1 to 1.5 ug/cm2.min for tantalum nitride, and from 3 to 4.5 ug/cm2.min for titanium nitride.
Editorial note, tabletop extrapolation: Sputter deposition is the durable-target counterpart to the ORNL-3021 evaporation recipes - slower, but the film adheres and survives beam heating; backing choice and beam-power suitability still get verified per design rather than assumed from the process name.
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Keep hydrocarbons out of any sputtering/discharge deposition system — they crack in the discharge and load the film with carbon or carbides — and condition before deposit: outgas substrates hot, pre-sputter 10-15 min with shutters CLOSED onto the shield to expose fresh cathode, dump the contaminated gas, then refill and open the shutters with the cold trap filled.
oil-free pumping (sorption + sputter-ion in the source system); 15-min closed-shutter pre-sputter; captive reactive gas replenished as consumedSource quote & editorial note
Hydrocarbons crack during the sputtering process and deposit car[b]on or form carbides with the refactory [sic] metals used (Stinson, "Nitrogen Targets Produced by Reactive Sputtering")
Editorial note, tabletop extrapolation: The same cracking chemistry threatens any glow discharge backed by an untrapped oil diffusion pump - hydrocarbon backstreaming can contaminate whatever the discharge sees. Condition the discharge on a closed shutter before exposing the workpiece (removes initial cathode contamination), and control CONTINUING contamination with a working cold trap/baffle or oil-free pumping - the shutter trick does not cure ongoing backstreaming.
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An uncooled sputtering cathode heats up during long runs and the sputter rate climbs with it, so deposited thickness is NOT linear in time — either water-cool the cathode or calibrate thickness against weighed samples rather than clock time.
rate spread 1-1.5 (TaN) and 3-4.5 (TiN) ug/cm2-min attributed to cathode heatingSource quote & editorial note
the longer sputtering times required for thick targets produce higher temperatures, and higher rates (Stinson, "Nitrogen Targets Produced by Reactive Sputtering")
Editorial note, tabletop extrapolation: Applies to any deposition where the source drifts hot — time-based thickness control needs either thermal steady state or an in-situ monitor (quartz crystal, witness plate).
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Protect oxidation-prone target layers as a sandwich (Folger & Klemm): evaporate 0.01-0.2 mg/cm2 of carbon, titanium, nickel or gold over the active layer; their thick layers (20-100 mg/cm2) went bare onto ~2-mm copper chips instead.
protective covers 0.01-0.2 mg/cm2 (C/Ti/Ni/Au); 20-100 mg/cm2 layers evaporated onto 2-mm-thick, 25-mm-dia copper chipsSource quote & editorial note
Evaporated films of carbon, titanium, nickel, or gold of 0.01 to 0.2 mg cm-2 are used to protect the uranium layers from oxidation (Folger & Klemm, "Uranium Sandwich Targets of 0.1 to 100 mg-cm-2")
Editorial note, tabletop extrapolation: Two transferable patterns, each with arithmetic attached: a cover layer buys shelf life and in-beam oxidation resistance at an energy-loss cost that is NOT negligible at sub-MeV energies (0.2 mg/cm2 of gold takes a real bite - run the stopping numbers for the actual beam and cover); and a thick copper chip spreads heat but sinks it only through a designed low-resistance path to actual cooling.
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Refractory-metal evaporation practice from the cited tungsten work (Ellsworth): electron-bombardment heating of an outgassed isotope ball on a tungsten pedestal in a water-cooled crucible; higher evaporation rates gave LESS stressed targets, and tank pressure above 4e-6 torr made the films brittle with short shelf life.
6 kV / 130 mA loop-filament e-bombardment; pressure ceiling 4e-6 torr; NaCl on 10-mil stainless at 400-600 F; 0.1-0.3 mg/cm2 self-supporting from 300-500 mg of isotopeSource quote & editorial note
Tank pressure above 4 x 10-6 torr made the targets more brittle and shortened their shelf life (Ellsworth, "Preparation of 3/4-in Dia. Self Supporting 182W and 184W Targets for Cyclotron Bombardment")
Editorial note, tabletop extrapolation: Transfer the method - control pressure, rate and substrate temperature, then calibrate stress, adhesion and shelf life on the actual material - not the tungsten numbers: the 4e-6 torr boundary and the rate-stress trend are that process's results, and residual stress can move the other way in another material/substrate system.
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What kills solid targets as current rises (Tietsch et al.): where heat conduction is poor, beam-spot temperatures reach ~3000 C - past the melting points of most usual target materials; their answer was a windowless supersonic gas-jet target (the failure-mode inventory and jet parameters are the paper's account - scan re-read queued).
Laval-jet density knot ~5 mm long x 3 mm dia; thickness linear in inlet pressureSource quote & editorial note
in cases of poor heat conduction temperatures up to 3000 C occur and exceed therefore the melting points of most of the usual target materials (Tietsch, Feist, Bethge & Schopper, "A High Density Windowless Gas Jet Target")
Editorial note, tabletop extrapolation: The checklist stands: conduction, charge relief and structure all have to be engineered as current rises, and a gas target is the limiting alternative when no solid survives - trading foil failure for nozzle, flow-stability and differential-pumping engineering rather than achieving unbreakability.
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Mount curl-prone foils on frames pre-coated with Canada Balsam dissolved in xylene: once the solvent dries the balsam stays tacky indefinitely at low vapor pressure and retains foils that would otherwise curl off on drying; keep a cover frame over freshly floated films until dry.
Canada Balsam in xylene, applied to frame, solvent dried before pick-upSource quote & editorial note
The Balsam remains tacky and retains foils indefinitely. It also has a low vapor pressure (Riel, "Gallium Rich Ga2O Targets for Use at Room Temperature")
Editorial note, tabletop extrapolation: A tacky mounting adhesive solves the foil-jumps-off-the-frame failure of float-mounting; pairs with the ORNL-3021 float-off recipes. 'Low vapor pressure' is the source's claim for their chamber - run an outgassing/base-pressure test (and consider beam-induced decomposition near the spot) before trusting balsam in a tighter vacuum budget.
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Rollability of chromium is set by chemistry (Friebel et al.): small impurities of nearly all metals at the few-hundred-ppm level largely enhance brittleness - so the reduction route chosen upstream fixes the ductility available downstream (their route choice and processing thresholds are the paper's account - scan re-read queued).
few-hundred-ppm impurities embrittle Cr; ductile fragments 10-15 mg; interpass anneals above 1 mg/cm2; minimum reached 700 ug/cm2Source quote & editorial note
small impurities of nearly all metals in the order of magnitude of a few hunderd [sic] ppm largely enhance the brittleness (Friebel, Frischke, Grossmann & Maier, "Preparation of Isotopically Enriched, Self Supporting Chromium Targets")
Editorial note, tabletop extrapolation: When a foil cracks in the mill, suspect chemistry before technique - assay or provenance-check the stock before burning days on rolling variables. The few-hundred-ppm sensitivity is chromium's measured result; treat other brittle metals as innocent until their own data convict.
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Derive the gas-purity spec for hydrogen reduction from equilibrium thermodynamics (Friebel et al.): for their Cr2O3 + H2 process the equilibrium maximum tolerable water content of the hydrogen was 540 ppm - with the practical spec set well below it for workable kinetics (their temperature, working ppm and furnace time are the paper's recipe - scan re-read queued).
p(H2O)/p(H2) equilibrium ratio 5.4e-4 at 1400 K (Cr2O3); working spec <=10 ppm; 6 h at 1400 K for completionSource quote & editorial note
in equilibrium the maximum tolerable water content of the hydrogen atmosphere is 540 ppm (Friebel et al., "Preparation of Isotopically Enriched Chromium Targets")
Editorial note, tabletop extrapolation: The template for judging whether tank-grade gas is good enough for any reduction or annealing atmosphere: compute the equilibrium H2O/H2 ratio at the furnace temperature before blaming the furnace - then verify the DELIVERED atmosphere (dew point or oxygen potential at the work zone), since a purifier's outlet spec says nothing about downstream leaks and outgassing.
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Thick carbon foils (1-8 mg/cm2) need no evaporator (Lozowski): settle 325-mesh graphitized powder from an air suspension onto carbon-coated glass, then press at ~14 tons/in2 into a lustrous flexible film (uniformity <10%); the tested amorphous powder was rejected - it would not bind, and its low thermal conductivity and high resistivity made it a poor choice for their accelerator targets.
325-mesh graphitized (2500 C) powder; 14 ton/in2 (1.93e8 N/m2) between carbon-coated glass; 1-8 mg/cm2, uniformity <10%Source quote & editorial note
additional properties of low thermal conductivity and high electrical resistivity reveal it to be a poor choice for accelerator targets (Lozowski, "A Dry Powder Technique for the Preparation of Carbon Foils")
Editorial note, tabletop extrapolation: Beam-stopping carbon from a powder blower and a hydraulic press - plus the selection principle that a target material must conduct heat and charge away. The amorphous-carbon verdict belongs to that powder and process: evaporated amorphous-carbon foils serve routinely as accelerator targets and strippers, so judge each carbon form on its measured conductivity and binding, not the category.
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Ion-beam power density on a sputter target forces cooling (Baumann & Wirth): at their ~10 kV and 2-4 mm focus the loading exceeded 100 W/cm2 and a low-conductivity surface ran several hundred C - hot enough to oxidize reactive materials mid-deposition and spoil thickness reproducibility - so the material post required cooling.
q'' = f*V*I/(pi*(d/2)^2) with current, intercepted fraction and duty explicit - voltage and spot size alone cannot give a flux; the cited >100 W/cm2 is their operating point's resultSource quote & editorial note
a cooling system for the target material post is required (Baumann & Wirth, "A Heavy Ion Sputtering System with a Penning-Ion-Source")
Editorial note, tabletop extrapolation: The same arithmetic sizes cooling for beam stops, probes and targets on a small machine: compute the flux from the actual current, spot and duty (mm-scale spots reach 100 W/cm2-class loading at mA-and-tens-of-kV operating points, not automatically at tens of uA), then get temperature from a stated thermal model before deciding whether cooling is needed.
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For long uninterrupted deposition runs, the cited cold-cathode Penning source made its case: 165 hours of stable beam without any trouble (0.2% stability at 0.58 mA), no filament to burn out, run on reactive gas, at under 30 W total source power.
PIG end-extraction source, 120 mm dia x 70 mm; up to 2 mA Ar; energy spread 40-80 eV; gas consumption 1-5 std-cm3/min; <30 W totalSource quote & editorial note
the source ran with a stable ion beam intensity for 165 hours without any trouble (Baumann & Wirth, "A Heavy Ion Sputtering System with a Penning-Ion-Source")
Editorial note, tabletop extrapolation: The filament-free argument is the same one that favors PIG sources inside a cyclotron, and the documented design point (geometry, discharge mode, gas flow, stability) is valuable prior art - as a demonstrated result, not a category win: PIG cathodes still sputter and erode, chemical resistance is gas- and materials-specific, and whether <30 W runs uncooled depends on where the watts concentrate and what the mounting conducts. Check those for the actual build.
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Electrodeposited platinum targets proved less fragile in beam than evaporated ones in the cited work (Saettel), with ~250 mA/cm2 the workable compromise (higher densities gave spongy deposits) - but the paper's numbers carry an internal tension: at 250 mA/cm2 even 20% Faradaic efficiency would deposit ~1.5 mg/cm2-min, not the stated ~3.6 ug/cm2-min, so either the current-density unit, the rate, or the meaning of its 20% 'yield' needs the scan re-read before use (dg-501 pattern).
Pt at 250 mA/cm2, ~3.6 ug/cm2-min, thickness linear in time and current density; yield ~20% (vs 85% for Fe/Ni/Zn plating)Source quote & editorial note
they are less fragile than those made by evaporation in that they withstand the accelerator beam better (Saettel, "Preparation of Self-Supporting Platinum Targets by Electrodeposition")
Editorial note, tabletop extrapolation: Electroplating joins rolling on the durable side of the durable-vs-evaporated divide, and it works at milligram scale with a beaker and a regulated supply - for platinum by this process on this evidence; other metals earn the durability label with their own beam tests.
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Carbon foil breakage under ion beams tracked TOTAL integrated fluence in the cited study (Livingston, Berry & Thomas): over their tested species, energies and 2-22 ug/cm2 thickness range, breakage time depended on the total number of bombarding ions, following tau(p-uA-min/mm2) ~ A*E^1.15 with A per species (their fit).
cited fit: tau(p-uA-min/mm2) = A*E^1.15 (MeV/amu); A ~20 (Ar), ~60 (N), ~5 (Ni, Br); thickness-independent over their 2-22 ug/cm2 testsSource quote & editorial note
the foil breakage time is dependent on the total number of bombarding ions (Livingston, Berry & Thomas, "Thin Carbon Foil Breakage Times Under Ion Beam Bombardment"; reprint of NIM 148 (1978) 125)
Editorial note, tabletop extrapolation: Plan foil replacement by integrated charge where the fluence law holds - and verify it holds: dose-rate heating, spot profile and mounting can break the current-independence outside the tested window. Thickness buys nothing in beam life WITHIN the cited range, so choose it from mechanics, handling and dispersion - not as a lifetime lever.
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Optical transmittance calibrates surface density for evaporated METAL films too (Al, Cr, Cu, Au, Ag, Sn, Ti; ~+-20% at 546.1 nm) — but gravimetric calibration fails on slides coated with soap-like parting agents, which lose weight in vacuum; reactive metals (Ti, Al, Cr) reproduce worst because of oxide/gas uptake.
transmittance vs ug/cm2 curves at 546.1 nm, +-20%; Al/Cr/Sn/Ti useful to ~50-80 ug/cm2, Ag/Au/Cu to ~300 ug/cm2Source quote & editorial note
For evaporated metal coatings (Al, Cr, Cu, Au, Ag, Sn, and Ti) we have developed curves of optical transmittance vs surface density that can be used to estimate surface densities to within about +-20%. ... measured at 5461 A ... it was not possible to carry out accurate measurements with slides that had been coated with a soap-like parting agent, since these would lose weight upon being placed in vacuo. ... It is certain that all of our coatings were contaminated either by oxide layers, burial of residual gas, and/or adsorption of active molecules. The curves indicate such effects by the extent of their non-reproducibility, most serious for the active species
Editorial note, tabletop extrapolation: Extends the carbon transmittance gauge to the metals a small lab actually evaporates; weigh calibration slides bare, never soaped — the parting agent is part of the tare and it evaporates.
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Kill pinholes by fixing the SUBSTRATE: an argon glow discharge 'leveled' the commercial copper foil in the cited 208Pb work, enabling pinhole-free films (the film thickness, area and boat-mapping data are the paper's results - re-read queued).
Ar glow discharge ~1 h on Cu substrate; boat maps (200 mg Pb, 8x8 cm grid): chimney at 1.5 cm -> one 1.5-cm spot; central-hole at 5/10/15 cm -> 20/43/80% relative edge thicknessSource quote & editorial note
The sputtering "leveled" the copper surface (Meens, "Vacuum Tight 208Pb Foils")
Editorial note, tabletop extrapolation: Two habits transfer: substrate preparation is a first-order pinhole control (one control among several - particulates, shadowing, stress and coverage also make holes), and a sacrificial natural-material run with a grid of weighed squares characterizes a boat geometry FOR THOSE CONDITIONS - remap when loading, material, rate or distance change.
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Load titanium with hydrogen by heating in sub-atmospheric purified gas (Gursky & Sherwood): outgas at 800 C in vacuum first, absorb at ~650 C, pass the gas through a deoxygenating cartridge AND a liquid-nitrogen trap - the trap is essential; the gas is not absorbed otherwise - and meter uptake as the pressure drop in a known volume (via n = d(PV/RT), converting to STP volume afterward if wanted); reversible by pumping at 800 C.
absorb at ~650 C sub-atmospheric; outgas 800 C; uptake = dP * V_system at STP (example - 0.817 of available gas absorbed, 130 cm3 per cone)Source quote & editorial note
The trap is essential; the gas is not absorbed otherwise (Gursky & Sherwood, "Hydriding of Titanium Cones for a Sputter-Ion Source")
Editorial note, tabletop extrapolation: The bench recipe for Ti-H or Ti-D loaded pieces - executed as a hydrogen process, not a casual one: hydrogen-rated containment and plumbing, leak checking, ventilation and ignition control, and a trap that gets inspected (an LN2 trap can concentrate oxidants if purification fails). Tritium is a different world entirely - licensed containment, monitoring and recovery - and is not an amateur variant of this recipe.
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Size the target heat problem by straight beam-power arithmetic before any material choice: P(W) = particle rate x energy per particle. Folger (GSI) example: 3e11/s of 17.5 MeV/u 238-U carries ~208 W total; focused to ~0.2 cm^2 that is ~1 kW/cm^2 specific deposition.
P[W] = (dN/dt) * E[J]; specific load = P / spot areaSource quote & editorial note
If the beam is focused to an area of about 0.2 cm2, the resulting specific energy depositions amounts to 1 kW/cm2.
Editorial note, tabletop extrapolation: The reference machine at ~3 nA / ~150 keV deposits ~0.5 mW - no realistic solid target is troubled by half a milliwatt. Rerun the two-line arithmetic at every upgrade, using the energy LOST IN the target rather than incident beam power where targets are thin: a 10 uA / 1 MeV machine puts up to 10 W into a mm-scale spot, which is rotating-target or water-cooled-backing territory.
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Rotate the target when average power exceeds what a static foil stands: Folger (GSI) ran 9 sector ("banana") targets covering 59.6% of a 97.4 cm circumference at 15.5 cm radius, spun at 666 rpm phase-locked to the beam macropulse (20 degrees per 5 ms pulse) so successive pulses hit different targets; ~1e17 particles were integrated without significant radiation damage.
wheel synchronization; 666 rpm = 20 deg per 5 ms macropulse (25% duty, 5 ms in 20 ms)Source quote & editorial note
The wheel thus had to be rotated at a velocity of 666 rpm (equal to 20 deg in 5 ms or during one macropulse).
Editorial note, tabletop extrapolation: The design move transfers whole: spread the duty over many target areas, and if the beam is pulsed, phase-lock the rotation so no spot sees consecutive pulses - it scales to a bench wheel behind any external beamline. The 1e17-particle survival belongs to GSI's target, beam and cooling; a tabletop wheel's achievable dose comes from its own thermal, stress and deposited-dose arithmetic.
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Interlock target rotation with the beam - Folger's account: a GSI rotating disc of Au targets survived its designed beam load while spinning, but a target exposed to full beam with the drive motor switched off (the quoted event) was destroyed, the paper's SEM showing molten zones.
Source quote & editorial note
exposed to the full beam intensity while the disc-driving motor was already switched off
Editorial note, tabletop extrapolation: Folger's before/during/after SEM sequence is the reference picture of beam kill on a metal foil. Any moving-target scheme needs a rotation-OK permissive in the beam interlock chain: a stalled wheel concentrates the whole designed-for-distributed load on one spot.
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Sandwich low-melting-point target metals between carbon layers - GSI practice for Pb and Bi on high-current wheel targets, e.g. C/Bi/C at 0.03/0.5/0.03 mg/cm2 - extending stability and lifetime under bombardment.
C/metal/C sandwich, typ. 0.03 / 0.5 / 0.03 mg/cm2 - i.e. 30 ug/cm2 of carbon per side, 60 totalSource quote & editorial note
Low melting-point elements like Pb or Bi are sandwiched between C layers for the use on target wheels, thus extending the stability and life-time
Editorial note, tabletop extrapolation: A demonstrated construction for Pb/Bi-class soft metals; for another soft metal, run the compatibility, adhesion and beam tests before promoting it to recipe. Budget the carbon honestly - 60 ug/cm2 total is real material in a sub-MeV beam's energy-loss budget - and credit the skins with mechanical containment first; the thermal mechanisms are plausible but unquantified here.
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Multi-layer overcoats buy target lifetime through conduction: the 1983 heavy-ion discussion recorded that metal/carbon overcoat layers appear to enhance thermal and/or electrical conductivity, shunting both thermal gradients and accumulated charge to the heavy frame around the target - significantly increasing lifetime; energy accumulation showed up as local melting, evidenced by broadening of scattering peaks.
Source quote & editorial note
Additional features of such multi-layer targets appear to be their enhanced thermal and/or electrical conductivity. Both thermal gradients and electrical charge generated in or on the target during bombardment appear to be shunted to the relatively heavy frame surrounding the target. This improved energy transfer tended to significantly increase target lifetime under bombardment. Accumulation of energy was also reported to cause local melting of the target material as evidenced by significant broadening of scattering peaks.
Editorial note, tabletop extrapolation: Two transferable ideas: treat the frame as the heat sink and design the film-to-frame conduction path deliberately; and watch the elastic-scattering (or yield) peak width online as a degradation warning - broadening flags trouble worth investigating (melting is one cause; thickness change, roughening, charging and detector drift are others).
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Protect reactive target metals with a thin sacrificial overcoat, sized by experiment: Argonne reported lithium (500 ug/cm^2 on pinhole-free Ni) protected by ca. 500 ug/cm^2 of copper — possibly as thin as 100 ug/cm^2 — which held oxygen/moisture attack off for about five minutes of air exposure; gold at 30-40 ug/cm^2 gave only marginal protection.
Cu overcoat ~100-500 ug/cm^2 on Li; ~5 min air handling windowSource quote & editorial note
Representatives from Argonne National Laboratory indicated their partial success using a thin layer of copper (ca. 500 ug/cm2 or less). With this protection, it was observed to take five minutes before any significant amounts of oxygen or moisture were detected. The minimum thickness of copper required was indefinite, but 'it could possibly be as thin as 100 ug/cm2'. The overcoating was successful with lithium layers of 500 ug/cm2 on pin-hole free nickel substrates. ... others in the group indicated only marginal success with gold coatings. The thickness suggested for the gold layer was 30-40 ug/cm2.
Editorial note, tabletop extrapolation: Sets the realistic SCALE for air-handling of reactive targets - minutes, not hours - from one measured case (Li under Cu, with 'partial success' and detection-limited timing): use inert transfer where possible, validate each target/overcoat pair, and remember overcoat nuclei scatter too, so the coating choice is coupled to the experiment.
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Monitor target condition in-beam rather than trusting pre-weighing (GSI practice): a surface-barrier detector watching the elastic-scattering peak at a fixed forward angle - broadening of the peak indicates target changes or damage - with detectors calibrated against weighed standard targets and counts tagged by target-wheel position for per-target histories.
Source quote & editorial note
broadening of the peak indicates target changes or damages
Editorial note, tabletop extrapolation: A silicon detector at a fixed forward angle is cheap on any small machine and the lightest target diagnostic going: baseline the peak width first (detector resolution, kinematic broadening and straggling all live in it), then read CHANGES as the damage flag. For luminosity, use the calibrated integrated peak yield at known cross-section and acceptance - the width tells you about the target, the counts about the luminosity.
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When resolution does not matter, diffuse the beam (Ford, ORNL/HHIRF): their class-1 experiments ran rolled 0.5-5 mg/cm2 targets at 0.5-5 electrical uA and deliberately spread the beam spot on the target to manage heating.
Source quote & editorial note
target heating can be a problem and efforts are made to diffuse the beam on the target.
Editorial note, tabletop extrapolation: Spot size is a powerful cooling knob - average flux is P/(pi*r^2), so doubling the radius quarters it - but use it inside a checked budget: compute beam power and allowable target temperature first, confirm the full swept or defocused beam still lands on target (not the holder), and treat active cooling, temperature monitoring and beam-trip protection as their own requirements rather than things defocus postpones.
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For small-quantity evaporations the flagged failure mode is a molten ball overheating the substrate (1983 general-targets discussion): cool the substrate or back it with a heat sink, and keep the heating beam off the water-cooled hearth (the isotope-quantity and boron-pedestal specifics are the discussion's further detail - scan re-read queued).
Source quote & editorial note
An important problem is overheating of the substrate by a large, molten ball of material.
Editorial note, tabletop extrapolation: Relevant to boron and enriched-isotope work in a bench evaporator: budget the substrate's heat exposure from the melt's radiation before the run, and confine the molten zone to the charge - with the pedestal dimensions and per-method details taken from the re-read source rather than memory.
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Balance substrate heating against water cooling with visible diagnostics: Hinn (U. Washington) deposited thick Si on 0.3 mil Cu foil clamped loosely to a water-cooled copper beam-stop block; if pitting or burn-up of the foil occurs, increase cooling; if the deposit curls as it thickens, increase heating by slowing the water flow. Substrate sat at 900-1000 C purely from 35 mm source proximity.
Source quote & editorial note
If pitting or burn-up of the copper foil substrate occurs increase cooling. if curling occurs as the deposit thickens, increase heating
Editorial note, tabletop extrapolation: The pitting-vs-curling pair is a tuning heuristic FOR THE CITED Si-on-Cu hot-deposition process, readable by eye - worth copying for similar hot depositions onto cooled backings (with the loose clamp so the foil can contract), but check independent temperature limits first: pitting can also mean excess flux or chemical attack, and curling can be contamination or expansion mismatch, where more heat makes things worse.
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Make elemental Si from enriched SiO2 by magnesium reduction in a closed crucible (Hinn) - SiO2 + 2Mg -> Si + 2MgO - avoiding a large excess of Mg, which forms Mg2Si instead of Si (the full recipe - charge masses, firing cycle, leach and outgassing - is the paper's procedure; scan re-read queued, including reconciling its ~70% yield against the ~93 mg theoretical Si from 200 mg oxide).
SiO2 + Mg reduction; 200 mg oxide to 170 mg Mg; ~70% yieldSource quote & editorial note
A large excess of Mg must be avoided to preclude formation of Mg2Si instead of Si.
Editorial note, tabletop extrapolation: The metallothermic pattern (reductant choice, closed crucible, acid leach of the oxide by-product) is the standard route from affordable oxide feedstock to a solid target. Boron-from-oxide is its own chemistry with its own purification and hazards - parallel in shape, not in recipe.
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Internally stressed deposits can have a shelf life: Hinn's silicon targets slowly curled and fractured in storage (his lifetime, mechanism and recovery details are the paper's account - scan re-read queued).
Source quote & editorial note
they would slowly curl and fracture
Editorial note, tabletop extrapolation: Plan target fabrication against the run schedule, not the calendar, for any film KNOWN to carry stress - and qualify rather than generalize: store finished targets under vacuum or argon, inspect periodically, and learn each film type's actual shelf behavior from a witness piece instead of assuming a universal use-within-weeks rule.
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Slackened stripper foils lived about ten times longer than taut ones at ATLAS (Pardo): 2 ug/cm2 arc-evaporated carbon mounted on a holder whose diameter is then reduced to slacken the film; ORNL mass-produced slackened foils by mounting them still wet in an airstream so they slip on the frame.
slackening ~10x foil lifetimeSource quote & editorial note
slackening gives approximately an order of magnitude increase in the foil lifetime.
Editorial note, tabletop extrapolation: Deliberate slack is a proven mounting method for thin STRIPPER-class foils, where letting the film move beats letting it tear - one mechanism among several (sublimation, sputtering and radiation damage also kill foils, in shares that depend on the beam). It does not generalize to pressure-bearing windows or thickness-critical degraders, which need controlled tension or support by design; budget spare stock either way.
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Treat stripper/degrader foils as magazine-fed consumables and design the changer in from the start: HHIRF's tandem carried a 180-foil magazine (5-10 ug/cm^2 glow-discharge carbon); a slackened foil under a 1 uA, 10 mm^2 127-I beam at 25 MV was expected to last only ~1 hour (Ford).
Source quote & editorial note
is expected to be only the order of 1 hr.
Editorial note, tabletop extrapolation: The engineering lesson: when estimated or measured consumable lifetime makes venting burdensome, design in-vacuum replacement (magazine or multi-position ladder) from the start - it costs little at design time and a vent-and-pump cycle per failure otherwise. The ~1 hour is the cited 127-I conditions; estimate a proton foil's life from its own thermal and dose numbers before deciding.
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Foil flatness is an orbit-quality parameter: ripples increase the effective source thickness and thereby degrade performance - the flatness requirement Chalk River states for its in-dee stripper-foil system (the chain-changer mechanism, lifetimes and magazine details are the paper's description - re-read queued).
Source quote & editorial note
foils must be flat since ripples increase the effective source thickness and thereby degrade the performance.
Editorial note, tabletop extrapolation: The cleanest statement in this collection that foil flatness is physics, not cosmetics - applicable to any internal foil in proportion to how its incidence geometry turns ripple into path-length spread; and the Chalk River system stands as an existence proof that in-vacuum consumable-changers can share space with a live dee structure (details per the re-read).
-
On stripper-foil fabrication comparisons the cited discussion's verdict (Adair) is skepticism: no method seemed superior to arc-evaporated foil, because published lifetime comparisons mostly used different beams and current densities - the call was for same-beam, side-by-side tests (the thickness-regime observations are the discussion's detail - scan re-read queued).
Source quote & editorial note
no method seems superior to the arc evaporated foil.
Editorial note, tabletop extrapolation: Two lessons: distrust any foil-lifetime or target-durability claim not measured under your own beam and current density, and settle fabrication-method questions with a side-by-side test on the actual machine rather than the literature's confounded comparisons.
-
The saddle-field source ran cold in the cited setup: a cold filament producing a temperature rise of the evaporant of only ~10 C (the beam-neutral fraction, focus size and insulator capability are the paper's further characterization - re-read queued).
Source quote & editorial note
a cold filament which produces a temperature rise of the evaporant of only ~ 10 C
Editorial note, tabletop extrapolation: A candidate route to boron and refractory films without an e-gun - qualified in place: a small bulk temperature rise does not preclude local sputter damage to a substrate or release layer, so verify with witness pieces; the commercial gun class is bench-scale, and its insulator/neutral-beam claims come from the re-read source, not the summary.
-
Saddle-field sputter-gun geometry (Thomas, ANL): the gun at thirty degrees to the target surface and about 5 cm from the sputter source - steeper angles back-sputter material into the gun (the operating pressures, current and alignment notes are the paper's account - scan re-read queued).
30 deg incidence, 5 cm standoff, ~1e-5 Torr, ~2 mA @ 6 kVSource quote & editorial note
the gun be at a thirty degree angle to the horizontal surface and about 5 cm from the sputter source.
Editorial note, tabletop extrapolation: Useful geometry prior-art for a sputter gun in a diffusion-pumped bell jar of exactly the archive's class - commissioned as HV apparatus, not from a recipe card: engineered enclosure, current limiting and bleeders, grounding, door and pressure interlocks, and the pump's own precautions come before first beam; the visible beam then makes alignment easy.
-
Budget time, not power, for sputtered targets: the reported saddle-field rates ran about 4-44 ug/cm2 per hour by material (Au ~44, Sn ~14, W ~12.5, Ni 5-13, Fe 4-10, Si ~4), with about half an hour to stabilize; the cited rig then ran virtually unattended for days with only slight adjustments.
Au ~44, Sn ~14, W ~12.5, Ni 5-13, Fe 4-10, Si ~4 ug/cm2/hr - schedule per material: 1 mg/cm2 is ~23 h at the Au rate, ~250 h at the Si rate (verify rate linearity at thickness)Source quote & editorial note
it can be left virtually unattended overnight and usually for several days with only slight adjustments.
Editorial note, tabletop extrapolation: Schedule per material from the actual rate - Au-class films are an overnight job, Si-class a couple of weeks - or reserve sputtering for thin layers and adhesion coats. Unattended running was the cited lab's practice; an amateur HV/vacuum rig earns that only with interlocks that fail safe.
-
Focused-ion-beam sputtering economizes scarce isotopes: GSI consumed only 2.3 mg of Zr in preparing five 0.1 mg/cm2 targets (1 mA / 10 kV Ar+ focused ~1 mm, Sletten-type apparatus); self-supported rare-earth sputter layers were routine after dissolving a copper substrate.
2.3 mg Zr -> 5 targets x 0.1 mg/cm^2Source quote & editorial note
only 2.3 mg of Zr were consumed in the preparation of 5 targets of 0.1 mg/cm2
Editorial note, tabletop extrapolation: An economy benchmark in the sense of an existence proof - milligrams in, several targets out. For boron or another feedstock, the efficiency is its own measurement (yield, cathode fabrication losses, coated area and recovery all move it); compare candidate routes by measured end-to-end material balance rather than by the Zr anecdote.
-
With adequate care for cleanliness, high-quality RDM targets and stoppers can be produced reliably and easily - the cited conclusion of the Argonne foil-stretcher practice, which draws fragile foils taut over an optically polished reference surface via O-ring compression (the construction, success rates, beam tests and capacitive gap verification are the paper's account - re-read queued).
Source quote & editorial note
with adequate care to ensure cleanliness, high quality RDM targets and stoppers can be produced reliably and easily
Editorial note, tabletop extrapolation: The mounting lesson: flatness comes from a polished reference surface plus elastomer-mediated even tension, with cleanliness setting achievable quality. Capacitance-vs-distance is a fine nonmagnetic gap gauge between conductive, near-parallel, calibrated surfaces - with a vacuum-rated elastomer when used in vacuum.
-
Metallize plastic films gently and in stages: Chalk River's attempts at single-step evaporation to the needed coating thickness ruptured the polypropylene foil through radiant heat damage - staged deposition with cooling pauses was the fix (the stretch-temperature profile, undercoat and per-layer recipe are the paper's process - re-read queued).
stretch 105/115/125 C; CN 10 + Cr 5 (2 steps) + Au 20 ug/cm^2 (3 steps)Source quote & editorial note
Attempts at single step evaporations to these thicknesses were unsuccessful because of rupturing of the foil due to heat damage.
Editorial note, tabletop extrapolation: Stretched polypropylene is a workhorse thin window for gas counters and low-energy vacuum isolation, and the step-and-cool discipline is the transferable method - applied to another polymer as a trial with its own thermal and adhesion checks, not as a universal recipe.
-
Outgas the substrate and dry the finished foil completely — water is the hidden stress agent: McMaster's self-supporting rare-earth targets (Yaraskavitch & Peng) required baking the glass slides at 400 C before depositing the ~25 ug/cm^2 NaCl parting layer (residual moisture caused self-support failure via high film stress) and, after float-off, flushing all water from the mounted foil with methanol drops or pinholes and breakage appeared on drying. Success rate ~80% for 100-300 ug/cm^2 Dy/Er/Gd/Yb.
Source quote & editorial note
any remaining traces of moisture would result in failure to produce a self-supporting target
Editorial note, tabletop extrapolation: Two moisture checkpoints worth evaluating on any float-off evaporation where water-driven stress or breakage shows up: bake the substrate before the parting layer (400 C worked for their glass/NaCl process - check compatibility for other substrates and agents), and displace residual water from the mounted foil with a compatible low-surface-tension rinse (their methanol). Demonstrated for the McMaster rare-earth process; transfer by test, not assumption.
-
Rotate the substrate for uniformity: with the substrate offset r from the source axis and rotating, thickness variation across a 2 cm target falls below 1% at the optimum ratio r/h ~ 0.7 in the cited Behrndt geometry, versus 23% for a static substrate at close range; Maier measured ~1% in practice by Au x-ray fluorescence. Static close-crucible geometry still wins on economy: 186 ug/cm2 collected per mg of evaporant at h = 15 mm.
optimum r/h ~ 0.7; static h=15 mm gives 186 ug/cm^2 per mg but ~23% variation on 10 mm diaSource quote & editorial note
there is a "best ratio" r/h 0.7 which generates a minimum relative thickness variation far below 1% across the target.
Editorial note, tabletop extrapolation: The uniformity-vs-economy trade in one number pair. The r/h ~ 0.7 optimum belongs to that geometry and source distribution - map the deposited thickness for your own fixture rather than copying the ratio. The same volume's GSI stripper-foil paper (rotator tilted 7 deg, 12 rpm) held +-(0.6-1.1)% on plate centers by the same principle - rotation is a cheap, testable upgrade for a bell-jar evaporator.
-
Store hygroscopic and oxidizing targets under vacuum with out-rush protection: Argonne's computer-controlled target store (Nardi & Worthington) keeps 100 targets in a vacuum chamber with transfer under vacuum to the experiment; on recovery from a fault it roughs through a restrictor valve first, specifically to prevent target damage by gas out-rush, and its legacy failure list is instructive — plugged water-cooling pipes, loosening thermocouple connectors, a valve slamming on the transfer rod.
Source quote & editorial note
This prevents target damage by gas out-rush.
Editorial note, tabletop extrapolation: Even a desiccator-scale target store benefits from the transferable habit: throttled first venting/roughing near fragile foils (the source's restrictor-valve recovery). The legacy failure list is instructive where the corresponding hardware exists - IF the store or target uses water cooling, monitor flow and let a hazard assessment decide whether the monitor must interlock beam or heating rather than just alarm.
-
A solid target in a stored (circulating) beam is thickness-capped by heating and thermal runaway: the IUCF Cooler design tolerated only ~1-1.5 ug/cm2 with the beam traversing the target ~1e6 times per second; proposed solid-target routes were grazing the beam edge and fiber/whisker substrates.
stored-beam bookkeeping: crossing rate = N_stored * f_rev, target current = q*N_stored*f_rev - this IS the circulating current (times intercepted fraction); the turn multiplier applies against stored inventory and injection rate, never a second time against circulating currentSource quote & editorial note
thermal runaway would occur and the stored beam would be lost.
Editorial note, tabletop extrapolation: Directly relevant to the synchrotron campaign, not the cyclotrons: compare target heating with the circulating current and intercepted fraction - a nanoamp of circulating current is a nanoamp at the target - and apply the traversal multiplier where it belongs, to how fast the stored inventory or injected charge is consumed.
-
Chemical vapor deposition makes thick refractory films from milligram feedstock (Gallant, Chalk River): dilute H2 + WF6 over a heated susceptor at ~500 C - WF6 + 3H2 -> W + 6HF - gave good tungsten films over 2 mg/cm2; only the susceptor reaches reaction temperature, so very small metal quantities serve. Flagged as nearly absent from target-lab practice at the time.
WF6 + 3H2 -> W + 6HF (susceptor ~500 C; films > 2 mg/cm2); the by-product is hydrofluoric acid gas, not a vague 'fluorine'Source quote & editorial note
very small quantities of metals such as tungsten, tantalum, and molybdenum can be used in miniature systems
Editorial note, tabletop extrapolation: The one route in the volume to thick refractory targets without an e-gun or rolling mill - and an institutional corrosive-gas process, full stop: WF6 is acutely toxic and makes HF on contact with moisture, the exhaust is HF, and the carrier is hydrogen. Compatible closed plumbing, gas cabinets, leak detection, scrubbing and trained operation are the entry fee; Ta and Mo have their own precursor chemistries, not this one with substitutions.
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Durable self-supported oxide targets by cation-loaded cellulose decomposition: Quinby (ORNL) soaked purified carboxy-methyl-cellulose (dialysis-tubing) membrane in a boiling nitrate solution of the element, then decomposed it flat in staged heating (weighted teflon/copper/quartz sandwich under a heat lamp, 230 C oven, then furnace oxidation); films of 100 ug/cm^2 to several mg/cm^2 were strong, near-transparent, weighable, and frame-mountable — cohesion attributed to chemical bonding of cations in the polymer, well below sintering temperatures.
Source quote & editorial note
relatively high strengths and in some cases were virtually transparent.
Editorial note, tabletop extrapolation: A genuinely low-tech thick-oxide route - solution chemistry plus an oven, no vacuum plant - for the metal-cation nitrate systems the source demonstrated (rare earths and similar), where elemental form is not required. Loading adjusts with solution concentration within the membrane's ion-exchange capacity. Boron is NOT a drop-in: borate chemistry doesn't cation-load cellulose the same way, so a boron oxide target needs its own sourced procedure.
-
Actinide-alloy targets for in-beam work were arc-melted into cubic non-paramagnetic host intermetallics and mounted on thick brass holders serving as heat sinks; the Stony Brook fission-isomer team chose the UIr2 host to defeat paramagnetic relaxation, with radiation damage from recoil implantation the other standing obstacle (paraphrase only — journal reprint, no quotation).
Source quote & editorial note
NO QUOTE — paper IV-1 is reprinted from Nucl. Instr. and Meth. 206 (1983) 361-366 with North-Holland permission; finding paraphrased, cite the journal article.
Editorial note, tabletop extrapolation: NOT a tabletop construction example. Actinide targets - arc-melting the alloy, mounting it, putting it in a beam - are licensed radiological-laboratory work: contamination control, shielding, dosimetry, fission-product and activation handling, and radioactive-waste management, on top of the licence itself. Keep this rule as a literature example of matching host-material physics (crystal symmetry, conductivity, heat sinking) to what a measurement needs, and as the rights-boundary marker for this volume; the transferable idea is the matching, never the material. Cite the journal article (Nucl. Instr. and Meth. 206 (1983) 361-366) for the paraphrased finding. [Corrected 2026-08-23: earlier note called this merely "marginal technically" for a proton machine, which understated the hazards that actually decide it.]
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Expect oscillation start-up failure specifically where the dee IS the oscillator tank: the report contrasts machines driven from external oscillators with their own resonant tanks (slight difficulty) against simple-dee-as-tank-circuit systems, which have trouble breaking into full oscillation (the quoted difficulty; the contrast's other half is on the same page - scan re-read queued).
Source quote & editorial note
in cyclotrons using a simple dee system as the tank circuit difficulties are encountered in getting the oscillator to break into full oscillation.
Editorial note, tabletop extrapolation: DIRECT: this names the exact configuration of the reference machine - a simple dee system as the tank circuit - and matches its documented pattern of RF amplifiers failing to bring the dee to voltage. Multipactor loading in the ~100 V band is the report's named mechanism and a testable CANDIDATE cause, not a confirmed diagnosis: the bias and drive-through cures (dg-1274) double as the discriminating experiments.
-
The report's menu for multipactor-band start-up: (1) bias the dee and stem several kV from ground - customary on FM cyclotrons - at the cost of HV-isolating the dee structure; (2) drive the oscillator strongly from an external source so the voltage rises through the ~100 V multipactor region faster than the loading builds (the quoted mechanism); the report's own contribution is the impulse-shock start.
Source quote & editorial note
multipactor loading, which occurs with voltages of the order of a hundred, cannot build up sufficiently to prevent the rise of voltage through the multipactor region.
Editorial note, tabletop extrapolation: The decision menu for any machine that stalls in the multipactor band: bias, drive-through, or impulse shock. On a small machine the driven start maps to an external exciter ahead of the power stage; the bias cure maps to a DC offset on an insulated dee (dg-320, dg-805), with the magnitude found empirically.
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Pick the multipactor cure that does not fight your mechanical architecture: Rochester rejected dee biasing not on physics grounds but because insulating the dee/stem for several kV of DC bias was too awkward on an already complicated variable-frequency (telescoping shorting bar) structure, and built an impulse starter instead.
Source quote & editorial note
The dee biasing scheme was considered too awkward to apply, chiefly because the variable frequency requirement had already led to a rather complicated mechanical design.
Editorial note, tabletop extrapolation: Transferable decision pattern: on a machine whose dee stem is grounded through the tank structure, retrofitting DC bias means rebuilding the stem insulation, so Rochester's choice of an impulse starter is the additive option. Additive is not hazard-free: a shock starter is a high-voltage pulser coupled into an RF vacuum structure and needs a rated feedthrough, insulation and current limiting, grounding, an interlock, and a check for RF coupling and unintended arcs. Compare the two cures by the actual RF/HV insulation and safety design, not by port count. [Corrected 2026-08-23: earlier note said the starter "touches nothing but a spare port".]
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Third multipactor cure - impulse (shock) excitation: a small coupling loop in the dee stem tank, fired by a capacitor discharge through an air spark gap, rings a surge of HF current into the tank; on the cited machine the dee circuit then began oscillating at several hundred volts amplitude and the oscillator carried the voltage up to full value unaided.
kick target: clear the top of the machine's own multipactor band (order-100-V class on the cited machine) - measure the stalled band on the actual resonator; the oscillator does the restSource quote & editorial note
the dee circuit begins to oscillate with a dee voltage amplitude of several hundred volts. The oscillator then begins to carry the voltage on up to its full value.
Editorial note, tabletop extrapolation: One loop, one capacitor, one spark gap, one HV supply - a genuinely cheap cure for a stalled self-excited start. The transferable insight is that the kick need only clear the loading band, not deliver operating power; what that band and required amplitude ARE on a given resonator is a measurement, not an inheritance from the 27-inch.
Cited in: Driving the Dee: RF Coupling
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Sparker circuit values that worked on the cited 27-inch machine: 500 pF charged through 700 kilohm from a 30 kV supply into an air spark gap (~0.22 J per spark), the gap spacing set for roughly two sparks per second - and ordinarily a single spark started the oscillator.
E = C*V^2/2 = 0.5*500e-12*(3e4)^2 ~ 0.22 J per spark; repetition rate is a gap-breakdown setting, not the RC timeSource quote & editorial note
The spark gap is adjusted so that the sparking rate is roughly two per second. Ordinarily a single spark will cause oscillation to commence.
Editorial note, tabletop extrapolation: A sub-joule impulse sufficed on a 27-inch machine; what a smaller system needs follows from its dee capacitance, coupling efficiency and the voltage the kick must reach - calculate or measure it rather than scaling by size. The 30 kV charger is the one nontrivial part, and it must be a properly engineered, current-limited supply with the right polarity and isolation - a bare NST or flyback is a starting component, not the finished charger.
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Interlock an impulse starter so it can only fire when wanted: charging supply energized only while oscillator power is on AND dee voltage is absent, de-energized automatically the moment dee voltage appears — so the operator gets no new control to manage; he presses the normal "on" button, hears a spark if the start hesitated, and the oscillator starts.
Source quote & editorial note
automatically turned on when the oscillator power is on and there is no dee voltage, but which is automatically turned off as soon as dee voltage appears.
Editorial note, tabletop extrapolation: DIRECT automation pattern: gate the starter on (RF enabled) AND (dee pickup below threshold) - a dee voltage pickup is standard monitoring hardware, and where one exists it is exactly the signal needed. The same gate makes stalls detectable: a starter that keeps refiring means the machine is not coming up, so alarm on repeated firings, with the rate threshold chosen at the machine.
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Decouple an auxiliary coupling loop from steady-state operation by geometry: with its plane oriented for minimal flux linkage to the operating mode, the sparker loop saw very small induced RF even at full dee voltage, and sparks during operation caused no perceptible change on the cited machine.
Source quote & editorial note
Because the loop is oriented at right angles to the axis of the cavity, the RF voltage induced in the loop is very small, even with full dee voltage.
Editorial note, tabletop extrapolation: General principle for any starter or diagnostic coupling on a resonator: orient it weakly coupled to the operating mode - remembering reciprocity: a true null for pickup is a null for drive through the same port, so the impulse works through the residual coupling (and other current paths), which is fine because the required kick is small. Verify the coupling both ways, and rate the spark circuitry for the transients it will still see.
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The decay envelope of a ringing dee can map multipactor-band edges: in the cited apparatus, spark-induced dee oscillations fell smoothly until the voltage reached roughly 1/3 of its (few-hundred-volt) maximum, dropped steeply through a loading band, then decayed slowly again below it - consistent with multipactor loading occupying a BOUNDED voltage window, refining mddc-1045 p.12 (discharge exists only below ~500 V extinction) with an observable top edge. The observation bounds the band but does not discriminate between the proposed gap and axial multipactor mechanisms.
sharp-drop onset at ~1/3 of the ringdown maximum; loading band top ~ order 100 V hereSource quote & editorial note
the envelope of the oscillations was found to fall smoothly until the dee voltage had fallen to a value roughly 1/3 its maximum, then for a short time to drop steeply, then afterward to decay slowly once again.
Editorial note, tabletop extrapolation: A free diagnostic worth running: ring the dee (impulse or drive-and-release), scope the pickup envelope through a calibrated divider, and look for a kink - a steep-decay segment is a candidate multipactor band on YOUR machine. Corroborate with pressure and conditioning dependence before labeling it multipactor (other nonlinear losses kink envelopes too), and don't transfer the 1/3 ratio - localize your own band and compare it with the operating voltage.
Cited in: Driving the Dee: RF Coupling
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A shock start did not depend on the oscillator tube's ACTIVE state on the cited machine: dee response to the sparker was unchanged with plate power or filament on or off, while retuning the grid circuit changed the spark-induced amplitude severalfold - the impulse reaches the dee through the passive resonant system, with considerable capacitive current through the (passive) tube.
Source quote & editorial note
Changing the tuning of the grid circuit changed the amplitude of spark-induced dee oscillation severalfold, which seems indicates the flow of considerable capacitative current through the oscillator tube.
Editorial note, tabletop extrapolation: Two consequences, one caution: every branch circuit hanging on the resonator participates in the ring, so commission the starter at the operating tune, not on the bench. And the tube's passive capacitances were part of the tested path - a solid-state driver changes that path AND is far less transient-tolerant, so model the coupling with the PA's output network, isolate or disconnect the devices for first tests, and check transient ratings before calling the method transferred.
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Impulse starting needs a healthy resonator: on the cited machine the sparker loop rang at about 12 Mc regardless of oscillator conditions, decaying 50% in about 3 cycles (effective Q ~ 14) - a fixed, moderately damped ring, with the machine's 10-20 Mc band coupled through whatever overlap and residual paths exist (the pressure/tuning/outgassing failure conditions are the report's operational notes - scan re-read queued).
50% decay in 3 cycles -> Q = 3*pi/ln 2 ~ 13.6; characteristic bandwidth ~ f/Q ~ 0.9 Mc at 12 Mc - not an octave of guaranteed coverageSource quote & editorial note
The ringing frequency of the current in the sparker loop was found to be about 12 mc, independent of the oscillator conditions. The amplitude of ringing is found to decay 50% in about 3 cycles.
Editorial note, tabletop extrapolation: Sets expectations honestly: the shock cures the multipactor stall, not bad vacuum or a detuned feedback network - if a spark fails to start the machine, work the fault list (pressure, tune, outgassing state). Whether one fixed sparker covers a whole tuning range is a startup test at the band edges, not an assumption (trivially satisfied at fixed frequency).
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For an add-on impulse coupler, the cited team chose inductive over capacitive coupling to the dee - partly convenience in a crowded dee chamber, partly expecting less RF-pickup trouble; the energy-transfer efficiency was 'extremely small' and still adequate, with tighter coupling available as an upgrade they never needed.
Source quote & editorial note
partly because it was more convenient in our case since the dee chamber is rather crowded, and partly because we thought that the RF pickup problem would cause less trouble with inductive coupling.
Editorial note, tabletop extrapolation: A useful trade note, not a theorem: in a small chamber where every square inch near the dee is contested, try a loop near the dee stem (outside the beam region) first - then MEASURE steady-state pickup and impulse coupling before fixing the location; whether inductive actually beats capacitive depends on the local field geometry and the mode.
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A passive magnetic mirror from a 1/8-in steel bearing ball at the top of the arc hood reflects electrons streaming up the arc channel (mirror cone sin^2(theta_c) = B0/Bmax): before the ball the graphite hood top glowed bright orange from electron bombardment; after, it stayed black - taken by the authors as evidence of strong mirror action, converting the hooded-arc source toward reflex operation in the cyclotron's own field.
sin^2(theta_c) = B0/Bmax (electrons outside the cone reflect; Spitzer 1956)Source quote & editorial note
a magnetic mirror built into the upper end of the arc hood by the simple insertion of a steel bearing ball 1/8 in in diameter. ... Before the steel ball was added the top of the graphite hood glowed a bright orange color when the arc was operating, because of the intense electron bombardment. After the ball had been added the top of the hood was found to remain black when the arc was operating. This result is taken as evidence of a strong mirror action.
Editorial note, tabletop extrapolation: Nearly free to TRY on a filament hooded source running in the main field - a bearing ball is stock hardware and the hood exists - but not automatic: whether electrons reflect depends on Bmax/B0 at the ball, injection pitch angles and collisions, so replicate the source's own A/B glow test (hood-top color/temperature with and without the ball) and check the companion negative result (dg-1288) before counting on it.
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Read where arc electrons land from incandescence: the graphite hood top glowed bright orange during arc operation, attributed to intense electron bombardment - a viewport diagnostic of where the arc's power is going.
Source quote & editorial note
the top of the graphite hood glowed a bright orange color when the arc was operating, because of the intense electron bombardment.
Editorial note, tabletop extrapolation: A diagnostic that costs a glance, used as a controlled A/B: at fixed arc power, cooling, surface state and sightline, an orange chimney-top says axial electron loss is real, and a change after adding a mirror or repeller says the geometry change did something. A black hood alone proves less - lower power, emissivity and sightline all dim the glow - so pair the glance with beam and arc-current numbers.
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Reflex electron economy: with electrons presumably oscillating - reflected by the magnetic mirror above and electrostatic repulsion from the filament structure below - the arc current required for a satisfactory hydrogen ion current fell severalfold in the cited source.
Source quote & editorial note
The arc current required to produce a satisfactory current of hydrogen ions has been reduced severalfold, presumably because the electrons oscillate, being reflected by the magnetic mirror at the top and by electrical repulsion from the filament structure below.
Editorial note, tabletop extrapolation: The physics argument for reflex geometry at small scale: multiple-pass ionization, bought here with one filament and a mirror instead of a PIG's two cathodes. Measure ion yield versus arc current on the actual geometry - the severalfold factor and its knock-ons (filament drive, heat, gas decomposition are separate quantities from arc current) are things the source's own 'presumably' invites you to verify, not inherit.
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Filament life responded dramatically in the cited source: typical lifetimes had ranged 15-30 hours; the first filament in the new (reflex) source was intact, though thin, at removal after 109 hours - one censored observation, encouraging rather than statistical.
lifetime 15-30 h at full emission -> >109 h severalfold-reduced emission (same 60 mil W hairpin)Source quote & editorial note
Typical lifetimes of filaments had ranged from 15 to 30 hours. The first filament installed in the new source was intact, though thin, when removed after 109 hours of operation.
Editorial note, tabletop extrapolation: Directly relevant to the standing filament-maintenance complaint: electron economy is a candidate filament-lifetime fix, since tungsten evaporation is brutally steep in temperature - so any arc current not needed pays back in hours. Establish the actual gain with controlled heater settings and more than one run-to-failure; a single intact-at-109-h filament sets hope, not a multiplier.
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Mirror-assisted source behavior is geometry-sensitive and was not understood even by its inventors: the same steel-ball mirror in a second hooded source was 'in this case unsuccessful' - the obvious difference being the hairpin filament's plane parallel to the cyclotron field instead of perpendicular. Test the trick on your geometry; do not assume transfer.
Source quote & editorial note
in this case unsuccessful ... also a hairpin-shaped 60 mil tungsten wire, is mounted with its plane vertical, parallel to the magnetic field of the cyclotron, rather than perpendicular as in the first source.
Editorial note, tabletop extrapolation: An honest negative result from 1961 that still stands. The filament-orientation reading (injection angle into the mirror deciding loss-cone membership) is a HYPOTHESIS consistent with the one observed difference - local electric fields and emission distribution matter too - so plan the mirror experiment as an A/B test with the glow diagnostic and vary filament orientation if the first try fails.
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Shrink the hood extraction opening to cut source gas flow into the tank: the source reports lower tank pressure partly from reducing the hood opening to about 1/32 in - but expect the slit to erode: within days it had enlarged in the direction of ion rotation. Slit wear is a consumable-maintenance item; inspect and re-measure it.
hood opening ~1/32" x 3/16" (0.8 x 4.8 mm) for H/D; helium source used ~1/8" x 3/8"Source quote & editorial note
The gas pressure in the cyclotron tank is lower. This came about partly because the opening in the hood (through which the ions to be accelerated are [extracted]) ... reduced in size to about 1/32 in ... after a few days of operation, it was found to have become somewhat enlarged in the direction of ion rotation.
Editorial note, tabletop extrapolation: Two lessons: (a) the chimney slit is the gas throttle, and sizing it down is a cheap pumping win - balanced against plasma and beam extraction, so optimize rather than minimize; (b) the asymmetric erosion (along rotation) is a clue about where early-turn ions strike the hood - corroborate with tracking or witness marks before reading it as a diagnostic.
Cited in: The Vacuum Budget of a Cyclotron
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Hooded-arc operating envelope on the 27-inch (7-14 kG): arc currents to 2 A and voltages to 250 V were used, but deuterium ran on about 0.75 A at about 100 V - roughly 75 W of arc - and pushing arc current from 1.0 to 2.0 A bought only a relatively small beam increase. (The species is a handwritten correction over typed 'hydrogen' on the page.)
deuterium point: ~0.75 A x ~100 V ~ 75 W; 1 -> 2 A arc gave only a relatively small beam gain; B = 7-14 kGSource quote & editorial note
Arc currents up to 2 amperes and arc voltages up to 250 have been used. For deuterium operation a current of about 0.75 amperes and a voltage of about 100 are usually sufficient.
Editorial note, tabletop extrapolation: Concrete supply-sizing anchor: sub-100-W arcs fed a 27-inch machine's beam. The operating doctrine is diminishing returns - find the knee of the yield curve on your own source and park below it, since past the knee extra arc current buys mostly filament wear and gas load.
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Optimize the source per species rather than forcing one design: the H/D mirror source gave only ~1/10 the beam of the dedicated helium source - itself hooded, with a tantalum button on quartz tubing atop a tantalum-tubing hood and a larger ~1/8 x 3/8 in opening.
Source quote & editorial note
Cyclotron beam currents were found to be of the order of 1/10 those obtained with our standard helium ion source, which is also of the hooded type, having a tantalum button supported by a short piece of quartz tubing at the upper end of a tantalum tubing hood. For these tests a hood with a larger hole, about 1/8 in x 3/8 in was used.
Editorial note, tabletop extrapolation: A scoping warning for any future gas change: a source tuned for hydrogen is not a universal source - the tenfold gap is one uncontrolled comparison, so let measurements on the actual gas assign causes. The tantalum-button-on-quartz sketch is this collection's only helium-specific hooded-source construction, useful if alphas are ever on the menu.
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Keep the magnet gap well under the orbit radius wherever the field must be shimmed to a prescribed shape: the source calls proper shimming impractical when gap length is 'much greater than one-half the radius' - a soft boundary, not a cliff at rho/2.
l_gap <= ~rho/2 for shimmable fieldSource quote & editorial note
The properties of a magnetic field in space make it impractical to obtain a properly shimmed field if the gap length is much greater than one-half the radius p.
Editorial note, tabletop extrapolation: An 8-12 in. pole with a 1-2 in. gap sits far inside this limit, which is why small cyclotron shims work at all; the rule bites for any short-radius bending/analysis magnet where a generous gap is tempting for access.
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Derive the allowable field gradient from the allowable bowing of the flux lines: for a current-free, symmetric gap with small deflection, a line bowing x over half-gap h obeys x = (h^2/2)(1/H)(dH/dx); Powell's worked case - 0.5 mm allowable bow, h = 125 mm - gives a maximum edge-ward gradient of 0.16 percent per inch.
x = (h^2/2) * (1/H) * (dH/dx); calutron limit 0.0016/inSource quote & editorial note
is the maximum allowable space rate of change of the magnetic field in a direction toward the edge of a gap.
Editorial note, tabletop extrapolation: The transferable move: translate a beam-geometry tolerance into a measurable dH/dx budget via the curl-free midplane relation - a quick LOCAL gradient check to run on a field map when flux-line bowing is the relevant tolerance. It is a calutron criterion, not a cyclotron field-quality spec: orbit, focusing, flutter and resonance checks still decide.
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First-pass excitation: NI = 2.02 x H(gauss) x gap(inches) for the air gap alone; in well-proportioned iron-return magnets the gap consumes 85-95 per cent of the total mmf, so take total NI ~ 1.15 x (NI)_gap as the starting approximation and let the model (or simulation) refine it.
(NI)_g = 2.02 * H[G] * l_g[in]; NI_total ~ 1.15 * (NI)_gSource quote & editorial note
the quantity (NI)g represents 85 to 95 per cent of the total mmf required (i.e., the efficiency ranges from 85 to 95 per cent), and Eq. 7 can be used to give a useful first approximation
Editorial note, tabletop extrapolation: The same arithmetic every H-frame designer runs today (Wouters and Zickler's CAS notes corroborate the sizing). The 85-95% efficiency band is the source's result for WELL-PROPORTIONED iron-return magnets: use it as a sanity check on FEMM excitation for a magnet in that class, and expect worse from lean yokes, corners, or parasitic joint gaps (dg-128).
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The product of coil power and conductor weight is a design invariant set by ampere-turns and coil size: P x W_c = 0.118 x (NI/10^5)^2 x (mean turn length, in.)^2 for copper (0.131 for silver, 40 C mean). Choose the P/W_c split afterwards from cooling or cost — it fixes current density via J[A/in^2] = 486 x sqrt(kW/ton) for Cu.
P[kW] * W_c[tons] = 0.118 * (NI/1e6)^2 * (mean turn length, in.)^2 for copper (0.131 silver, 40 C mean) - the 0.118 rides with MEGA-ampere-turns squared and length squared (cf. dg-212); J = 486*sqrt(P/W_c)Source quote & editorial note
the product of the power and weight of a coil conductor depends on the ampere turns and the mean diameter of the coil.
Editorial note, tabletop extrapolation: The cleanest statement in this collection of the copper-vs-power trade: double the copper, halve the dissipation, at fixed NI. Lets a coil be resized on one line when a surplus supply or a heat limit is the binding constraint.
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Continuous-duty current-density ceilings from calutron practice: ~1600 A/in^2 (2.5 A/mm^2) is the upper limit for oil-cooled coils, ~1000 A/in^2 (1.55 A/mm^2) for open bus bar in free convection; the project's economic balance point P/W_c ~ 5 corresponded to ~1050 A/in^2. Careful cooling design is what buys anything higher.
J_max ~ 1600 A/in^2 oil-cooled continuous; ~1000 A/in^2 free-convection busSource quote & editorial note
For continuous operation, 1600 amp/sq in. is about the upper limit used for oil-cooled coils. This compares with 1000 amp/ sq in. for open bus bars cooled by free convection
Editorial note, tabletop extrapolation: Brackets modern air-cooled small-magnet guidance from the 1940s operating side - mapped to the right geometry: the 2.5 A/mm^2 was for OIL-cooled calutron coils, and the 1.55 A/mm^2 for open bus bar with free-convection area a wound coil does not have. A passively cooled wound tabletop coil therefore belongs below both, in the ~1 A/mm^2 territory of the coil rules (dg-092), unless its own thermal test justifies more.
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Coil space factor (copper volume over coil-container volume) came out 0.37 and 0.30 on two experimental models forced to use available conductor sizes rather than purpose-designed ones - the quote; the report's expectation for designed conductor is its surrounding discussion (scan re-read queued).
space factor ~ 0.5 designed; 0.30-0.37 with off-the-shelf conductorSource quote & editorial note
Two experimental models had values of 0.37 and 0.30, but in both cases it was necessary to use conductor sizes which were available but not specifically designed for the job.
Editorial note, tabletop extrapolation: Amateur coils are usually wound from whatever magnet wire is available: budget a pessimistic 0.3-0.4 space factor when sizing the coil window, and read handbook ~0.5 figures as purpose-designed-conductor numbers.
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Magnet cost scales roughly linearly with beam radius at fixed Hrho: with gap length proportional to rho and H proportional to 1/rho, both power and copper weight scale ~rho and steel weight scales as rho^n with 1 < n < 2. Powell: choose radius on beam physics, not on magnet cost, because cost climbs only proportionately.
P ~ rho; W_c ~ rho; W_steel ~ rho^n, 1<n<2 (at fixed H*rho)Source quote & editorial note
both the first cost and the power cost of a magnet increase almost proportionately with an increase in beam radius.
Editorial note, tabletop extrapolation: Useful scaling honesty for any pole-diameter trade study — going from 8 to 13 in. poles at fixed final energy is a near-linear cost move, not a quadratic one, so long as the field comes down as the radius goes up.
Cited in: Choosing Your Machine
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Budget for the sideways force that tries to INCREASE pole area, not just the attraction across the gap: any split through a pole (segmented poles, bolted pole caps, diametral joints) sees a spreading force; each half of a diametrally split circular pole is pushed sideways with (1/2)(H^2*l*a/8pi), l = gap length, a = pole diameter.
F_spread(each half) = 0.5 * H^2 * l * a / (8*pi) [cgs]Source quote & editorial note
The forces tending to separate the halves are surprisingly large and if overlooked can be disastrous.
Editorial note, tabletop extrapolation: Directly relevant to removable pole caps and bolt-on shim plates on a small H-frame: check the retention for lateral load wherever the joint geometry can see one - splits with a component parallel to the flux see spreading, while a complete cap on a plane parallel to the pole face mainly sees the axial pull. The formula is the diametral-split case, not every joint's.
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Working force formulas from the report's engineering pages (English units): pull between pole faces F[lb] = (kG)^2 x area[in^2] / 1.735 (the quoted line); its companion values give conductor force F[lb] = kG x amp x length[in] / 1750 and a copper strip hot-spot check dT[C] = 0.0094e-6 x width^2 x J^2.
F_pole[lb]=kG^2*A[in^2]/1.735; F_cond[lb]=kG*I*l[in]/1750; dT_Cu=0.0094e-6*w^2*J^2Source quote & editorial note
Force between pole faces (lb) = 1/1.735 X (kilogauss)^2 X area (sq in.)
Editorial note, tabletop extrapolation: The 1.735 pole-force constant is the imperial twin of B^2/2mu0 and matches it to 1%; the hot-spot width formula is a one-line check before winding wide flat strip on a driver-amplifier-fed coil.
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Keep the driving coils as close to the air gaps as possible - the quoted reason: less spreading and bowing of the field, and the largest usable fraction of gap area; the report's design discussion builds its order of operations around this (gap, field and uniformity first, then iron topology - full sequence: scan re-read queued).
Source quote & editorial note
it is desirable to keep the driving coils as close to the air gaps as possible in order to reduce spreading and bowing of the field and to keep the largest possible fraction of the gap area usable.
Editorial note, tabletop extrapolation: Coils-near-gap is the reason cyclotron coils hug the poles rather than the yoke; the usable-fraction-of-pole-area argument is exactly the good-field-radius economics of a small machine.
Cited in: Choosing Your Machine
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For absolute field intensity with an induction coil, the source accepts only full 180-degree flips: the flipped flux change is 2*B*A_eff at a true reversal (times cos(theta) for endpoint misalignment theta, so alignment is part of the measurement); partial throws serve relative and bucking work.
delta-phi(180-deg flip) = 2*B*A_eff*cos(theta); = 2*B*A_eff for aligned endpoints in a uniform fieldSource quote & editorial note
In accurate determinations of the absolute magnetic field intensity, only angular throws of 180 deg are considered satisfactory.
Editorial note, tabletop extrapolation: The flip coil remains the cheapest absolute cross-check on a Hall probe - an NMR-free lab can tie its Hall calibration to a geometry-defined coil area plus a CALIBRATED integrator, provided the flip is a true reversal with aligned endpoints.
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Calibrate deflection instruments by bracketing, not by assuming linearity: interleave flux-standard deflections with the unknown and interpolate. Linearity of a ballistic galvanometer holds only to ~1 per cent when the standard deflection is about half the unknown (damping changes with amplitude); bracketing recovers 0.5 per cent field accuracy. Keep circuit resistance identical between calibration and measurement — sensitivity depends on R.
bracket unknown between standard deflections; hold R_circuit constantSource quote & editorial note
Field measurements may be made to 0.5 per cent accuracy by bracketing the deflections to be interpreted with deflections from the flux standard and then interpolating.
Editorial note, tabletop extrapolation: The transferable method: calibrate at deflections spanning the readings, through the same signal path, rather than trusting one scale factor. For a modern ADC/integrator mapper that means multi-point calibration across the operating range; matched input impedance matters where source loading affects the transfer - check it rather than assuming either way. The 0.5% is the cited galvanometer arrangement's result.
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Build the calibration chain on geometry: a single-layer coil wound on an accurately machined cylinder has effective area pi*D^2*N/4 good to at least 0.1 per cent when the wire diameter is small against the cylinder diameter - verified in the source's practice (the comparison methods for transferring to working coils are the report's procedures - re-read queued).
A_eff = pi*D^2*N/4 (single layer; D center-of-wire to center-of-wire; wire << cylinder)Source quote & editorial note
As verified by practice, Eq. 68 holds true to at least 0.1 per cent accuracy when the diameter of the wire is small compared to the diameter of the cylinder.
Editorial note, tabletop extrapolation: The piece that turns a flip coil from a relative into an absolute instrument - a machined-spool area standard any shop can make. What absolute field accuracy the whole home chain achieves is its own uncertainty budget (machining, winding, temperature, alignment, field nonuniformity, integrator) - build the budget, then claim the number it supports.
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Expect ~0.35 per cent from a well-run secondary flux standard: calibrating against a standard mutual inductance (phi = 10^5*M*i) carries the RSS of the mutual-inductance calibration (~0.25%) and deflection matching (~0.25%) — and the error formula prediction was verified in practice. Treat sub-0.1% claims from simple induction chains with suspicion.
phi[line-turns] = 1e5 * M[mH] * i[A]; X = sqrt(X1^2 + X2^2) ~ 0.35%Source quote & editorial note
The value of X is 0.35 per cent, which is verified in practice.
Editorial note, tabletop extrapolation: The cited chain's honest arithmetic - two ~0.25% terms RSS to ~0.35%, verified in practice - models how to audit any simple coil-and-integrator chain: enumerate the terms, RSS them, and treat any claim that beats the budget (sub-0.1% included) as unproven until its own budget shows the terms. A traceably calibrated chain can do better; a Hall probe certified to 0.1% is only better in a non-uniform cyclotron gap once its temperature, angle and positioning terms are in the budget too. Compare the two by a full uncertainty budget, not by the certificate. [Note revised 2026-08-23: earlier note made the 0.35% a general floor and the Hall probe 'genuinely better'.]
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When the magnet supply is unregulated, make uniformity measurements differential: fix a bucking coil in the field, series-oppose it with the moving search coil, and trim until excitation on/off gives zero net deflection. Supply drift then enters only the measured field DIFFERENCES - the source: a 1 percent current change costs 1 percent of the (small) nonuniformity, ~1e-4 of the field for a 1 percent contour.
series-bucked pair; error ~ (dI/I) x (delta-H/H), not (dI/I)Source quote & editorial note
A 1 per cent change in the exciting current produces an error of only 1 per cent in the changes in the magnetic field.
Editorial note, tabletop extrapolation: The classical answer to shimming with a wandering surplus supply: map relative structure differentially, pin the absolute scale with occasional flips. The cancellation assumes both coils see a common, effectively linear B(I) - check the local dB/dI, saturation and hysteresis on an iron magnet first. A two-channel Hall differential inherits the immunity only with simultaneous sampling and matched, temperature-stable channels.
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Match the probe to the field structure and the placement to the requirement: the model survey needed field position known to 1/32 in on the models (0.5 in full scale), and the survey coils were built small (0.20 in dia x 0.15 in high, ~350 turn-cm2) - two different error terms: coil PLACEMENT accuracy, and the area-averaging any finite coil performs.
the measured value = true field convolved with the probe's active-area response; placement error and averaging error enter the budget separatelySource quote & editorial note
It was desirable to know the magnetic field accurately to within 0.5 in. on the full-scale magnet. This corresponded to 1/32 in. on the models.
Editorial note, tabletop extrapolation: For Hall-mapping a shim edge: the sensor's active area averages across the gradient, so where the gradient scale approaches the sensor size, either model the convolution or verify with a smaller probe; jig position repeatability sits in the same budget as its own line. Neither substitutes for the other.
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In drift-limited flux integration, LOW sensitivity wins: a many-turn search coil driving a low-sensitivity fluxmeter beats a few-turn coil on a sensitive one — same signal, but drift from thermal/contact emf scales with instrument sensitivity, and lead/contact resistance and stray loop area matter less. Drift, not gain, is the enemy; check and re-zero it continuously through a run.
drift rate (const emf) ~ 1/G ~ sensitivity; signal fixed by n_coil scalingSource quote & editorial note
Since drift is the most troublesome feature of a fluxmeter, the advantages of the low-sensitivity fluxmeter far outweigh those of the high-sensitivy fluxmeters for accurate, reliable measurements.
Editorial note, tabletop extrapolation: Maps onto modern integrator front-ends as a conditional: putting gain in the coil (turns) and keeping electronics gain low reduces the relative weight of input-referred offset drift - but turns also add resistance, inductance and capacitance (noise, settling, bandwidth), so optimize the coil rather than maximizing it, measure the actual input-referred drift, and treat offset/zero checks as part of every run.
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Two low-tech field-shape tools from the calutron plant: iron filings map stray-field direction - with slightly magnetic stainless filings arranging themselves along the lines of force without accumulation near sharp corners - printable directly onto blueprint paper for a permanent record; and a mercury-arc discharge tube aligned with the field collapses its glow onto the field line, readable with a cathetometer.
Source quote & editorial note
stainless-steel filings (being slightly magnetic) sprinkled in this area will arrange themselves along the lines of force without accumulation.
Editorial note, tabletop extrapolation: Historical techniques worth knowing, deployed with modern care: filings near a strong magnet accelerate and infiltrate - use them sealed in a flat transparent container, never near open vacuum hardware or the pole gap; the discharge-tube method needs a sealed commercial tube plus mercury/UV/HV precautions, and the machine's own ion source is not a movable substitute for it. As qualitative first looks before a probe survey, both still earn their keep.
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Turn beam-physics tolerances into go/no-go field acceptance tests before measuring: the calutron plant's integral criterion required measured and theoretical INTEGRAL h_z dx along the beam arc to agree within 3 cm of galvanometer deflection - field quality became a pass/fail reading, not a judgment call (the coil count, template gradients and mass-unit objective are the report's surrounding practice - scan re-read queued).
acceptance = |integral h_z dx (meas) - (theory)| < deflection criterion; gradient templates 0.2%/in and 0.1%/inSource quote & editorial note
it was necessary for the values of the quantity integral h_z dx, experimental and theoretical, to differ by less than 3 cm, in terms of galvanometer deflection.
Editorial note, tabletop extrapolation: The discipline transfers: derive numeric field-map acceptance bands from the orbit tolerance (phase-slip or centering budget) BEFORE surveying, so the survey ends in pass/fail per region. Use integral criteria where the beam observable demonstrably depends on the integral, and keep pointwise limits where local gradients, resonances or extraction physics bite - both kinds of band, each where it belongs.
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The model-magnet scaling law: a linear scale model built from steel with the same magnetic properties, operated at the same field strength (same B everywhere, currents scaled to keep NI per gap-length), reproduces the prototype's field distribution exactly — magnetostatics has no intrinsic length scale until saturation properties differ. Leakage coefficients measured on the model apply directly to the full-scale magnet; forces follow with area (L^2) scaling.
geometric scaling at fixed B and fixed material B-H curve; L_leakage(model) = L_leakage(full scale)Source quote & editorial note
a linear scale model built from steel with the same magnetic properties as planned for the prototype magnet and operated at the same field strength will give results directly applicable to the prototype.
Editorial note, tabletop extrapolation: The physics that lets FEMM stand where models stood — and the terms of validity are the same for both: correct B-H data and correct geometry. Any cheap sub-scale mock-up of a planned magnet obeys it too, provided the steel matches and B is held, not NI.
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Match model scale to question precision: the team judged the 1/8-scale model's results inherently more accurate than the 1/16-scale's, and reserved it for where that accuracy mattered (which questions each model answered is the report's program history - re-read queued).
Source quote & editorial note
since the X Beta model was built to 1/8 scale it seemed true that the results would be more accurate than those which could be obtained on a 1/16-scale model.
Editorial note, tabletop extrapolation: The mesh-refinement decision in physical form: coarse resolution for excitation, force and leakage questions; fine resolution only for the finest field-uniformity region - spending fine-model effort on questions the coarse model already answers is waste in either medium. Accuracy also rides on geometric similarity, material scaling and construction error, not scale alone.
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The calutron model-test suite, as quoted: a magnetization curve, gap-to-gap performance comparison, uniformity contour maps, magnetic-force determination, and flux density through the various iron members - the historical characterization a predictive model owed the design.
report H_g(NI/l_g), eta(NI/l_g), L(x), (H-Hg)/Hg contour map, stray mapSource quote & editorial note
The usual measurements made included a magnetization curve, a comparison of gap performance at different points in the magnet, uniformity contour maps, determination of magnetic forces, the density of flux through various parts of the magnet
Editorial note, tabletop extrapolation: A ready-made deliverables checklist for a FEMM campaign on a new magnet: produce the quoted five (B-H behavior, gap comparisons, uniformity contours, forces, member-by-member flux audit) and add the modern staples - efficiency and leakage accounting and a stray-field map - as the extended set; the point is a defined deliverables list agreed before the runs, not after.
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Track efficiency (gap mmf / total mmf) at TWO field levels as a saturation health check: the revised Alpha II model measured 95.4 +/- 2.0 per cent at 3400 Oe, equal within error to its higher-field value - which the report read as the design being rather conservative; falling efficiency with rising field is the first GLOBAL symptom of a saturating member.
eta = 2.02*H_avg[G]*l_gap[in]/(NI); compare at two excitations - equality shows no detectable aggregate reluctance rise over the tested rangeSource quote & editorial note
With 3400 oersteds in the gaps the efficiency obtained was 95.4 +/- 2.0 per cent. Within experimental error they were the same at both field strengths. This indicates that the magnet design is rather conservative.
Editorial note, tabletop extrapolation: A two-point excitation scan (measured B vs I against the linear NI prediction) is the coarse global check on an H-frame - it flags that saturation is happening somewhere, not where: localizing the saturating member takes FEM or local flux measurements. Local saturation can also hide inside an unchanged global efficiency, so treat a clean two-point result as necessary, not sufficient.
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Audit the flux through EVERY iron member - the report's ballistic-loop method: wound loops read by a ballistic integrator, with loop-flux differences over enclosed-area differences giving local leakage components; the quoted judgment is that 10-15 kilogauss in the yokes gave good flux density without excessive permeability drop.
B_member = (phi_loop difference)/(A_steel); leakage component = d-phi/d-A between loop pairsSource quote & editorial note
In the neighborhood of 10,000 to 15,000 gauss the flux density is good, yet the yokes are not overloaded to the extent that the permeability of the steel drops excessively.
Editorial note, tabletop extrapolation: The 10-15 kG working band for structural mild steel is the same number modern small-magnet guidance gives (cf. Wouters; Zickler CAS) — and the loop-audit method is the measurement twin of integrating B over member cross-sections in a FEMM postprocessor: every member gets a number, every number gets a verdict.
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Saturation red-line by permeability, with a material margin: at 17,200 G the model core steel had mu ~ 150, and the (magnetically poorer) full-scale steel would drop to mu ~ 118 — "dangerously low," possibly worse in local regions; the fix was 24 per cent more iron to bring the core to ~14,000 G. Judge margins on the PROTOTYPE material's B-H curve, at the worst local induction, not the average.
keep working mu >> 100; core fix sized to reach ~14 kGSource quote & editorial note
the corresponding permeability would drop to 118, which is dangerously low. In certain localized regions it might even be lower.
Editorial note, tabletop extrapolation: A quantitative 'too far' AS THAT PROJECT JUDGED IT: mu ~ 100-150 at the working point was their failure territory, fixed by 24% more iron. What a given magnet tolerates depends on its mmf budget and field-quality needs; the transferable instruction is auditing against the ACTUAL steel's B-H curve - the same reason a FEMM model of an H-frame is only as good as the B-H table fed to it.
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Correct model predictions for known model/prototype differences, with signs stated: the team measured the permeability of BOTH steels and noted the full-scale material's was higher - so slightly better full-scale performance could be expected (the geometry-difference tallies are the report's accounting - re-read queued).
Source quote & editorial note
The permeability of the material of the full-scale unit is higher than that of the model. This indicates that a slightly better performance could be expected from the full-scale unit than from the model.
Editorial note, tabletop extrapolation: The sign-audit habit transfers to simulation directly: list every model-vs-hardware difference (B-H table provenance, fillets, packing factor, joint gaps) with the direction it biases the prediction, so measured-vs-predicted discrepancies arrive pre-explained - direction-audited, which is weaker than bounded: a bound needs magnitudes for every term, not just signs.
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Find end-cell compensation empirically: end coils adjacent to a yoke nominally need 50 per cent of a full coil, but yoke reluctance leaves the end gaps low - Alpha II measured 4.0 per cent low at the 50% setting, and practice converged on higher end-coil ratios settled by measurement, so BUILD IN TAPS (the intermediate measurements and other machines' ratios are the report's data - scan re-read queued).
measure end-gap deficit at two end-coil turn ratios; extrapolate linearly to zero deficitSource quote & editorial note
It was found that when the number of turns on the end coils was 50 per cent of a full coil, the field in tanks adjacent to the yokes was 4.0 per cent low.
Editorial note, tabletop extrapolation: The pattern transfers to any edge-compensation knob - outer-radius shim thickness, trim turns near a yoke window, correction-coil ampere-turns: measure the deficit at two settings, extrapolate linearly to zero as the FIRST estimate, then confirm with a third measurement - saturation and coupling bend the response, so one iteration is the hope, not the promise.
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If flux leaves the pole structure at higher density than the gap average, spread it before it crosses any tolerance gap: Alpha II's cellular core emitted flux at twice the average density, and a steel faceplate over the core face spread the flux evenly before it crossed the gap (full-scale analog: stacked core inserts forming a continuous plane).
parasitic-gap mmf scales LINEARLY with local B (~B*g/mu0); magnetic pressure scales as B^2/(2*mu0) - flux at 2x density over half the area doubles the integrated force and quadruples the local pressure; the faceplate must itself stay below saturationSource quote & editorial note
a steel faceplate was placed over the face of the core, as shown in Fig. 3.14, to spread out the flux evenly before it crossed the gap.
Editorial note, tabletop extrapolation: The reason laminated or relieved pole structures carry a continuous pole face; applies to any lightening-hole or bolt-pattern pole cap on a small magnet - size the face sheet against saturation (thickness x permeability doing real work), don't just add a modest skin.
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Convert the model into a force ledger before detailing structure - the report's Alpha II ledger combines magnetic wall pressures with atmospheric loads per wall; the quoted method point: forces computed from the average field over a region UNDERSTATE the true force, so use the mean of the squares.
F ~ integral H^2 dA (use mean of squares); tabulate per-member envelope with marginSource quote & editorial note
the forces calculated on the basis of the average over the entire region will be lower than the true force.
Editorial note, tabletop extrapolation: On a tabletop the same ledger is short but identical in kind — gap pull, atmospheric load on the chamber, unbalanced pull on any asymmetric iron — and the mean-of-squares point matters wherever the field is nonuniform over the loaded area (pole edges, shim steps).
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Gap-spacing tolerance for field quality between a pole structure and an inserted wall (calutron criterion): keep the separation large enough that the maximum separation never exceeds twice the minimum - fractional tolerance on a parasitic gap, not absolute flatness, is what the field cares about.
s_max <= 2*s_min; for symmetric variation about a nominal s0 this means |delta| <= s0/3 (about +/-33%, NOT +/-50%)Source quote & editorial note
the space between the tank and the cores must be great enough so that the maximum separation is never more than twice the minimum separation.
Editorial note, tabletop extrapolation: Useful thinking for a shim pack, pole-cap seat, or chamber-lid-under-pole arrangement: a deliberately larger uniform standoff can pass where a tiny irregular one cannot - at the price of added reluctance (more ampere-turns for the same field), so treat enlarging the gap as a trade to compute, and validate the 2:1 criterion's adequacy for the new geometry rather than assuming the calutron number.
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The calutron model program's validation verdict — the benchmark for trusting scaled prediction: full-scale tests confirmed the 1/16-scale models as "dependable and accurate," with full-scale performance slightly BETTER than predicted (source-region field more uniform than model results, stray field weaker, track efficiency ~94% vs 95.6 +/- 2% model, core-to-tank field concentration 18% vs model 22%); 71 of 71 production tanks met the theoretical field criteria, worst case 2.8 cm against a 3.0 cm limit.
Source quote & editorial note
The magnetic performance of the track is better than predicted from the model experiment.
Editorial note, tabletop extrapolation: The historical calibration point for a predict-then-verify magnet pipeline: one faithful same-steel scaled-model campaign landed close on global quantities and erred conservative because the prototype's iron out-performed the model's. One campaign is precedent for the METHOD - predict, then verify at full scale - not an accuracy guarantee for models or FEM in general: each pipeline earns its own error bars (dg-080's 3% benchmark, dg-817's first-beam case).
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After the first article validates the prediction chain, acceptance testing can degrade to mechanical metrology - for replicas: track 1's testing showed a dimensional check of the shim positions entirely adequate for the following production, with magnetic checks reserved for special questions.
Source quote & editorial note
the excellent results obtained in testing track 1 showed that a dimensional check of the shim positions was entirely adequate.
Editorial note, tabletop extrapolation: The economic payoff of validation, with its boundary drawn correctly: dimensional-only acceptance covers exact replicas made under the same materials, tooling and process - a CHANGED shim geometry is a new magnetic configuration and gets its own field map. In one-off tabletop practice, that means the caliper substitutes for the gaussmeter only when re-making the same part, never when revising it; keep periodic magnetic audits regardless.
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Expect field CORRECTION to be trial and error, and budget for it: this team's theoretically grounded shim-tilt correction scheme failed validation (predicted and measured tilt effects disagreed near the tilted shim - partly because a theory assumption, iron stuffing behind the tilted shim, was not implemented in hardware), and they concluded the only feasible correction method was iterative cut-and-try.
Source quote & editorial note
It would appear that the only feasible method of making corrections when the necessity arises is by trial and error.
Editorial note, tabletop extrapolation: A 1944 warning that survives every FEMM run: analysis predicts changes to an as-built field only if the change is modeled as executed - and even then B-H uncertainty, hysteresis, stress and omitted 3-D features can dominate. Plan shimming as measure-cut-measure iterations with FEM as the starting estimate, and keep shim stock adjustable.
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Members held in place by field symmetry are in unstable equilibrium - anchor them: plant tanks crept as much as 2.5 inches out of their gaps over days of energized operation, and the report's analysis treats the ejection force by reluctance-minimization energy accounting (their computed force bracket: scan re-read queued).
F = d/dx [ (H^2/8pi) * V_field(x) ] ; force increases with displacement from symmetrySource quote & editorial note
a check on the positions of the tanks in this quadrant showed that some of them had moved as much as 2.5 in. out of the gaps.
Editorial note, tabletop extrapolation: Anything ferromagnetic sitting in or near the gap on nominal-symmetry grounds - chamber, probe carriages, shim plates, tools - needs positive mechanical retention: the destabilizing force is smallest at the symmetric position and grows as the part displaces, which is exactly when it is hardest to stop.
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Cheap full-scale field techniques that earned their keep: compass-and-drawing-board flux plots traced field-line shape, with a repeat-trace of the same line agreeing within 1/16 in - a repeatability check (the absolute-accuracy figure, meter-calibration practice and normalization scheme are the report's account - re-read queued).
Source quote & editorial note
A check of the accuracy of this method was made by determining the same line twice, and this check indicated that the error was not greater than 1/16 in.
Editorial note, tabletop extrapolation: Three habits for a home lab, each with its honest scope: repeat-trace to establish a method's REPEATABILITY (absolute accuracy needs an independent reference); calibrate the current meter, usually the floor of a B-vs-I curve; and normalize survey data to a monitor reading so supply drift cancels out of shape maps - valid once shape invariance over the current excursion is verified and the hysteresis cycle is reproducible.
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Copy a proven machine when one exists at your scale: the UW 60-inch worked from a complete set of Berkeley Crocker plans, followed 'closely on the magnet design', drew sustained advice from the originating lab, and reached assembled-ready-for-test in three years - a schedule the report credits to exactly that inheritance; original design effort went to the subsystems where the precedent was silent.
Source quote & editorial note
We have had available for our use a complete set of the Berkeley plans which was kindly placed at our disposal by Professor E. O. Lawrence.
Editorial note, tabletop extrapolation: The strategy transfers directly: for any new machine, start from the closest documented working design - this corpus and the builds census exist to make that possible - and spend novelty only where the precedent is silent.
Cited in: Choosing Your Machine
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Know the fixed-frequency niche boundary: a 60-inch pole at ~15 kG is "about the optimum dimensions in which deuterons may be accelerated profitably without resorting to frequency modulation" — beyond this scale relativistic phase slip forces FM/synchro operation. Below it, constant-frequency operation buys large beam currents.
Source quote & editorial note
A magnet of this size when used with detuerons, is about the optimum dimensions in which deuterons may be accelerated profitably without resorting to frequency modulation.
Editorial note, tabletop extrapolation: Any tabletop proton/deuteron machine sits far inside the fixed-frequency regime: phase slip there is dominated by field shaping and dee voltage, not relativity. Fix small-machine beam loss with shimming and volts-per-turn first (dg-273's summed-slip check), and reserve frequency modulation for the relativistic regime this rule bounds.
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Use the site as shielding: the UW building was placed to exploit a natural ravine, and the machine sits in a 40-ft-diameter circular room with 10 ft of earth on the perimeter and 24 in of water above the ceiling — earth and water doing what concrete would otherwise cost.
Source quote & editorial note
It is designed so as to take maximum advantage of naturally occurring shielding of a small ravine.
Editorial note, tabletop extrapolation: The siting lesson transfers even if the scale does not: cheap mass - earth berms, water, basement corners - is legitimate shielding MATERIAL for a D-D-capable machine, once treated as engineering rather than slogan: effectiveness depends on composition, thickness, geometry and the capture gammas that moderation produces (hydrogenous media slow neutrons well, then emit 2.2 MeV capture photons), so earth and water get designed and surveyed like any shield (see the shielding deep dive). Spec detail: PDF p.128.
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Specify magnet-core steel chemistry in the purchase order and verify it yourself - the quoted lesson: 'control of the magnetic properties in the manufacture of steel is rather uncertain.' UW's practice per the report: specified maximum chemistry (C 0.15 / Mn 0.5 / P 0.04 / S 0.045 / Si 0.2 per cent, Table A) and a Rowland ring machined from the same heat for a full magnetization curve (procedure detail: scan re-read queued).
Specified max: C 0.15%, Mn 0.5%, P 0.04%, S 0.045%, Si 0.2%Source quote & editorial note
Apparently the control of the magnetic properties in the manufacture of steel is rather uncertain.
Editorial note, tabletop extrapolation: For a next machine's magnet, low-carbon steel chemistry is worth a mill cert, and a sample ring (or bar) from the same stock measured on a cheap B-H rig turns FEMM's material curve from a guess into a measurement. Same measure-your-own-steel discipline as nyo-780.
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State the field-shape requirement as separable specs before shimming - the quoted pair: (1) in the median plane the radial variation must conform closely to a fairly well defined relation, and (2) inside the exit radius the field must be accurately symmetrical (which symmetry planes, and the shimming-campaign details, are the report's: scan re-read queued).
Source quote & editorial note
(1) in the median plane the variation of the intensity with radial distance must conform closely to a fairly well defined relation, and (2) inside the exit radius ... the field must be accurately symmetrical
Editorial note, tabletop extrapolation: DIRECT — the same decomposition (radial law, azimuthal symmetry, median-plane flatness) is how a tabletop field survey should be organized, each with its own instrument and its own fix.
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A scale-model magnet is a close call - UW's experience: the shim testing required was 'much less than anticipated', partly because part geometry 'limited the possible variations more closely than was expected'; their full weighing of the model's advantages and difficulties is the report's own list (scan re-read queued).
Scaling at constant B: J ~ 1/L; heat/volume ~ J^2 ~ 1/L^2Source quote & editorial note
the amount of testing required to arrive at a final shim design was much less than anticipated. This was due in part to the fact that the geometry of parts limited the possible variations more closely than was expected.
Editorial note, tabletop extrapolation: With FEMM the model-magnet role is filled by simulation (ucrl-31 showed the scale-model method itself; MacKenzie AECD-1850 the model-test discipline), but the balanced verdict is the lesson — physical iteration budget should go where the computable model is least trustworthy (saturation, real steel, mechanical tolerances).
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If you build a model magnet, minimize material variability: UW's 1/12 model used forgings poured from the same heat as the cyclotron magnet - the source's own words being 'it can be assumed magnetic properties are identical' - a precise replica except bolts and carrying lugs, with cover plates from scraps of the actual cover-plate stock.
Source quote & editorial note
The steel for both the cyclotron magnet and the model was poured from the same heat and it can be assumed magnetic properties are identical.
Editorial note, tabletop extrapolation: The transferable rule is representative material between test article and final article: a next machine's FEMM model should use a B-H curve measured on the actual purchased steel - on coupons matching the real stock's processing and orientation where possible - not a library curve for the nominal grade; same-heat stock reduces one variability source, it does not guarantee identity after different forging and machining.
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Support model (and real) coils against magnetic forces, not just gravity: UW's model coils, cooled by direct water contact "at the expense of structural support," were distorted when the supporting structure failed "presumably under the magnetic forces," developing shorted turns that dropped the field ~20% below the Rowland-ring prediction. Recovery expedient worth knowing: adding steel around the outer face of the yoke raised the gap field to its proper value "without affecting its shape appreciably."
Source quote & editorial note
the supporting structure for the coils failed, presumably under the magnetic forces. The coils became distorted and short circuits developed.
Editorial note, tabletop extrapolation: DIRECT at any scale: coil-on-coil and coil-on-iron forces scale with NI and B and have crushed amateur windings - brace windings as if they will be pushed, not just held up. (The outer return-path steel in UW's recovery is that machine's expedient; whether added steel raises gap field depends on where the circuit's reluctance actually sits - FEMM answers it.)
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Measure relative radial field dependence with two flip coils in opposition on a common rotating shaft - one fixed at the magnet axis, one moved radially - flipped simultaneously: cancelling most of the EMF permits high sensitivity on the DIFFERENCE and, in the source's words, eliminates the importance of drifting exciting current, inaccurate flipping, fluxmeter inconstancy and temperature effects; close current regulation became unnecessary. One reduced-sensitivity reading with the fixed coil alone establishes the percentage scale.
Source quote & editorial note
drifting of the exciting current, inaccurate flipping, inconstancy of the fluxmeter, and temperature effects
Editorial note, tabletop extrapolation: The differential trick ports to modern probes with its limits stated: two matched Hall/NMR channels read as a difference suppress the CORRELATED (common-mode) part of supply and thermal drift - each channel's independent drift, gain mismatch and temperature coefficient survive subtraction, so calibrate individually, synchronize acquisition, characterize the common-mode rejection, swap channels periodically, and anchor the percentage scale with an absolute reference reading.
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Shim-design criteria worth copying verbatim: (1) inside the exit radius the field as uniform as possible, decreasing no more than ~1% from center; (2) with a central spike, take the center value as the extrapolation ignoring the spike; (3) the decrease must be monotonic; (4) at the exit radius the field index n = -(r/B)(dB/dr) shall be 0.4; (5) exit Br as large as possible consistent with the rest. UW shim space: annular ring against each cover plate, 25.75 in inner radius, 3 in wide, 1 in high; optimum found was a rectangular section equivalent to 5/8 in x 3 in; external shims in the 1/2-in pole-face-to-cover-plate air gaps "were found to have no appreciable added effect."
n = -(r/B)(dB/dr) = 0.4 at exit radius; interior droop <= 1% of centerSource quote & editorial note
at the exit radius the parameter n = - (r/B)(dB/dr) shall have the value 0.4.
Editorial note, tabletop extrapolation: DIRECT as an as-built spec that produced a working field: UW's n = 0.4 exit value and ~1% monotonic interior droop sit in the same territory as this collection's Wouters and Livingston rules. Adopt the criteria's STRUCTURE as a FEMM shim-study objective - uniform interior, monotonic decrease, a defined extrapolation convention, a specified exit index - and set the NUMBERS from the machine's own stability and extraction analysis: 0.4 was their exit choice, not universal physics.
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Check a max-performance shim against reduced-field operation before accepting it: UW's highest-exit-momentum shim produced a minimum in the radial dependence when the exciting current was reduced - 'an objectionable feature' - and the adopted compromise (3 in x 1/2 in shim, 25-in exit radius, per the report's scrambled-OCR pages: usable shape over roughly 13,900-15,000 gauss with exit droop up to ~2.2% - figures sighted in the scan, verbatim re-read queued) shows a shim design is valid over a FIELD RANGE, not at a point.
Source quote & editorial note
with this shim design a reduction of the exciting current produced a minimum in the radial dependence, which is an objectionable feature.
Editorial note, tabletop extrapolation: A variable-energy or B-scanned tabletop machine must verify field shape at the extremes of its intended excitation range, not just the design point - iron saturation moves the shim's effect as B changes.
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Magnetic force on ferromagnetic chamber covers inside the gap can exceed the atmospheric load - size the structure for both: UW's model study found the pull on the mild-steel vacuum-tank cover plates exceeded 35 tons against 24 tons of atmospheric force - half again the vacuum load, on that machine.
UW 60-inch: magnetic pull on covers > 35 tons vs atmospheric 24 tonsSource quote & editorial note
the results indicated a force greater than 35 tons for the cyclotron magnet. For comparison the force of atmospheric pressure is 24 tons.
Editorial note, tabletop extrapolation: A ferromagnetic chamber lid or pole-integrated cover sees magnetic clamping of the same ORDER as the vacuum load at tabletop fields (B^2/(2*mu0) vs one atmosphere - dg-177's arithmetic): check deflection in both states (energized and not) and expect assembly/disassembly forces. A non-magnetic lid opts out of the magnetic term entirely.
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Verify the model's prediction on the full magnet before committing to shims: UW's comparison 'showed that the model data could be used as a basis of prediction with confidence' - the quoted conclusion; the measure-reconcile-then-shim sequence is the report's campaign narrative (scan re-read queued).
Source quote & editorial note
showed that the model data could be used as a basis of prediction with confidence.
Editorial note, tabletop extrapolation: The FEMM-era version — survey the bare magnet, reconcile with the simulation, THEN machine shims from the reconciled model. Same model-then-verify discipline as MacKenzie's aecd-1850.
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Central spikes: a cone-topped cylinder at the magnet center (UW: 1.5-in radius, 1/4-in cylinder + 1/4-in cone) is designed 'to produce a sharp increase in the induction at the center of gap without producing a minimum anywhere in the radial dependence' - adopted after a University of California report of a beam-current increase from such spikes (the 'remarkable increase' phrasing is sighted in the scrambled scan; verbatim re-read queued); even undersized spikes were judged worth installing.
Source quote & editorial note
The function of the spikes is to produce a sharp increase in the induction at the center of gap without producing a minimum anywhere in the radial dependence.
Editorial note, tabletop extrapolation: A central field bump gives axial focusing in the first turns, where small machines lose most of their beam - and a machined center button is one of the cheapest beam-current experiments available. The no-minimum constraint is the careful part: model and map B(r), check the field index, isochronism cost, and RF/vacuum clearance before installing.
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Expect azimuthal asymmetry from a definite checklist of construction features: UW's list runs from small asymmetric steel details - bolts securing the cover-plate sections, screws holding the copper liners, the gap where a shim is relieved for water lines - through (3) accidental asymmetries in the construction and placing of the coils, and (4) non-uniformities in the steel (the unsymmetric-yoke item (1) is the report's, sighted in the scrambled scan).
Source quote & editorial note
notably the bolts securing the one-inch thick sections of the cover plates, the screws holding the copper liners, and a gap where the shim is relieved to accommodate water lines, (3) accidental asymmetries in the construction and placing of the coils, and (4) non-uniformities in the steel
Editorial note, tabletop extrapolation: An H-frame yoke is asymmetric by construction. Keep fasteners, liner screws, and cooling-line reliefs symmetric in the pole region; for unavoidable asymmetries, measure the azimuthal Fourier harmonics and judge them against orbit tolerances - a bare field survey doesn't by itself say the beam doesn't care.
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Correct pole/cover nonparallelism with the FIELD as the criterion, not the machinist's indicator: UW's consistent 180-degree azimuthal field variation implicated nonparallelism (poles parallel within 0.007 in, cover plates off by 0.031 in "in just such a direction as would account for the variation"); they had deliberately delayed mechanical correction so the field itself could be the final-adjustment criterion. Spacing shims in the air gaps removed most of it; the residue was killed with ~0.001-in additional shims sized by EXTRAPOLATING the measured effect of the first set; leftover local imperfections took external mild-steel shims in the 1/2-in air gaps, to a limit set by the fact that "an attempt to correct the field at one point has extended influence."
Source quote & editorial note
this correction was made the criterion for final adjustment rather than reference to mechanical measurements.
Editorial note, tabletop extrapolation: Shim the measured field, not the dial indicator: use the mapped field as the final acceptance criterion, calibrate shim sensitivity from the first iteration and extrapolate to plan the next, and expect a floor - every local correction has extended influence. Whether a given pole tilt is VISIBLE on a tabletop survey depends on gap, probe resolution and orbit radius, so establish the machine's own sensitivity from that first shim iteration rather than assuming thousandths show.
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Azimuthal-uniformity achievable by systematic shimming of a 60-inch-class magnet (Table C, 15 kG central field, extreme variation in per cent): original 0.045 (r=5 in) rising to 0.496 (r=27 in); after paralleling the tank covers 0.027-0.344; final 0.002-0.132. Judge by the value near r ~ 21 in ("the most significant value ... because at smaller radii the field is uniform, while larger radii correspond to the conclusion of the acceleration process where misdirection of the beam does not have serious consequences").
Worst-case azimuthal variation: as-built ~0.5% -> covers paralleled ~0.35% -> shimmed ~0.13% (at r=27 in, 15 kG); ~0.04% at working radiiSource quote & editorial note
at smaller radii the field is uniform, while larger radii correspond to the conclusion of the acceleration process where misdirection of the beam does not have serious consequences.
Editorial note, tabletop extrapolation: Sets a realistic bar as HISTORICAL performance: a carefully shimmed 60-inch-class iron magnet held azimuthal variation to a few parts in 1e4 over its working radii, and UW judged the spec at the radius that mattered dynamically (~80% in their machine - because inner radii were already uniform and the outermost turns tolerate misdirection). For a tabletop machine, pick the radius-weighting and the tolerance from its own orbit tracking and extraction plan; the UW numbers calibrate ambition, not the spec sheet.
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The median SURFACE is a separate spec from azimuthal symmetry: 'an azimuthally symmetric field may still have a dish-shaped median surface.' UW mapped it with a dipping needle - a soft-iron rod 0.10 in dia x 1.50 in long on a tensioned horizontal silk thread carrying a mirror, read by telescope - finding max departure 0.5 in from the geometric midplane, accepted without direct correction; their later azimuthal shimming was kept symmetric about the midplane to avoid introducing new vertical asymmetry.
Source quote & editorial note
an azimuthally symmetric field may still have a dish-shaped median surface.
Editorial note, tabletop extrapolation: DIRECT physics: a displaced or dished magnetic median surface costs vertical aperture and can steer the circulating beam into a dee lid at small gap heights. Put a dip-needle analog (or vertical probe-pair difference) in the survey plan, keep deliberate shims matched top-and-bottom - and REMAP the median surface after shimming: symmetric shims avoid adding first-order asymmetry, but changed gradients can still move a pre-existing displaced surface. Needle details PDF p.44, map Fig. 3.13 p.45.
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Choose chamber material for activation, not just vacuum: the UW tank is 2.5-in 61S-T4 aluminum, heliarc (argon TIG) welded, machined in an outside shop — "Aluminum was chosen over stainless steel because of its short half-life property" — and held 2e-6 mm Hg. The steel cover plates were poured from the same heat as the magnet forgings (they are part of the magnetic circuit): 4.5-in plate plus 1-in plate attached by screws.
Source quote & editorial note
Aluminum was chosen over stainless steel because of its short half-life property.
Editorial note, tabletop extrapolation: DIRECT for any machine that will make neutrons: aluminum's dominant activation products are short-lived compared with stainless steel's cobalt-trace Co-60 (years) - the report's reasoning - though aluminum is not activation-proof: fast neutrons make 24Na (15 h) and alloying elements add their own products, so 'short half-life' is comparative, never absolute. Choose the beam-facing metal for the machine you hope it becomes; TIG-welded aluminum is proven UHV-adequate practice from 1951.
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Double gaskets with a pumped interspace, everywhere possible: UW used "Berkeley standard double groove gaskets with pump outs ... on all joints" of the tank, and double gaskets with pump-out space wherever possible throughout the 4800-liter envelope; single stuffing-box gaskets only around water lines, ion-gauge tubes, RF-loop insulators, viewports. Materials: Garlock style 8474 hycar rubber, molded hycar sandwich gaskets, standard O-rings; chevron seals on moving shafts (O-rings on small ones). The leak record vindicates the ranking: leaks appeared in two stuffing-box seals and one flat gasket (rubber failure) — none in the double-gasket joints.
Source quote & editorial note
Double gaskets with a pump-out space between the two gaskets are used wherever possible for making seals at the joints in the system.
Editorial note, tabletop extrapolation: Same guard-vacuum doctrine as ornl-1196/anl-5907: on a tabletop machine the pumped interspace is most worth its complexity on the largest lid and any joint opened often. Material translation: the 1951 Hycar parts are the nitrile (Buna-N/NBR) family; Viton/FKM is a DIFFERENT modern option chosen on temperature, chemistry, permeation and compression-set grounds, not a synonym. UW's leak record (two stuffing-box seals, one flat gasket, zero double-gasket joints) is favorable single-system experience for the ranking, not proof.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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When welds leak, look at the dissimilar-metal joints first: initial testing of the UW envelope "disclosed two leaks in welds, both of which were in stainless to mild steel joints." Same-metal welds were tight.
Source quote & editorial note
Initial testing of the system disclosed two leaks in welds, both of which were in stainless to mild steel joints.
Editorial note, tabletop extrapolation: Treat dissimilar-metal welds (stainless-to-mild first among them) as leak-hunt and inspection PRIORITIES - their risk depends on filler choice, joint design and thermal cycling, so this is a where-to-look-first rule, not a they-always-leak rule. Keep such transitions accessible for repair, or design them out with transition flanges and gaskets.
Cited in: The Vacuum Budget of a Cyclotron
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Budget base pressure against interior surface area, and measure your diffusion pump's optimum heater power instead of trusting the nameplate: UW reached 2e-6 mm Hg bare (no traps, no refrigerated baffle); installing the copper liners, RF loops and insulators "approximately tripled the interior surface area" and moved the floor to 4e-6. Pumping-speed measurements set heater inputs at 3100 W (MC-7000, rated 3.5 kW) and 825 W (MB-200, rated 1 kW). Pump-down: 45 min roughing to 50 microns + 10-15 min diffusion to <2e-5; operating pressure 2-4e-5 mm Hg.
Surface x3 -> base pressure x2 (2e-6 -> 4e-6 mm Hg); pumpdown ~1 hr for 4800 L (110 cfm mech + 3500 L/s diff)Source quote & editorial note
Installation of the copper tank liners, R. F. loops and loop insulators approximately tripled the interior surface area
Editorial note, tabletop extrapolation: DIRECT: every liner, loop and insulator added to a chamber is outgassing area, and UW's base pressure roughly doubled when their additions tripled the surface. Base pressure follows total outgassing over delivered speed (P ~ sum(q_i*A_i)/S_eff), so area is the usual driver - materials and cleaning move the q's. The variac experiment (heater power vs measured speed) remains the way to find a surplus diffusion pump's real optimum.
Cited in: The Vacuum Budget of a Cyclotron
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Dee construction pattern for water-cooled copper dees: 1/8-in electrolytic high-conductivity copper skin with 1/4, 3/8 and 5/8-in copper tubes silver-soldered on the back for cooling; each dee and stem SPLIT longitudinally so halves separate for repair; joining surfaces of liner sections silver-plated for RF contact; the movable shorting "spider" that tunes the resonant line held at ~100 lb per lineal inch of contact pressure, with spring-loaded gear- and cable-driven fingers, externally controlled. Dees 53 in dia on 9.75-in OD stems inside a 31-in ID liner.
Source quote & editorial note
The skin is of electrolytic high conducitvity copper with 1/4, 3/8, and 5/8" copper tubes silver soldered on the back side for water cooling.
Editorial note, tabletop extrapolation: The construction vocabulary transfers as a menu, not a mandate: EHC copper skin with cooling sized from computed RF loss (a tabletop dee at tens of watts may need none), silver-plated joints where measured contact resistance warrants, high-pressure sliding contacts only on genuinely movable RF joints, and split-for-repair weighed against the RF seam it adds. Same contact-pressure concern as the nyo-9683/ornl-2648 sliding-contact rules when a movable short exists.
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Design vacuum locks so consumables and the whole source can be changed without venting: the UW ion source has a filament lock (replace the filament without breaking tank vacuum) AND a source lock — a heliarc-welded aluminum box with a swinging toggle- clamped gate — through which the entire source assembly withdraws upward on a guide track; three adjusting screws on a sylphon position the source in both planes from outside; the lock's 4-in glass viewing window carries a hinged brass shutter so metal vapor from the arc cannot coat it.
Source quote & editorial note
the filament may be replaced without breaking the vacuum of the tank proper.
Editorial note, tabletop extrapolation: The reference machine's filament-change downtime is this exact problem, solved in 1951: a small gate-valved source lock plus an external bellows positioner removes the main-tank vent from the service cycle - how much time that saves depends on the lock's own pump-down and the machine's recovery habits, so measure it rather than promise minutes. Positioning through the bellows under vacuum is the designed use; adjusting with arc, RF or HV energized is a separate safety analysis with its own interlocks, not an included feature. (The shuttered viewport is a free detail worth stealing.)
Cited in: The Vacuum Budget of a Cyclotron
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Size oscillator power from Q and dee reactance before choosing a tube, then add margin for what the analysis cannot know: UW measured/computed system Q ~ 7500 (line alone ~11,000 before dee and joint losses), dee capacitive reactance X ~ 40 ohms, so 160 kV peak gap needs ~21.2 kW and 250 kV needs ~52 kW; 150 kW was selected as the provided maximum "upon considering the approximations necessarily made in this type of analysis" (150 kW would drive ~450 kV — above what the dees could stand — so the margin is real headroom, not a target). Dees, stems, liner and supply components were all rated to the 150 kW figure, and the tube chosen to survive dee arcs.
P = Epk^2/(4*Q*X); 21.2 kW @ 160 kV, 52 kW @ 250 kV for Q=7500, X=40 ohmSource quote & editorial note
upon considering the approximations necessarily made in this type of analysis, the figure of 150 kw maximum r-f power was selected.
Editorial note, tabletop extrapolation: DIRECT scaling method for the LDMOS upgrade: measure the dee system's Q and C, compute watts per kV from P = V^2/(4QX) (equivalently V^2/(2*R_shunt)), then add margin for what the lumped model misses - beam loading, coupling loss, arcs, duty cycle. UW's own practice sized 150 kW against a ~52 kW computed requirement, roughly 3x, 'upon considering the approximations'; let your margin come from your own unknowns inventory, with theirs as the precedent.
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A two-dee system has two coupled modes - a zero mode with the dees swinging in phase (no accelerating gap voltage) and a pi mode swinging opposite (gap voltage present) - and the oscillator coupling must select the pi mode: the quote records UW choosing the drive method easiest to hold at 180 degrees. Mode spacing depends on the coupling geometry.
Source quote & editorial note
This method should be easiest of the methods used to assure oscillation at the proper frequency with the dees operating 180 degrees out of phase.
Editorial note, tabletop extrapolation: For a one-dee-plus-dummy machine the mode problem collapses. For any driven system, verify which resonance the amplifier locks to - a network-analyzer sweep plus a phase comparison between dee pickups distinguishes the modes - because the wrong one accelerates nothing.
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Plan the multipactor climb-through at design time: UW knew that 'electron oscillations in the vicinity of the dees and dee stems at low r-f voltages tend to absorb energy and prevent the oscillations from building up' - and designed for it; their booster/driver arrangement is the report's implementation (topology, rating and isolation details: scan re-read queued).
Source quote & editorial note
Electron oscillations in the vicinity of the dees and dee stems at low r-f voltages tend to absorb energy and prevent the oscillations from building up.
Editorial note, tabletop extrapolation: The corpus's driven-start cure (mddc-1045 tickler; nyo-9359's catalogue) as a 1951 DESIGN feature rather than a retrofit, including the half-frequency/doubler isolation trick that spares a changeover switch. Directly relevant to the reference machine's dee-voltage buildup pathology: any LDMOS drive chain is inherently a driven start, but only if it can push watts through the multipactor loading band without foldback or protection tripping - and that band's voltage is geometry-, frequency-, pressure- and surface-dependent, so measure it on the actual dee. [Note revised 2026-08-23: the earlier note quoted '~100 V' for the band as if it were a design constant.]
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Model the RF system at reduced scale before building it: UW's quarter-scale model of the resonant system was the answer to 'many uncertainties in the exact determination of the constants of the equivalent circuit' - calculated values 'serve well as a guide', and the model settles them (the model's dimensions, Q and adjustment history: scan re-read queued).
Source quote & editorial note
there are many uncertainties in the exact determination of the constants of the equivalent circuit ... the calculated values ... serve well as a guide
Editorial note, tabletop extrapolation: A tabletop resonator IS the scale model — build the dee/stem mockup on the bench, measure f and Q before committing to vacuum hardware, and trust lumped calculations as guides not gospel. Berkeley used the same quarter-scale method on the 88-inch (ucrl-9435), which also confirms the Q-degradation-at-joints lesson (ornl-2648).
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Ground the anode DC and float the filament for a big-tube oscillator, and the cooling plumbing simplifies: UW runs the ML 354 with the plate at d-c ground (shunt feed), "so that no insulation is required in the water lines," cooling water flowing through the plate line's inner conductor; the filament sits at high negative voltage, its transformer insulated for full plate voltage to ground, and deliberately of high-reactance design so the cold-filament inrush is limited to 500 A — the tube's own safe limit — with 13 V / 225 A normal rating.
Source quote & editorial note
the plate is operated at d-c ground potential so that no insulation is required in the water lines.
Editorial note, tabletop extrapolation: Solid-state amps moot the HV plumbing, but two doctrines survive: pick the grounding scheme that minimizes what the coolant circuit must insulate - DC-grounding the plate removed the DC insulation requirement, while RF potentials, leakage control and water quality stay on the checklist - and use source impedance (here transformer reactance) as passive inrush protection where a component's own rating allows it.
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Instrument HV circuits by magnetic isolation where a direct meter would sit at kilovolts: UW measures grid current (in a lead at high negative voltage) by passing it through the control winding of a SATURABLE REACTOR whose AC winding sits in an inductance bridge at ground — the DC value is read as a bridge unbalance with full galvanic isolation. Dee voltage is read by series-type peak voltmeters fed from small capacity probes facing copper paddles soldered to the dee edge, the diode voltmeter housed in a magnetically shielded box outside the tank.
Source quote & editorial note
measured by means of a saturable reactor ... The dee voltmeters are of the series type coupled ... by a small capacity between the probe and a copper paddle soldered to the dee edge.
Editorial note, tabletop extrapolation: The capacitive-paddle dee voltmeter is the instrument Koeth calibrated on the Rutgers 12-inch and the missing calibration behind the reference machine's ~1.3 kV: a soldered paddle + defined-gap probe + diode peak detector, calibrated IN SITU against an RF-RATED reference at the operating frequency - and recalibrated after any geometry, frequency, detector or cabling change (dg-307's Houghton data show the factor moves with frequency). The saturable-reactor trick survives as the Hall/fluxgate-sensor principle - never bring an HV node to the meter; a bare shunt is not isolated, it needs a rated isolation amplifier.
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A protective subsystem may be deleted only with its function accounted for and the reasoning recorded: UW omitted the customary constant-current (current-limiting) network between rectifier and oscillator "on the basis of cost," accepting the risk because the main breaker clears faults within 6 cycles and a glo-coil resistor bank can be inserted for initial operation and commissioning.
Source quote & editorial note
On the basis of cost it was decided to omit this refinement.
Editorial note, tabletop extrapolation: The decision pattern - name the deleted protection, name what stands in for it, keep a commissioning-only resistor in the drawer - is reusable as an engineered, recorded risk acceptance, not a license: verify the stand-ins actually bound the fault energy for YOUR stored energy and clearing time (a 6-cycle breaker passes ~0.1 s of fault current), and re-examine the acceptance at each upgrade. Contrast ucrl-9435, where the 88-inch - with 20x the stored energy - bought the full hard-tube-modulator protection instead. Scale decides.
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Control-system requirements worth copying whole: (1) EVERYTHING interlocked "in such a manner that serious damage cannot occur" for ANY fault — operator error, water failure, vacuum leak; (2) all major equipment startable from the control room in a definite sequence; (3) pilot lights showing both the exact operating state and THE REASON any unit failed to operate; (4) wiring arranged so units can be added with minimum rework (UW: cross-connect terminal boards in each room, one master schematic kept up to date, books of vacant terminals/wires/relay contacts). Operationally: gang-switched start sequence; paired on/off pushbuttons whose green READY light means the interlock chain ahead is satisfied; the LAST button in the chain applies oscillator plate voltage; on shutdown a time delay keeps cooling water, towers and oil pumps running ~5 minutes.
Source quote & editorial note
it should be completely interlocked in such a manner that serious damage cannot occur due to any failure of the operator or of equipment such as water failure or a vacuum leak.
Editorial note, tabletop extrapolation: A strong SEED for a tabletop control panel or PLC - the quoted requirement (no serious damage from ANY single operator or equipment failure) plus their sequence logic - to be completed rather than copied: the 1951 scheme is equipment protection, and a modern chain adds the personnel-safety layer on top (access, radiation, e-stop: dg-1065, dg-1072, dg-1075).
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Sequence deflector fabrication behind first internal beam: UW completed the deflector's preliminary design but scheduled that "machining work will begin after the oscillator is operating and an internal beam produced" — the probe (water-cooled internal target, 10-25 in radius by remote control, through its own vacuum lock) comes first, because internal beam data retire more risk than a finished deflector does.
Source quote & editorial note
Machining work will begin after the oscillator is operating and an internal beam produced.
Editorial note, tabletop extrapolation: The commissioning-order lesson as an explicit 1951 schedule decision: internal beam first, extraction hardware behind it. A sensible default for a next machine - the probe and its lock as first-beam hardware, extraction machining held until the internal beam teaches you the real orbit - a default, not a law.
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Deflector doctrine from the UW study, anchored on its phase analysis: a minimum of 80 kV dee-to-ground RF was calculated necessary so ions never enter decelerating phase within the dees (the 70-degree geometry, DC-supplement thresholds, channel dimensions and energy-spread figures are the study's design narrative - scan re-read queued, including which electrode is RF-energized in their plate-at-RF-ground scheme).
UW: 70-deg deflector from 60 deg past gap; >=80 kV RF floor; DC supplement below ~120 kV dee; selective channel 0.90 cm -> ~1.5 MeV spread at 21 MeVSource quote & editorial note
a minimum of 80 kv dee to ground r.f. potential is necessary in order that the ions do not enter the region of decelerating phase at any time within the dees.
Editorial note, tabletop extrapolation: Two transferable ideas for any future extraction study: run the phase-floor analysis BEFORE cutting metal (the computation this collection's deflector cluster expects), and consider using the machine's existing RF field for deflection with DC as supplement - after resolving the geometry from the re-read, since a deflection field needs a potential difference and the as-summarized grounded-plate-vs-grounded-dee-edge description cannot be right as written.
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Measure extracted beam power by direct charge collection when the calorimetric signal is weak: UW preferred the insulated-probe current measurement because at appreciable water flow the temperature difference was very small and hard to read accurately.
Source quote & editorial note
the direct measurement is preferable since for appreciable water flow the temperature difference is very small.
Editorial note, tabletop extrapolation: Do the arithmetic before dismissing either method: P = I*E/q puts 1 uA at 0.1-1 MV at 0.1-1 W - readable by a thermally isolated calorimeter, invisible in high-flow cooling water. The Faraday cup with secondary-electron suppression remains the primary tabletop instrument (with energy known independently to convert current to power); calorimetry earns its place when isolation makes the temperature rise measurable, not at any fixed wattage threshold.
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Construction cost structure of a university-built 60-inch, 1948-1951: total ~$642,000 to April 15, 1951, excluding University of Washington overhead and staff salaries; the report's accounting (allocation figures sighted in the scrambled scan - verbatim re-read queued) puts buildings at ~$225,000 against machine materials ~$201,500, with visible payroll only ~$14,000 - most machine labor being institutional or donated (Navy-supplied machine tools, supplier assistance).
Buildings $225k > machine materials $201.5k; visible payroll only $14k of $642kSource quote & editorial note
Total expenditures to date from all sources, excluding University of Washington overhead and staff salaries, has been $642,000.
Editorial note, tabletop extrapolation: A historical cost-accounting example that corroborates the plan's assumption from the construction side: facility/infrastructure rivalled machine materials HERE, and reported totals understate true cost by the labor the institution absorbed - for an educational-accelerator business, price materials PLUS the labor a customer cannot donate. One project's ratio is context, not a law.
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Cyclotron RF differs from industrial RF in ways to design for from day one - the report's headline differences: (a) the resonator is a sparking load that can deliver large energy into the electronics; (b) multipactoring, 'common in the field of particle accelerators, rarely occurs in other industrial applications' (the quoted item); (c) frequency agility where the machine class needs it.
Source quote & editorial note
(b) the multipactoring problem, common in the field of particle accelerators, rarely occurs in other industrial applications
Editorial note, tabletop extrapolation: The checklist for adapting any industrial or ham RF gear (an LDMOS pallet included) to a cyclotron: add spark protection, add a multipactor start plan, and only then worry about power. Fixed-frequency tabletop machines are spared only (c).
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Multipactor physics in one sentence pair: electrons in the dee-ground gap whose transit time is half the RF period multiply when the secondary-emission ratio exceeds unity — "The threshold of secondary emission is about 150 electron volts for most surfaces; consequently, multipactoring becomes possible when the voltage across the dees reaches this value." One standard cure on the 88-inch: a dc sweeping field superimposed across the RF gap to pull electrons out faster than they multiply.
multipactor onset near the secondary-emission threshold (~150 eV -> ~150 V-class gap voltages) WHERE a resonant transit condition also holds; band edges move with gap, frequency and surface yieldsSource quote & editorial note
The threshold of secondary emission is about 150 electron volts for most surfaces; consequently, multipactoring becomes possible when the voltage across the dees reaches this value.
Editorial note, tabletop extrapolation: DIRECT: a small machine's dee voltage passes through the ~100-150 V-class region on every start - whether multipactor actually lights there depends on the gap-frequency resonance and the surfaces' secondary yields, which is why some machines never see it. Completes this collection's cure set: mddc-1045 (bias + tickler), nyo-9359 (impulse start), ucrl-64 (volume reduction + bias).
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Bake in a new dee system by letting it spark - by the hundred thousand: the 88-inch's conditioning involved several hundred thousand sparks, after which the dee would usually hold many times its initial voltage; each spark's energy (~4.5 J stored in that resonator) burns out the whisker or inclusion that initiated it - sparking as the conditioning mechanism, not merely a failure mode.
conditioning scale: ~1e5-1e6 sparks (88-inch); per-spark energy = the RESONATOR'S stored energy, computed from C, V and Q - never assumed from physical sizeSource quote & editorial note
It usually involves permitting the dee to spark several hundred thousand times. Afterwards, it will usually hold many times the voltage that it would initially.
Editorial note, tabletop extrapolation: For the 5-13 kV dee upgrade, plan a conditioning campaign rather than reading early sparking as failure - a supervised one: compute the actual stored and delivered fault energy first, current-limit and arc-detect, set the auto-recycle behavior from that arithmetic, monitor temperatures, and inspect between sessions. Corroborates the ornl-2648/nyo-9683 conditioning rules and quantifies the count.
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Every dee spark is a system-wide transient that can trigger a spark inside the oscillator tube and divert the full dc supply as a power arc - so protection is layered by speed: Berkeley's hard-tube series switch opens the anode circuit within 10 microseconds of a fault (the quoted spec), with slower switch layers behind it (their arrangement: scan re-read queued).
Protection ladder: hard-tube series switch ~10 us; ac vacuum switches ~10 ms; (alternative: ignitron crowbar)Source quote & editorial note
In this service it will open the anode circuit within 10 usec of a fault.
Editorial note, tabletop extrapolation: The modern translation, mapped by FUNCTION rather than spec-for-spec: an LDMOS drain supply wants a fast electronic disconnect (the hard-tube modulator's descendant), a slower breaker layer, and snubbing on the dc feed - each layer rated against the actual stored energies and fault modes of the build (dg-330, dg-679, dg-1371).
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THE SELF-EXCITED POSITION (design tension with the MOPA position of ornl-2403): Smith's 88-inch runs the resonator as the frequency-determining element - 'hence it is called a self-excited oscillator' - with the report's implementation figures (AFC, regulation) as its own record (scan re-read queued for those numbers).
Source quote & editorial note
In this type of system the resonator is the frequency-determining element of the system; hence it is called a self-excited oscillator.
Editorial note, tabletop extrapolation: The live architecture decision for a next machine. An LDMOS chain driven by a synthesizer is a MOPA — it inherits ornl-2403's virtues (frequency authority, instrumentation) AND the self-excited literature's start-up disease (nyo-9359): the synthesizer holds frequency while multipactor holds the dee at zero. Smith's phase-discipline logic (feedback phase correct across the whole operating range) is the checklist item either way. High-SWR argument p.6.
Cited in: Driving the Dee: RF Coupling
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Budget resonator power in four named parts, and the beam is not negligible: for the 88-inch at 70 kV dee — RF skin losses 121 kW (computed several ways from the measured voltage/current distribution of the resonator), stray-ion loss at the machine center ~30 kW at maximum energy, beam power 60 kW (1 mA at 60 MeV), miscellaneous (couplings, harmonics radiated into the tank) ~10 kW; total 221 kW, so 300 kW was provided. A corrugated dee stem (longitudinal corrugations increase skin perimeter) cut current density enough to save ~70 kW of the copper loss.
P_total = P_skin + P_stray-ion + P_beam + P_misc; 88-inch @ 70 kV: 121 + 30 + 60 + 10 = 221 kW -> 300 kW installedSource quote & editorial note
At the maximum particle energy, the beam requires 60 kw of power.
Editorial note, tabletop extrapolation: The four-line budget is the right form at any scale. A tabletop version: watts of copper loss (dg-313), a beam line computed from ITS current and energy - 1 nA at 500 keV is 0.5 mW, 10 uA at 1 MeV is 10 W, small only until the source improves - a stray-ion line that follows source gas and RF (measurable as the loading difference with the source on vs off), and a misc line that is mostly coupling and radiation.
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Kill parasitics on paper first: the 88-inch adjusted its RF circuit elements so the first two higher modes would not be excited by an oscillator harmonic - verified on a quarter-scale RF model - after experiencing destructive voltages at the grid vacuum insulator when a mode landed wrong.
design check: no resonant mode (with its bandwidth) within margin of ANY materially present drive harmonic across the tuning range - low harmonics carry the most energy in class-C service, but a high-Q mode can be excited by higher ones if coupledSource quote & editorial note
The circuit elements of the rf system were adjusted so that the first two higher modes would not be excited by an oscillator harmonic.
Editorial note, tabletop extrapolation: For a fixed-frequency machine: sweep the dee system on a VNA, list the modes WITH their widths and couplings, and check them against the drive's measured harmonic spectrum - detune offenders with a strap or stub before blaming the amplifier for instability. Same mode-vs-harmonic discipline as the msucp-9 and ornl-2648 lines.
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Choose oscillator/amplifier tubes for spark survival, not just gain: sparks dump joules into "an area determined by the cross section of the spark," and conventional squirrel-cage grids of very light wire get blasted through, shorting grid to cathode. "For accelerator applications, a tube should have a sufficiently heavy grid to absorb several joules of energy" — the 6949's heavy grid bars hide behind massive copper shield tees "almost immune to spark damage," and its high power sensitivity (3 kW drive for 319 kW out) shrinks the grid line and allows a large safety factor in the grid vacuum insulator.
Source quote & editorial note
For accelerator applications, a tube should have a sufficiently heavy grid to absorb several joules of energy in an area determined by the cross section of the spark.
Editorial note, tabletop extrapolation: The solid-state translation: LDMOS devices have finite ESD, avalanche and mismatch ratings rather than a tube grid's joules of thermal mass, so the ruggedness must live in the coupling network - series blocking, clamping, fast drive-cut (dg-338, dg-758). A dee-side fault arrives first at the OUTPUT network, which is where the protection belongs.
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Interlock RF to the RATIO of dee voltage to oscillator anode dc — an arc holds the ratio low even while current flows: "The rf-dc interlock compares the dee voltage with the amount of oscillator anode dc. If the ratio is too low, indicating the presence of an arc, the fault detector opens the anode circuit and recycles, approximately 1 sec later." The ~1-s off-time is what the vacuum system needs to pump away the discharge products; normal operation EXPECTS periodic dee sparks, so recovery is automatic, not an operator event.
Trip on (V_dee / I_or_V_anode-dc) below threshold; auto-recycle after ~1 sSource quote & editorial note
The rf-dc interlock compares the dee voltage with the amount of oscillator anode dc. If the ratio is too low, indicating the presence of an arc, the fault detector opens the anode circuit and recycles
Editorial note, tabletop extrapolation: DIRECT and cheap: a comparator on the dee-voltage-to-drive ratio with a drop-and-retry turns dee sparks from session-enders into log entries - the ratio form matters, because absolute thresholds miss arcs that still draw full power. Two amendments for a tabletop copy: cap the retry count and latch out on repeated faults, since an endless auto-recycle would keep re-feeding a failed feedthrough or persistent arc; and if forward power stands in for anode dc, validate the arc signature on the actual amplifier - it is not the same quantity Smith's ratio used.
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Tune the fault-detector delay as a physics compromise, and Smith gives the number: the interlock signal is deliberately RC-slowed so the discharge persists about a millisecond — "long enough to vaporize the foreign material which initiated the spark. If the circuit is made too fast, it takes too long to bake the resonators in. If it is made too slow, the spark damage to the dee and liner surfaces will be excessive. Experience indicates that 1 msec is about the right delay." (Overcurrent faults in tube anode/grid circuits bypass this delay and open the hard-tube modulator in ~10 us.)
Spark dwell before interrupt: ~1 ms (conditioning); tube overcurrent path: ~10 usSource quote & editorial note
If the circuit is made too fast, it takes too long to bake the resonators in. If it is made too slow, the spark damage to the dee and linear surfaces will be excessive.
Editorial note, tabletop extrapolation: A protection spec you cannot derive from electronics alone: the dwell is chosen so each spark finishes cleaning the spot that caused it. The compromise transfers; the number does not - Smith's ~1 ms suits his machine's stored energy and electrode scale, so a tabletop supply picks its own dwell from its fault energy, starting shorter and lengthening only if conditioning stalls. Amplifier-device faults still trip as fast as the electronics allow: two speeds, two purposes.
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A cyclotron resonator's vacuum envelope relieves the stray-RF problem 'somewhat' - the quoted qualifier: the chamber that must be vacuum-tight is thereby RF-tight over its solid surfaces, and what escapes does so at the penetrations and the drive side.
Source quote & editorial note
the resonator has to be vacuum-tight, automatically making it rf-tight.
Editorial note, tabletop extrapolation: Comforting for a residential machine, with 'somewhat' doing real work: the metal chamber contains the dee's RF well, and the leakage paths are feedthroughs, viewports, gauge ports and the amplifier chain - gasket and shield those, then VERIFY with a receiver walk-around. Quiet neighbors' radios are a measurement, not a promise.
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Publish (and read) the tube operating point as a sanity anchor - Table I for the 6949 at 88-inch maximum: plate 15 kV / 25 A dc (375 kW input), grid current 1.4 A, bias -700 V from a 500-ohm grid resistance, driving power 3 kW, RF plate swing 14 kV / 130 A peak, output 319 kW - i.e. 85% plate efficiency in class C, power gain ~106 (20.3 dB), drive two orders below output.
6949 point: 319/375 = 85.1% plate efficiency; 319 kW / 3 kW = 20.3 dB gain; drive ~1/100 of outputSource quote & editorial note
Maximum operating conditions for the RCA 6949 for the 88-in. cyclotron
Editorial note, tabletop extrapolation: The ratio HABIT transfers, the numbers are this tube's: work out the equivalent operating-point ratios for the actual device from its own datasheet and measurements, and treat large departures from the device's own expected ratios as a prompt to look for mistuning, parasitics or multipactor loading - among other causes (topology, matching and the efficiency definition all move the numbers).
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Before dimensioning anything, draw the dependency diagram of the five subsystems (magnet, acceleration, ion, vacuum, detector) and separate the given inputs (pole radius, maximum orbit radius, nominal pumping speed, flux density, pole gap, gap width, dee amplitude, specific charge) from the quantities calculated from them (cyclotron frequency, rigidity, final velocity and energy, first-orbit radius and velocity, number of accelerations, total path length, effective pumping speed, mean free path, final pressure, permissible gas load).
Source quote & editorial note
Bevor man an den Nachbau eines Zyklotrons geht, muss man sich darüber im Klaren sein, was man benötigt. ... Bei den fünf Teilsystemen handelt es sich im einzelnen um das Magnet-System, das das Führungsfeld liefert, das Beschleunigungs-System, das für die Hochspannung sorgt, das Ionen-System, verantwortlich für die Produktion der Ionen, das Vakuum-System, das das erforderliche Vakuum zur Verfügung stellt, und schließlich das Detektor-System, das die beschleunigten Teilchen registriert. ... Die Vorgaben in den grünen Kreisen sind zum einen gerätespezifische Größen. Dazu gehören: der Radius der Magnetpole rp und der maximale Bahnradius ... das Nenn-Saugvermögen SN des Pumpstands [tr.: before building a cyclotron one must be clear what is needed; the five subsystems are the magnet system supplying the guide field, the acceleration system providing the high voltage, the ion system producing the ions, the vacuum system, and the detector system registering the accelerated particles; the givens in the green circles are device-specific quantities - the pole radius, the maximum orbit radius, the pump stand's nominal pumping speed - the calculated quantities in blue circles]
Editorial note, tabletop extrapolation: A small machine has few free parameters; listing which are fixed by hardware (pole radius, pump) and which are design choices (B, gap, U0, species) keeps the sizing chain consistent and exposes circular dependencies early.
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Treat magnetic rigidity zeta = B*rho (T m) as the magnet system's design variable: an ion that reaches radius rho carries p = q*B*rho and, nonrelativistically, E = q^2*(B*rho)^2/(2m) - the field-and-geometry CEILING on energy; dee voltage sets turn count and whether the ceiling is reachable, not the ceiling itself.
p_max = q*B*rho ; E_max = q^2*(B*rho)^2/(2*m) ; v_max = (q/m)*B*rhoSource quote & editorial note
Sie bestimmt die maximal erreichbare Energie der Ionen und diese ist somit nur vom Magnetfeld und dem Radius der Austrittsbahn abhängig [tr.: energy depends only on field and exit radius]
Editorial note, tabletop extrapolation: For 0.5 T and 10 cm usable radius, zeta = 0.05 T m gives ~120 keV protons; doubling either B or rho quadruples the ceiling. Low dee voltage doesn't lower it - but capture, phase acceptance and losses can keep the beam from ever reaching rho, which is the caveat behind 'regardless of dee voltage'.
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A worked magnet-selection step: a rigidity of 0.040 T m yields about 76 keV protons or 38 keV H2+ (v ~ 3.8e6 and 1.9e6 m/s); on the B-rho chart that is met by, for example, 1.0 T with a pole radius of at least 40 mm, so read the required (B, rho) pair off a constant-rigidity curve before shopping for a magnet.
B*rho = const ; rho_min = zeta/BSource quote & editorial note
Beträgt die Steifigkeit etwa 0,040 Tm, so liest man ab, dass die maximale Energie von Protonen ca. 76 keV [tr.: at 0.040 T m protons reach about 76 keV]
Editorial note, tabletop extrapolation: Recomputed and correct: 0.040 T m gives ~76.6 keV protons; the same chart logic at 0.06 T m (0.6 T, 10 cm) gives ~172 keV. Read the geometry carefully: 1.0 T with a 40 mm orbit needs 40 mm of USABLE-FIELD radius - the physical pole must be larger, by the fringe margin the field map shows (dg-1382). Scale energy targets from rigidity, not from voltage.
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Below a rigidity of about 0.3 T m (protons: 0.31 T m, 4.7 MeV, v = 0.1c) the source treats the machine as non-relativistic; the relativistic regime would demand fields of 3-6 T on 50-100 mm poles and is out of reach for small magnets. The boundary is a tolerance statement, not a switch: at beta = 0.1 the cyclotron frequency is already ~0.5% low.
zeta_rel = m*(0.1c)/q = 0.31 T m (H+), 0.63 T m (H2+)Source quote & editorial note
Für ζ ≤ 0,3 Tm ist man demnach im nichtrelativistischen Bereich [tr.: for zeta <= 0.3 T m one is in the non-relativistic regime]
Editorial note, tabletop extrapolation: A tabletop proton machine (zeta ~ 0.03-0.12 T m) sits comfortably below the bound - by a factor of 2.5 at the top of that range, not an order of magnitude. Constant-mass orbit codes are fine for geometry, but check the RF phase budget: even the ~1e-3-class frequency shift at 0.12 T m accumulates over hundreds of turns, so run the accumulated-phase check alongside the field-shape one rather than crediting all slip to field errors.
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COLUMBUS's practice for its borrowed laboratory magnet: run continuously at no more than half the MAXIMUM coil current to avoid overloading it, and pick the operating field where the data-sheet homogeneity is best rather than where the field is highest.
Source quote & editorial note
Um den Magneten nicht zu überlasten, sollte er im Dauerbetrieb höchstens mit der Hälfte des maximalen Spulenstroms betrieben werden [tr.: run at no more than half the maximum coil current in continuous duty]
Editorial note, tabletop extrapolation: For any other borrowed or surplus magnet, use its actual continuous-duty specification (maximum and continuous ratings differ) and verify winding temperature under your duty cycle - half-of-maximum is this book's conservative default when no continuous rating is known. The choose-field-by-homogeneity move transfers as stated; record the chosen point as a thermal/homogeneity compromise, not a hard limit.
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Read the magnet radial-homogeneity curve at the intended extraction radius and express it relative to B0: a laboratory magnet with 150 mm poles at a 75 mm gap shows at most 0.02 percent deviation at r = 70 mm for all three plotted central fields, so a plain flat-pole magnet of that class is homogeneous enough for a few-keV teaching machine without shimming.
dB/B0 at r = rhoSource quote & editorial note
Bei allen drei zentralen Feldstärken beträgt die relative Inhomogenität bei r = 70 mm maximal nur 0,02 % bzgl. B0 [tr.: at r = 70 mm the inhomogeneity is at most 0.02 percent of B0]
Editorial note, tabletop extrapolation: The 0.02% figure is a commercial NMR-class magnet's vendor-chart datum at gap/pole-ratio 0.5 - a CANDIDATE uniformity level: check its adequacy against your machine's allowable cumulative phase slip and turn count, and confirm with a two-dimensional map (radial AND azimuthal) before concluding no shimming is needed; a home H-frame with a tighter gap will differ in both directions.
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The pole gap equals the chamber height plus the walls, so let the lid do double duty: COLUMBUS mills a 150 mm diameter, 12 mm deep recess into the chamber lid, lowers the upper pole into it - giving the chamber a fixed seat in the magnet - and houses the Hall probe in the recess; the chamber height dropped to ~72 mm and the minimum pole spacing to ~75 mm.
delta_z = h_chamber_internal + t_base + t_lid_remainingSource quote & editorial note
In den Deckel ist eine Vertiefung mit einem Durchmesser von 150 mm und einer Tiefe von 12 mm eingefräst. Dort befindet sich eine Hallsonde für die Messung der magn. Flussdichte. In diese Vertiefung wird der obere Pol des Magneten abgesenkt; so erhält die Kammer im Magneten einen festen Sitz. Außerdem konnte dadurch die Kammerhöhe auf ca. 72 mm verringert werden. Unter Berücksichtigung der Materialstärke beträgt der minimale Polabstand des Magneten schließlich ca. 75 mm. [tr.: a 150 mm diameter, 12 mm deep recess is milled into the lid. A Hall probe for measuring the flux density sits there. The upper pole of the magnet is lowered into this recess, giving the chamber a fixed seat in the magnet; the chamber height could thereby be reduced to ~72 mm, and allowing for material thickness the minimum pole spacing is finally ~75 mm]
Editorial note, tabletop extrapolation: Every millimetre of gap costs ampere-turns; the recessed-lid trick keeps the poles within a few mm of the dee envelope while fixing the chamber and giving the field probe a home. Size the recess floor (and any thin base) by an actual vacuum-vessel calculation - plate deflection and buckling for the real material and span - not by copying this machine's dimensions; and note the probe reads the field at the recess, not the median plane, so calibrate the offset.
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Keep the maximum orbit radius a few millimetres inside the pole radius: with 150 mm poles the dee inside diameter was 140 mm, so rho = 70 mm is 5 mm short of the pole edge where the field starts to fall.
rho = r_pole - 5 mm (reference machine)Source quote & editorial note
Da der Innendurchmesser des Dees 140 mm beträgt, hat ρ den Wert 70 mm und ist damit um 5 mm kleiner als der Polradius [tr.: dee ID 140 mm, rho 70 mm, 5 mm less than pole radius]
Editorial note, tabletop extrapolation: Treat the 5 mm as this machine's geometric margin, not a rule: COLUMBUS runs a very LARGE gap-to-diameter ratio (75/150 = 0.5), so its field is far from flat at the edge anyway and the machine needs no extraction. For a 20 cm pole with a 2-3 cm gap the ratio is much smaller and the flat region proportionally wider - but the usable radius still comes from a measured or FEMM field map plus orbit-excursion and clearance checks, not from a fixed edge offset.
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When both H+ and H2+ are present, COLUMBUS plans the RF so both species come into resonance by changing the FIELD rather than the frequency - at fixed 2.82 MHz, protons resonate near 185 mT and H2+ near 370 mT - the book judging it easier to double the field than the frequency.
f_cyc = (q/m)*B/(2*pi) ; H2+ needs 2*B of H+ at the same fSource quote & editorial note
Es ist nämlich leichter, das Magnetfeld von 185 mT auf 370 mT zu erhöhen als die Frequenz von 2,82 MHz auf 5,64 MHz [tr.: easier to raise B from 185 to 370 mT than f from 2.82 to 5.64 MHz]
Editorial note, tabletop extrapolation: A fixed-frequency resonator plus a 2:1 field range covers both hydrogen species IF the machine works at both fields - field quality, source output and capture must each hold at both points, so verify rather than assume. Two peaks at B and 2B are consistent with H+/H2+ but not unique to them (q/m degeneracy, dg-1432); use them as a species INDICATION to confirm.
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A lower RF frequency proved easier to tune on this machine: the as-built experience was that the pi-filter matchbox into the high-impedance dee was more tractable at 2.82 MHz than at 5.64 MHz - the book attributes the choice to the better tunability of the RF system at the lower frequency.
Source quote & editorial note
Dies ist auf die bessere Abstimmbarkeit des HF-Systems bei der kleineren Frequenz zurückzuführen [tr.: due to the better tunability of the RF system at the lower frequency]
Editorial note, tabletop extrapolation: When species choice leaves a frequency option open, tunability is a legitimate tiebreaker - established by trying both on YOUR network, not by a frequency ceiling: evaluate component Q, circulating current and voltage stress at each candidate. Documenting lead inductance and stray capacitance pays regardless of frequency.
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Record operating points by species and status: at B0 = 370 mT protons resonate at 5.64 MHz (~32 keV at full radius) while H2+ - whose period is twice as long - needs 2.82 MHz (~16 keV); the published experiments run at 2.82 MHz with 1000 V amplitude, the proton runs at roughly half the design field (~187 mT peak).
370 mT: H+ at 5.64 MHz (~32 keV) OR H2+ at 2.82 MHz (~16 keV) - same radius, species-dependent frequency; operated: 2.82 MHz / 1000 V; ~187 mT peak for the proton experimentsSource quote & editorial note
Mit einer Beschleunigungsspannung der Frequenz von 5,64 MHz werden Protonen in einem Magnetfeld von B0 = 370 mT resonant beschleunigt. Unter diesen Bedingungen wäre für die H2+-Ionen die Umlaufdauer doppelt so groß; sie würden dann den ersten Halbkreis im Dee nicht phasenrichtig zum elektr. Wechselfeld verlassen. ... Als Frequenz der Beschleunigungsspannung wählt man 2,82 MHz mit 1000 V Amplitude [tr.: at 5.64 MHz accelerating frequency, protons are resonantly accelerated in a 370 mT field; under these conditions the H2+ orbital period would be twice as long and they would leave the first semicircle out of phase; for the accelerating voltage one chooses 2.82 MHz with 1000 V amplitude]
Prechtl & Wolf, Das Lehr-Zyklotron COLUMBUS — Mit einem Teilchenbeschleuniger Physik und Technik erleben, Springer (2020) — p. 37-39, 70-71
Editorial note, tabletop extrapolation: The design-vs-operated distinction this card exists for: conference-paper numbers are usually design values - cite measured operating points with their species and date, and never let one row imply a field-frequency pair serves two species at once.
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Dee voltage does not set the final energy (ideal on-crest model): the magnet and usable radius fix the ladder height, the voltage is the rung spacing - k = E_max/(q*U0) crossings, first-orbit radius r1 = sqrt(2*(q/m)*U0)/omega_cyc.
k = E_max/(q*U0) ; v1 = sqrt(2*(q/m)*U0) ; r1 = v1/omega_cycSource quote & editorial note
Die Endenergie der Ionen ist so etwas wie die Höhe einer Leiter und die Beschleunigungsspannung ist dann der Abstand der einzelnen Sprossen [tr.: final energy is the ladder height, voltage the rung spacing]
Editorial note, tabletop extrapolation: Recomputed for 1000 V protons at 185 mT: r1 = 24.7 mm, matching the book. A 150 keV machine at 1 kV needs 150 ideal crossings; at 5 kV only 30 - relaxing vacuum and field-error tolerance roughly in proportion. The idealization to keep visible: real voltage also moves capture, turn separation and whether the top rung is reachable at all (dg-1376's ceiling-vs-attainability).
-
The minimum dee amplitude is the one whose first orbit clears the ion source: on COLUMBUS, protons clear from U0 >= 200 V and H2+ from U0 >= 400 V on the first turn (r1 ~ 11 mm at their respective fields, against the 20 mm chimney region).
r1 = sqrt(2*m*U0/q)/B; clearance threshold U0_min ~ (B*r_clear)^2*(q/m)/2 (ideal full-qU0 first kick)Source quote & editorial note
Protonen ab U0 ≥ 200 V und H2+-Ionen ab U0 ≥ 400 V – bereits beim ersten Umlauf – hinreichend weit von der Ionenquelle entfernt [tr.: clear of the source from 200 V / 400 V on the first turn]
Editorial note, tabletop extrapolation: The scaling is the useful transfer: at 0.6 T and a 15 mm clearance radius the same ideal estimate gives ~3.9 kV for protons - so a sub-kV dee on a higher-field machine would NOT clear a 15-mm-class source housing under these assumptions; trace the actual source and gap geometry (launch phase, initial position, 3-D fields) before trusting the ideal number either way.
-
Bound the dee amplitude from above by the actual weakest insulator: on COLUMBUS the vacuum feedthrough's voltage rating limited U0 to <= 3000 V, and the matchbox output was designed to that bound.
U0_max = feedthrough ratingSource quote & editorial note
Aus Gründen der Spannungsfestigkeit der Durchführung ist U0 ≤ 3000 V [tr.: because of the feedthrough voltage rating, U0 <= 3000 V]
Editorial note, tabletop extrapolation: A 5-15 kV dee upgrade is an insulation-coordination problem across the WHOLE RF path - feedthrough, stem supports, matching capacitors, connectors, plus contamination and conditioning state - with the feedthrough a frequent but not guaranteed weakest link. Specify every element for peak RF plus any DC bias, in vacuum, with tracking margin.
-
The authors state that with dee voltages below 2-3 kV they are 'on the safe side' for students beside the machine. Editorial: this is the authors' judgment for their apparatus, not a measurement, and a regulatory exemption threshold (the 5 kV class for incidental emitters) is a legal boundary, not a physical one.
Source quote & editorial note
Mit Spannungen kleiner als 2–3 kV sind wir auf der sicheren Seite [tr.: with voltages below 2-3 kV we are on the safe side]
Editorial note, tabletop extrapolation: Electron energies equal to the dee voltage produce bremsstrahlung with end-point energy of the same value; at 3 keV any metal wall stops it, at 15-30 keV it does not, and stray electron currents in a multipacting dee are not bounded by the beam current. Flashover can also occur below 3 kV with bad geometry, pressure or contamination. Check, do not assume: evaluate the actual electrode potentials, survey with a suitable low-energy detector at operating power, and treat viewports and thin windows as the weak points.
-
Measure the dee input impedance before designing the RF chain: COLUMBUS's dee-plus-stem measured about 330 kOhm - and if that is the resonant parallel loss resistance, the acceleration power is tiny: P = U0^2/(2*R_p) = 6 W at 2 kV peak.
P = U0^2/(2*R_p) for U0 peak and R_p the resonant parallel loss resistance; at 10 kV into 330 kOhm, ~150 WSource quote & editorial note
Diese beträgt nach aktuellen Messungen ca. 330 kΩ [tr.: according to current measurements this is about 330 kOhm]
Editorial note, tabletop extrapolation: The scaling explains why a 100-500 W amplifier class suits a 5-13 kV dee - sized with margin: P_source >= U0^2/(2*R_p*eta) with measured end-to-end efficiency eta (matchbox, feedline and base-load losses all sit between amplifier and dee), and the larger dee's own R_p measured, not borrowed from this machine.
-
A marine HF transceiver is a workable multi-MHz RF source for a teaching cyclotron: COLUMBUS uses an ICOM M 600, delivering in H3E (AM carrier) mode a sine of ~70 V amplitude over 0.5-35 MHz, about 45 W into 50 ohm; such transmitters shut down without a load, so the matchbox input presents a resistive base load.
Source quote & editorial note
Der verwendete Transceiver, ein ICOM M 600, liefert in der Betriebsart H3E eine sinusförmige Spannung (Amplitude ≈ 70 V) im Frequenzbereich von 0,5–35 MHz mit einer abgegebenen Leistung von ungefähr 45 W an 50 Ω Ausgangsimpedanz. ... Das Widerstandsnetzwerk der Eingangsstufe stellt dabei eine Grundlast für den Transceiver dar. Dieser würde sonst [...] abschalten [tr.: the transceiver used, an ICOM M 600, delivers in H3E mode a sinusoidal voltage (amplitude ~70 V) over 0.5-35 MHz with about 45 W into 50 ohm output impedance ... the input resistor network is a base load; otherwise the transceiver shuts down]
Editorial note, tabletop extrapolation: The load-requirement lesson generalizes as a check, not a law: characterize the chosen amplifier's required load, mismatch tolerance and protection behavior (an LDMOS deck without foldback dies where the ICOM merely shuts down), and budget a dummy-load fraction plus a VSWR interlock so a detuned dee - a plasma flash, say - cannot damage the final stage.
-
Match 50 ohm to the cyclotron's measured ~330 kohm with a pi (Collins) filter: C1 with L tunes to the 50-ohm input while L with C2 produces the 330-kohm side, stepping ~70 V input to 2-3 kV at the dee; the filter is optimally matched when the directional coupler shows zero reflected power.
Source quote & editorial note
muss die niedrige Ausgangsimpedanz (50 Ω) der HF-Quelle an die hohe Eingangsimpedanz (330 kΩ) angepasst werden. Außerdem ist die Ausgangsspannung von 70 V auf 3000 V zu transformieren. Beide Aufgaben werden von der Koppelstufe oder Matchbox erledigt. ... C1 bildet mit L einen Filterkreis, der auf die Eingangsimpedanz von 50 Ω abgestimmt ist, während L mit C2 die Impedanz Z = 330 kΩ des Zyklotrons erzeugt. Und bei diesem Impedanzmatching wird gleichzeitig die Eingangsspannung von ca. 70 V auf 2–3 kV am Ausgang erhöht. ... Eine optimales Matching des Pi-Filters ist dann gegeben, wenn die reflektierte Leistung Null ist [tr.: the source's low 50-ohm output impedance must be matched to the high 330-kohm input impedance (a recent measurement gives ~330 kohm for the cyclotron), and the 70 V output stepped up to 3000 V - both jobs done by the coupling stage or matchbox; C1 with L forms a filter circuit tuned to the 50-ohm input while L with C2 produces the cyclotron's 330-kohm impedance, the input voltage rising from ~70 V to 2-3 kV at the output; the pi filter is optimally matched when the reflected power is zero]
Editorial note, tabletop extrapolation: Two independent readouts are the honest minimum for tuning: reflected power at the input AND a calibrated dee-voltage pickup at the output - zero reflected power alone proves the power went in, not that it reached the dee rather than the base load or network losses. The output-side capacitor must be RF-rated (the book's own footnote: an HF-tauglicher capacitor to avoid flashover), since kilovolts appear across it.
-
To switch a pi-filter resonator between two frequencies an octave apart, short a series inductor with a vacuum relay: COLUMBUS runs 24 uH + 8 uH in series (32 uH total) at 2.82 MHz; the relay shorts the 24 uH coil, leaving 8 uH for 5.64 MHz. An ordinary switch cannot be used at this node - the book requires a vacuum relay.
f = 1/(2*pi*sqrt(L*C)); L_total = 32 uH (2.82 MHz) or 8 uH (5.64 MHz) - consistent with ~100 pF effective C; expect retune after relay/lead parasiticsSource quote & editorial note
Mit Hilfe eines Relais kann die Spule mit L = 24 µH in Serie zu der 8 µH-Spule [geschaltet werden] ... Zieht das Relais an und schließt den Kontakt, wird die 24 µH-Spule kurzgeschlossen, so dass nun nur noch die Induktivität von 8 µH wirksam ist. ... kann für diese Umschaltung kein Schalter verwendet werden, vielmehr muss sie mit Hilfe eines Vakuumrelais erfolgen [tr.: a relay puts the 24 uH coil in series with the 8 uH coil; when the relay closes, the 24 uH coil is short-circuited so only 8 uH remains effective; no ordinary switch may be used for this switching - a vacuum relay is needed]
Editorial note, tabletop extrapolation: A 4:1 inductance ratio gives the 2:1 frequency ratio at nominally constant capacitance, covering H+ and H2+ on one network - as an ideal-LC starting point: relay contact capacitance and lead inductance shift both points, so retune and re-measure at each setting, and rate the relay for the RF voltage and current at its node.
-
Provide a DC bias socket coupled to the dee so an additional steady extraction voltage (Saugspannung) can be superimposed on the RF to help pull ions out of the source.
Source quote & editorial note
Über sie kann eine zusätzliche „Saugspannung“ an das Dee angeschlossen werden [tr.: through it an additional extraction voltage can be applied to the dee]
Editorial note, tabletop extrapolation: A DC extraction bias shifts when ions leave the slit relative to the RF phase - a real tuning knob. Determine its magnitude from ion-optics measurement or simulation on the actual source (the book states the provision, not a value), and rate the feedthrough and insulation for the maximum instantaneous RF-plus-DC sum, which also moves the bremsstrahlung end-point.
-
With a single-ended drive, the book's design shortens the grounded electrode into a dummy dee - since it sits at chamber potential, the region behind it is already field-free; the hot dee keeps its full depth.
ideal peak gap voltage: U0 (grounded counter-electrode) vs 2*U0 (opposite-phase push-pull at the same per-electrode amplitude U0)Source quote & editorial note
Da ein Dee wie die Vakuumkammer selbst auf Masse liegt, kann dieses Dee verkürzt werden [tr.: since one dee is at ground like the chamber, it can be shortened]
Editorial note, tabletop extrapolation: Single-dee-plus-dummy gives half the energy gain per turn of an ideal push-pull pair at the same per-electrode amplitude, in exchange for one feedthrough and one resonator - a trade that favors simplicity on most small builds; state the amplitude convention whenever quoting the factor of two.
-
COLUMBUS chose the accelerating gap and the dummy-dee depth as one common dimension - 20 mm each, 'on plausibility grounds' - the book posing the two dimensions as a single question when dimensioning the dummy dee.
gap = dummy-dee depth = dee aperture height = 20 mmSource quote & editorial note
Bei der Dimensionierung des Dummy-Dees stellt sich natürlich die Frage nach der Tiefe und der Größe des Beschleunigungsspalts gap. Aus Plausibilitätsgründen wurde jeweils ein Maß von 20 mm gewählt. [tr.: in dimensioning the dummy dee the question arises of its depth and the size of the accelerating gap; on plausibility grounds 20 mm was chosen for each]
Editorial note, tabletop extrapolation: A wide gap simplifies the source mount (the chimney sits inside it) at the cost of transit-time factor; choose the gap from the transit calculation - T = sin(x)/x with x = omega*g/(2v) over the actual injection and orbit velocities - rather than adopting either 20 mm or any other fixed number.
-
Size the vacuum from the mean free path: l = k_B*T/(p*sigma) with sigma = pi*(R1+R2)^2 - the book's hard-sphere table for hydrogen ions in NITROGEN, e.g. H2+ going more than 123 m between collisions at 1e-6 mbar, scaling inversely with pressure.
l_bar = k_B*T/(p*sigma) ; sigma = pi*(R1+R2)^2Source quote & editorial note
Bei einem Druck von p = 10−6 mbar [...] würden die H2+-Ionen (im Mittel) also erst nach mehr als 123 m auf ein Stickstoff-Molekül treffen [tr.: at 1e-6 mbar H2+ travels more than 123 m between collisions]
Editorial note, tabletop extrapolation: The table is a historical order-of-magnitude estimate with two labeled limitations: a hydrogen-FED machine's residual gas is mostly H2 (measure it - an RGA settles it), and the loss process that matters for beam survival is charge exchange, whose energy-dependent cross-section must come from evaluated data (dg-460), not hard spheres. Use lambda_loss(E) = 1/sum_j n_j*sigma_loss,j(E) over the actual partial pressures.
-
The book's vacuum criterion is a path-length condition: the mean free path of the accelerated ion must be at least the total spiral path length to final radius, s_ges = r1*pi*sum_{i=1..k} sqrt(i) + k*gap - so lower dee voltage (more turns) demands lower pressure.
l_bar >= s_ges = r1*pi*sum(sqrt(i), i=1..k) + k*gap (the source's criterion; note lambda = s means ~37% survival, not arrival)Source quote & editorial note
muss die mittlere freie Weglänge für die betreffenden Ionen größer oder gleich der gesamten Bahnlänge sein [tr.: the mean free path must be >= the total path length]
Editorial note, tabletop extrapolation: The qualitative lever is real - raising dee voltage shortens the spiral and relaxes the pump requirement - but pressure thresholds don't follow from radius and voltage alone: compute survival as exp(-integral n*sigma_loss(E) ds) with the charge-exchange cross-section for the actual species, gas and energies (dg-460's lesson), and pick pressure from an explicit acceptable loss fraction.
-
The book's worked vacuum trade for a 16 keV H2+ target at 4e-5 mbar (l ~ 3 m): 2000 V needs 8 crossings, 1000 V needs 16 crossings and 2.76 m of path, 'barely reached with 3 m'; below that the criterion fails before full energy. This is the source's attenuation CRITERION, not a hard reachability wall - at s = lambda the uncollided fraction is ~37%, and survival falls smoothly, so read the table as a loss budget.
k = E/(q*U0); s_ges(k) vs l_bar(p); survival = exp(-s/lambda) for constant lambda. Recomputed: r1 = 17.5 mm, sum sqrt(i) i=1..16 = 44.47 -> 2.45 m arcs + 0.32 m gaps = 2.76 m; at 2000 V the same geometry gives ~1.27 m arcs + 0.16 m gaps = ~1.43 m total. Caution: the bitmap Table 6.2 lists 2.44 m and 1.27 m - arcs only, without the k*gap term; use the text figure.Source quote & editorial note
Für 16 Beschleunigungen wären 2,76 m Weglänge erforderlich, die mit 3 m knapp erreicht werden [tr.: 16 accelerations need 2.76 m of path, barely reached with 3 m]
Editorial note, tabletop extrapolation: Recomputed: r1 = 17.5 mm, sum sqrt(i) for i=1..16 = 44.47, giving 2.45 m of arcs plus 16*0.02 = 0.32 m of gap = 2.76 m. Caution: the bitmap Table 6.2 lists 2.44 m and 1.27 m, i.e. arcs only without the k*gap term; use the text figure.
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Steady-state chamber pressure under deliberate gas feed follows from the pV-flow balance: p_E = q_G/S_eff - COLUMBUS's worked point, 300 mbar inlet at ~0.14 ml/min actual flow = 7.0e-4 mbar*l/s, over S_eff = 17.2 l/s, giving 4.1e-5 mbar against the measured 4.0e-5.
p = (q_process + q_background)/S_eff; q_process = p_inlet*Q_actual (actual volumetric flow) or p_std*Q_std (sccm-reading MFC) - one convention consistently; background = leaks + desorption, measured with feed offSource quote & editorial note
für einen Volumenstrom von ca. 0,14 ml/min sich ein Enddruck pE = 4,0 · 10−5 mbar einstellt [tr.: at about 0.14 ml/min a final pressure of 4.0e-5 mbar establishes itself]
Editorial note, tabletop extrapolation: The one-line balance is the first thing to validate against the gauge on a new machine - at several MFC settings, with the background term measured separately (feed off) and the flow convention of the actual controller pinned down before trusting any prediction.
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Never size from nominal pumping speed: 1/S_eff = 1/S_N + 1/G_L. COLUMBUS's 28 l/s (H2) turbo behind a 0.615 m DN40 line (G_L = 44.3 l/s for H2) delivers 17.2 l/s at the chamber - a 39% loss; for nitrogen (35 l/s nominal, G_L = 11.8 l/s) the loss is ~75%.
1/S_eff = 1/S_N + 1/G_LSource quote & editorial note
Allerdings darf für S nicht das Nennsaugvermögen SN = 28 l/s der Turbomolekularpumpe für Wasserstoff angesetzt werden [tr.: the nominal 28 l/s hydrogen speed of the turbo must not be used for S]
Prechtl & Wolf, Das Lehr-Zyklotron COLUMBUS — Mit einem Teilchenbeschleuniger Physik und Technik erleben, Springer (2020) — p. 52, 82-83
Editorial note, tabletop extrapolation: The lesson is the calculation, not a flange size: compute each line's conductance for each gas that matters and pick the port from the required chamber speed - short and fat wins, and mounting the pump directly on the chamber removes the term entirely. The 39/75% figures are this installation's; other lines and gases differ.
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Use the long-tube molecular-flow conductance G_L = (pi/12)*v_bar*D^3/L (valid for Knudsen number l/D >= 10 and L/D >> 1), obtained from the aperture conductance (pi/16)*v_bar*D^2 times the transmission probability (4/3)*D/L; v_bar is the mean thermal speed of the actual gas.
G_L = (pi/12)*v_bar*D^3/L; G_aperture = (pi/16)*v_bar*D^2; P_R = (4/3)*D/L; short tubes: C ~ [1/C_aperture + 1/C_long]^-1 or a Clausing factorSource quote & editorial note
Damit erhält man letztlich als Berechnungsformel für den Rohr-Strömungsleitwert: GL = π/12 v̄ D³/L [tr.: the working formula for tube conductance]
Editorial note, tabletop extrapolation: The D^3 dependence means a DN63 line has ~4x the conductance of DN40 at the same length (compute from actual bores - DN designations don't fix the ID). For short stubs (L/D < 10) the long-tube limit OVER-predicts - it diverges as L -> 0 - so cap it with the aperture term via the series combination.
-
Design the pumping chain for hydrogen, not air, when hydrogen is the feed: during source operation it is essentially only hydrogen being pumped - and the turbo's hydrogen speed (28 vs 35 l/s nominal here) and the line's hydrogen conductance (3.7x the air value) both differ from the air numbers.
v_bar = sqrt(8*R*T/(pi*M)) ; H2: 1.75 km/s, N2: 0.469 km/s at 293 KSource quote & editorial note
Dabei ist noch zu berücksichtigen, dass jetzt nicht mehr Luft, sondern im wesentlichen nur noch Wasserstoff H2 abgepumpt wird [tr.: it is now essentially only hydrogen that is pumped]
Editorial note, tabletop extrapolation: Take the H2 column from the pump datasheet and compute conductances with hydrogen's v_bar (1.75 km/s at 293 K vs 0.469 for N2). Terminology discipline: BASE pressure is the no-feed number; during source operation the relevant quantities are OPERATING pressure and residual composition - hydrogen-dominated when the feed throughput exceeds the measured background load.
-
Publish the gas-load trade as a table, as the book does: 0.10 / 0.15 / 0.20 ml/min hydrogen gave 2.9 / 4.4 / 5.8e-5 mbar and proton mean free paths of 12.6 / 8.4 / 6.3 m (H2+: 4.2 / 2.8 / 2.1 m); run at the lowest flow that still yields usable source current.
p_E proportional to V_dot_G ; l_bar proportional to 1/V_dot_GSource quote & editorial note
Für V̇G = 0,10 ml/min ergeben sich mittlere freie Weglängen von 12,6 m bzw. 4,2 m [tr.: at 0.10 ml/min the mean free paths are 12.6 m and 4.2 m]
Editorial note, tabletop extrapolation: Specify the feed instrument from the measured requirement: the flow range and step stability the source actually needs (state the reference conditions of the flow unit - sccm vs actual ml/min matters here), then choose a calibrated MFC or a precision metering valve with regulated upstream pressure accordingly. Table 7.2 is a bitmap in the scan; the pressure row recomputes exactly from p_E = 300 mbar * V_G / 17.2 l/s.
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COLUMBUS's two-stage pumping: an oil-free diaphragm backing pump takes the chamber from atmosphere to the ~1e-2 mbar class, where the turbomolecular pump takes over for the molecular regime - the book noting the backing pump can go no lower and the turbo continues from there.
Source quote & editorial note
Nun lässt sich mit der Vorpumpe der Druck nicht weiter erniedrigen. Die weitere Druckreduzierung erfolgt jetzt durch die Turbomolekularpumpe [tr.: the backing pump can go no lower; the turbo takes over]
Editorial note, tabletop extrapolation: The two-stage division of labor is standard but its numbers are technology-specific: take the crossover pressure and backing requirement from the high-vacuum pump's own specification (turbo, diffusion, cryo all differ - a diffusion stage wants a rotary-vane backer and a trap or baffle). An oil-free diaphragm backer keeps hydrocarbons out and is classroom-quiet - this machine's genuine transferables.
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No single gauge covers the nine-decade pressure range, so combine technologies: on COLUMBUS a Pirani (thermal-conductivity) head covers atmosphere down to its floor and a cold-cathode head takes over for high vacuum - the specific ranges, the Pirani's end-conduction/radiation floor mechanism, and placement limits being gauge-model matters to take from the manufacturer's data.
Source quote & editorial note
gibt es auch bei der Druckmessung kein Messgerät, das über den gesamten Druckbereich von neun Zehnerpotenzen messen kann [tr.: no single gauge covers the nine-decade range]
Editorial note, tabletop extrapolation: Both gauge types are gas-species dependent: a Pirani reads hydrogen differently from nitrogen and a cold cathode needs a hydrogen correction factor, so the pressure that enters the mean-free-path budget should always carry its gas correction; and keep magnetically sensitive heads out of the stray field or shield them per their spec.
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COLUMBUS's chamber as built: 200 mm diameter, ~100 mm tall, rolled from 2 mm wall stainless tube with a 5 mm stainless base carrying a 150 mm centring ring seating on the lower pole; ISO200 flange lid on four claw clamps; ten radial ports.
Source quote & editorial note
ist aus einem Edelstahlrohr mit Wandstärke 2 mm gefertigt. Der Boden, ebenfalls aus Edelstahl, hat eine Dicke von 5 mm [tr.: made from 2 mm wall stainless tube with a 5 mm base]
Editorial note, tabletop extrapolation: Historical construction data, not a thickness table: a chamber's wall, lid, base, clamp and port loads get an external-pressure buckling and plate calculation (or validated FEA) for the actual geometry and alloy - a 300 mm evacuated lid alone carries ~7 kN of atmosphere. The transferable advice that survives: port count is the main regret driver on small chambers, so allocate spares.
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Quote which mean-free-path form a number uses: the stationary-background form l = 1/(n*sigma), or the Maxwell sqrt(2) form l = 1/(sqrt(2)*n*sigma) - the latter being the result for IDENTICAL molecules in a Maxwellian equilibrium gas, as the book applies it.
l = 1/(sqrt(2)*n*sigma) (identical-Maxwellian-gas result); fast ion in thermal gas: l ~ 1/(n*sigma_loss(E)) - the stationary form with the ENERGY-DEPENDENT loss cross-sectionSource quote & editorial note
Nach einem Ansatz von Maxwell wird dies durch einen Faktor √2 im Nenner berücksichtigt [tr.: following Maxwell this is accounted for by a factor sqrt(2) in the denominator]
Editorial note, tabletop extrapolation: For a beam ion crossing slow gas the stationary form is the better physical model (relative speed ~ ion speed) - but only with the right sigma: gas-kinetic hard-sphere values are not loss cross-sections, so a beam-loss budget needs sigma_loss(E) from evaluated data (dg-460), whatever the sqrt(2) bookkeeping.
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Hydrogen is the natural feed for a small machine: it ionises easily by electron impact, a 10 L / 10 bar disposable Hydrostick cartridge holds a small, cheap inventory, and both H+ and H2+ are produced. Its drawback, per the book, is relatively high permeation through hoses and cannulas, which particularly affects the ion source.
Source quote & editorial note
Ein Nachteil ist die relativ hohe Permeation von Wasserstoff durch Schläuche und Kanülen; dies betrifft insbesondere die Ionenquelle [tr.: a drawback is hydrogen permeation through hoses and cannulas]
Editorial note, tabletop extrapolation: Use metal lines with a mass-flow controller rather than elastomer tubing (PEEK is lower-permeation than elastomers, not zero). A small cartridge is still HYDROGEN: even ~10 standard litres forms a flammable mixture in air, so ventilate, leak-check, control ignition sources and handle the pressurized cartridge properly. Runtime: compute from the cartridge's usable standard volume at the actual MFC setting rather than quoting a lifetime.
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Gas-feed chain for a thermionic source, as built: cartridge -> pressure reducer to 300 mbar -> mass-flow controller at 0.10-0.20 ml/min -> directly into the source chimney; the reducer pressure enters the book's gas-load balance q_G = 300 mbar * V_dot_G, with V_dot the ACTUAL volumetric flow at the reducer pressure.
q = p_in * Q_actual (actual inlet volume) or q = p_std * Q_std for an MFC reading sccm - one convention, consistently; mixing 300 mbar with an sccm reading understates throughput ~3.4xSource quote & editorial note
Dieser Druck wird durch einen Druckminderer auf pH2 = 300 mbar reduziert [tr.: the pressure is reduced by a regulator to 300 mbar]
Editorial note, tabletop extrapolation: Fix the reducer pressure and log it - it is a term in the balance. Whatever meters the flow, state its reference conditions and take accuracy and repeatability from its specification rather than assuming a resolution.
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Thermionic chimney source construction, as built: a 0.3 mm thoriated-tungsten filament in a machinable Shapal ceramic body, a copper anode plate with a hole above it, electrons entering the chimney formation space, and the chimney closed by a ceramic lid carrying an insulated tungsten disc - an 'electron mirror' that charges negative and reflects electrons back for further ionisation, which the book says noticeably raises the electron count and ion current.
Source quote & editorial note
Die für die Ionisation notwendigen Elektronen treten aus dem glühenden Filament, einem thorierten Wolframdraht mit Durchmesser von 0,3 mm aus. Dieses befindet sich in einem Keramikkörper aus Shapal. Darüber liegt eine Kupferplatte als Anode. ... Durch ein Loch in der Anode treten die Elektronen in den Formationsraum eines sog. 'Kamins' ein ... Der Kamin wird durch einen Keramikdeckel abgeschlossen, an dem sich isoliert eine Wolframscheibe, ein sog. Elektronenspiegel, befindet. Dieser lädt sich durch die auftreffenden Elektronen negativ auf und reflektiert sie in den Formationsraum des Kamins, so dass sie für erneute Ionisationsprozesse zur Verfügung stehen. Auf diese Weise erhöht sich die Zahl der Elektronen und damit auch der Ionenstrom merklich. [tr.: the electrons emerge from a glowing 0.3 mm thoriated tungsten filament seated in a Shapal ceramic body; above it lies a copper plate as anode; through a hole in the anode the electrons enter the formation space of a 'chimney'; the chimney is closed by a ceramic lid carrying an insulated tungsten disc, an 'electron mirror', which charges negative from incident electrons and reflects them back into the formation space for further ionisation - noticeably raising the electron count and with it the ion current]
Editorial note, tabletop extrapolation: The floating electron mirror is a zero-cost reflex trick - no second cathode, no supply - that increases electron residence time; the book claims a noticeable ion-current gain, not a quantified one, so measure yours. Shapal (AlN-BN) machines with ordinary tools, unlike alumina - verify the grade's temperature rating against the filament environment.
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Run the source anode near the book's stated ion-yield maximum: it reports the number of ions formed peaking at 100-150 eV electron energy - beyond that interval the electrons are 'quasi too fast' and the rate falls - so the anode voltage is set to ~120-150 V. [Note: standard evaluated H2 electron-impact ionisation data put the broad maximum nearer 70-100 eV; the book's 100-150 eV band reads as its source's empirical optimum, which also folds in geometry and sheath effects.]
U_B = 100-150 VSource quote & editorial note
Die Anzahl der gebildeten Ionen hängt aber auch von der Elektronenenergie ab. Sie erreicht bei 100–150 eV ein Maximum [tr.: ion yield depends on electron energy, peaking at 100-150 eV]
Editorial note, tabletop extrapolation: Sweep anode voltage against extracted ion current on the actual source - the optimum is broad and machine-specific, anode volts are not electron collision energy volt-for-volt (sheaths and where ionisation happens intervene), and a current-limited 0-200 V supply covers the whole plausible band.
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Estimate source output from I_ion = sigma * I_e * l_e * p_H with sigma the differential ionisation coefficient (order 1-3 per cm*mbar for hydrogen), I_e the emission current, l_e the electron path, p_H the local hydrogen pressure - a first-order production estimate, not a bound.
I_ion = sigma * I_e * l_e * p_H ; sigma ~ 1-3 /(cm*mbar)Source quote & editorial note
Der differentielle Ionisierungswirkungsquerschnitt σ liegt in der Größenordnung von 1–3 1/(cm·mbar) [tr.: the differential ionisation coefficient is of order 1-3 per cm mbar]
Editorial note, tabletop extrapolation: Compare with measurement honestly: at 2-5 mA emission the sigma=1 estimate gives ~0.3-0.7 uA against measured 1-3 uA - a factor of a few, not an order of magnitude, and the gap closes further once the CHIMNEY pressure (well above chamber pressure) and the sigma range are used. The formula omits extraction efficiency and losses in both directions - calibrate it per source rather than reading it as floor or ceiling.
-
Do not chase ion current with filament heating: more heater current raises emission but heats the chamber - the book says the higher heater power raises chamber temperature and worsens the vacuum - and shortens filament life; COLUMBUS accepts a compromise operating point around 7-10 A.
Source quote & editorial note
Außerdem steigt durch die größere Heizleistung die Temperatur in der Vakuumkammer, was zu einer Verschlechterung des Vakuums führt [tr.: higher heater power raises chamber temperature and worsens the vacuum]
Editorial note, tabletop extrapolation: Log heater current against the vacuum gauge to find the knee for the actual source - the transferable procedure. Filament-life sensitivity to temperature is steep (evaporation-limited life, dg-379's tables) but the '10% hotter halves life' shorthand has no source here and current is not temperature; work from the W evaporation tables at the actual filament temperature if a lifetime estimate matters.
-
A coiled filament (3-5 turns, as on COLUMBUS) generates its own magnetic field that binds part of the emitted electron cloud by the Lorentz force, so not all emission reaches the chimney.
Source quote & editorial note
Bei einer Spulengeometrie (3–5 Wdg. wie bei Columbus) erzeugt dieses ein Magnetfeld, das die Elektronen infolge der Lorentz-Kraft bindet [tr.: a 3-5 turn coil produces a field that binds the electrons]
Editorial note, tabletop extrapolation: When comparing source geometries (coil vs hairpin vs straight, AC vs DC heating), meter EMISSION at the anode, not filament current - the self-field confinement is one reason the two differ. To estimate the self-field, B ~ mu0*N*I/(2R) needs the coil radius, not just turns and current; compute it against the electron Larmor radius at the actual energy before crediting or blaming it.
-
The cyclotron guide field itself boosts source output: the book reports collision rate and ion current rising with B (their Fig. 8.5, 0-160 mT), then an 'interesting' fall above ~160 mT, which the authors explain as the plasma column narrowing further and moving away from the extraction slit, lowering the extraction field strength there - the authors' own proposed mechanism ('could be'), not a demonstrated one.
I_ion(B) rises to ~160 mT then falls (measured)Source quote & editorial note
Somit erhöht sich die Stoßrate und damit auch der Ionenstrom mit zunehmender magnetischer Flussdichte, wie Abb. 8.5 für 0 ≤ B ≤ 160 mT zeigt. Interessant ist der Abfall des Ionenstroms bei Magnetfeldern größer als ca. 160 mT. Eine Erklärung hierfür könnte darin liegen, dass sich die Plasmasäule nun noch weiter verengt und sich damit weiter vom Extraktionsschlitz entfernt. Dadurch sinkt die Extraktionsfeldstärke in diesem Bereich und der Ionenstrom nimmt wieder ab. [tr.: the collision rate and hence the ion current rise with increasing flux density, as Fig. 8.5 shows for 0-160 mT; interesting is the drop of ion current above about 160 mT - one explanation could be that the plasma column narrows further and moves away from the extraction slit, lowering the extraction field strength there so the ion current falls again]
Editorial note, tabletop extrapolation: On a higher-field machine expect the optimum to sit elsewhere: scan source output against B and against slit position empirically. The narrowing-column picture predicts alignment sensitivity grows with field - a hypothesis worth testing with a slit-position scan, not a sub-millimetre tolerance to design to in advance.
-
Extraction geometry for a chimney source in a single-dee machine: a narrow slit on the chimney side facing the dee, two puller electrodes attached to the dee, ions leaving on the negative half-wave only. No counter-beam forms on the positive half-wave because the chimney sits at dummy-dee (ground) potential and has no slit facing the dummy dee.
Source quote & editorial note
Zu diesem Zweck wurden an dem Dee zwei Extraktions- bzw. Pullerelektroden angebracht. Nun bleibt noch die eingangs gestellte Frage zu klären, warum kein zweiter Ionenstrahl während der positiven Halbwelle entsteht. Ein Grund dafür ist die Tatsache, dass die Ionen nur aus dem Schlitz extrahiert werden können, der dem Dee gegenüberliegt. Ein weiterer Grund ist das Potenzial des Kamins, das das gleiche ist wie das des Dummy-Dees, nämlich Masse. Somit könnten auch während der positiven Halbwelle der Beschleunigungsspannung keine Ionen in das Dummy-Dee extrahiert werden. [tr.: two extraction/puller electrodes were fitted to the dee; the question why no second ion beam forms during the positive half-wave is answered by two reasons - ions can only leave through the slit facing the dee, and the chimney sits at the same potential as the dummy dee, namely ground, so no ions can be extracted into the dummy dee during the positive half-wave]
Editorial note, tabletop extrapolation: Grounding the chimney with a one-sided slit answers the reverse-beam question students raise - by construction on this machine. If the source is biased instead, the slit-to-puller spacing, the bias polarity and the counter-beam question all reopen: analyze, don't assume.
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Verified thermionic-source operating point on COLUMBUS: 7 A heater, 120 V anode, 2 mA emission at 0.10-0.15 ml/min hydrogen (the broader 7-10 A / 120-150 V / 2-5 mA window and the one-year filament life come from the bitmap Table 8.1 and await transcription against the page image).
I_heater 7-10 A ; U_B 120-150 V ; I_e 2-5 mA ; I_ion 1-3 uASource quote & editorial note
Bei einem Heizstrom von 7 A und einer Anodenspannung von 120 V fließt ein Emissionsstrom von 2 mA [tr.: at 7 A heater and 120 V anode, 2 mA emission flows]
Editorial note, tabletop extrapolation: A 0.3 mm thoriated-tungsten filament at these currents is receiver-tube-heater class in POWER - but the supply is not casual: it must be current-regulated with cold-start limiting (cold filament resistance is a fraction of hot), galvanically isolated and rated to float at the source bias with RF superimposed, through a feedthrough rated for both. Spec those before reaching for any bench supply.
-
A Faraday cup for a few-keV internal beam is a shielded metal beaker with a narrow entrance slit reading pA to nA through a sensitive amplifier; secondary-electron emission inflates the reading, which is acceptable when only the presence and field position of a peak matter, but any absolute current measurement needs a suppressor or bias.
Source quote & editorial note
Diese vergrößern den gemessenen Strom und verfälschen damit das Signal. Dies spielt im vorliegenden Fall jedoch keine Rolle [tr.: these inflate the measured current; irrelevant in the present case]
Editorial note, tabletop extrapolation: Secondary-electron emission inflates an unsuppressed cup's reading - fine when only the PEAK POSITION matters (the book's own point), not fine for absolute current: the yield depends on species, energy, angle and surface, so either suppress (dg-524), verify a current-vs-bias plateau, or state 'unsuppressed' beside every quoted beam current. No universal yield number exists to correct by.
-
COLUMBUS's home-built Faraday cup (no suitable commercial size existed): a double-sided PCB with one copper side as the shield, a box-shaped bent copper cup soldered to the other side, mounted on semi-rigid coax whose core is the signal line - the cable doubling as the guide rod that moves the cup radially, carrying the signal to the amplifier with low loss.
Source quote & editorial note
Bei dem in Columbus verwendeten Faraday-Cup handelt es sich um einen Selbstbau, da ein Cup passender Größe nicht verfügbar war. Auf eine doppelseitige Platine, dessen eine Seite die Abschirmung darstellt, wurde auf der anderen Seite ein schachtelförmig gebogenes Kupferteil angelötet. Diese Anordnung ist auf ein sog. Semirigid-Kabel montiert, dessen Seele die Signalleitung bildet und das Detektorsignal verlustarm an den Verstärker weiterleitet und das gleichzeitig als Führungsstange dient, mit der der Cup in radialer Richtung bewegt werden kann. [tr.: the COLUMBUS Faraday cup is home-built since no suitable size was available: onto a double-sided PCB whose one side forms the shield, a box-shaped bent copper piece is soldered on the other side; the assembly is mounted on a semi-rigid cable whose core forms the signal line, carrying the detector signal to the amplifier with low loss and simultaneously serving as the guide rod by which the cup is moved radially]
Editorial note, tabletop extrapolation: A movable shielded probe from PCB stock and semi-rigid coax is genuinely cheap and buildable in an afternoon - qualify it in place: vacuum-compatible feedthrough for a SLIDING cable, dark-current check with beam off, short exposed centre conductor and clean PCB edges so leakage doesn't swamp pA signals.
-
COLUMBUS mounts its Faraday cup at less than 90 degrees to the dummy dee because at the detection radius the ions already move on the field-curved semicircle - a cup face square to the dee edge would see the beam obliquely.
Source quote & editorial note
Aus diesem Grunde ist der Faraday-Cup unter einem Winkel von weniger als 90◦ gegen das Dummy-Dee montiert [tr.: the Faraday cup is mounted at less than 90 degrees to the dummy dee]
Editorial note, tabletop extrapolation: The transferable move: orient the cup entrance normal to the LOCAL ORBIT TANGENT at the radius where the probe sits - computed or ray-traced for the actual field polarity and orbit (early displaced turns and spirals bend the simple theta-rotation picture) - and re-check whenever the probe moves radially.
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Identify the accelerated species by specific charge without extraction: hold the RF fixed, ramp the magnet slowly (COLUMBUS: a 0.005 Hz triangle wave), plot Faraday-cup current against the Hall-probe field, and read candidate q/m values from the peak fields via q/m = 2*pi*f_RF/(h*B) with h the harmonic number (h=1 for fundamental operation).
q/m = 2*pi*f_RF/(h*B_eff), B_eff the orbit-relevant (calibrated, orbit-averaged) field; peaks are q/m CANDIDATES pending harmonic assignmentSource quote & editorial note
Wir legen uns also mit einem geeigneten Detektor auf die Lauer und verändern das Magnetfeld solange, bis wir ein Signal erhalten [tr.: lie in wait with a detector and vary the field until a signal appears]
Editorial note, tabletop extrapolation: Slow ramps help but don't grant immunity: characterize the electrometer/amplifier settling time and pick a sweep rate that resolves the narrowest expected peak - then confirm by comparing up- and down-sweeps (hysteresis and lag shift peaks in opposite directions). Correct the Hall reading to the median plane: a probe in the lid recess reads a different field than the orbit (the 1-7.5 percent class errors below), which moves every q/m assignment.
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Measured I(B) spectrum at 2.82 MHz / 1000 V: peaks at ~187 mT and ~370 mT, from which the book itself computes specific charges - Peak 1 giving q/m = 9.48e7 As/kg (1 percent below the proton literature value), Peak 2 giving half that, which the book assigns to H2+.
q/m = 2*pi*f/BSource quote & editorial note
Der erste Peak erscheint bei einer Flussdichte von ca. 187 mT, der zweite kleinere bei B = 370 mT. Somit ergibt sich für Peak 1 eine spezifische Ladung von [2*pi*2.82 MHz/0.187 T] [tr.: the first peak appears at about 187 mT, the second smaller at 370 mT; from this, Peak 1 yields a specific charge of ... - the book carrying the assignment computation itself]
Editorial note, tabletop extrapolation: On a 9 MHz machine the corresponding fields are 0.59 T (H+) and 1.18 T (H2+). A pair of peaks at B and exactly 2B is strong evidence CONSISTENT WITH H+/H2+ - not unique proof (D+ shares H2+'s q/m) - so confirm by frequency scaling or an independent species diagnostic before certifying the beam.
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Expect possible extra peaks at B0/3, B0/5, ... below a species' main peak: the book notes ions that happen to carry 1/3, 1/5, ... of the maximum velocity are also resonantly accelerated - odd-harmonic operation, omega_RF = k*omega_cyc with k odd.
B = (v/v0)*B0 for v = v0/3, v0/5, ... ; omega_RF = k*omega_cyc, k oddSource quote & editorial note
Ionen, die zufällig 1/3; 1/5; ... der Maximalgeschwindigkeit haben, werden jedoch ebenfalls resonant beschleunigt [tr.: ions with 1/3, 1/5 ... of the maximum velocity are also resonantly accelerated]
Editorial note, tabletop extrapolation: Odd reciprocal-field peaks are CANDIDATES for harmonic operation - same species, same probe radius assumed - and whether they are detectable depends on capture and gap geometry; treat them as one hypothesis in the peak ledger (dg-1426), not something every machine must show.
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Distinguish 'direct ions' from accelerated beam: ions never resonantly accelerated can fly a single semicircle from source to cup at the field where (1/2)(q/m)(B*rho)^2 equals their starting energy - the book's own calculation, with B = 0.165 T and its r = 25 mm entering AS THE GYRORADIUS, gives the Table 9.1 voltages (~808 V for H+, ~404 V for H2+; our recomputation 815/407 V, rounding).
U = (1/2)*(q/m)*(B*rho)^2 with rho the GYRORADIUS. Geometry caution: a semicircle from a central source displaces the ion by 2*rho, so if the 25 mm is actually the source-to-cup DISTANCE, rho = 12.5 mm and the voltages are 4x lower (~204/102 V) - the book does not state which; resolve against the apparatus drawing before reusing the numbers.Source quote & editorial note
Peak 2 kann dadurch zustande kommen, dass der betreffende Ionenstrahl direkt in nur einem Halbkreis [...] in den Faraday-Cup gelenkt wird [tr.: peak 2 may arise from ions steered directly into the cup in one semicircle]
Editorial note, tabletop extrapolation: On any machine, pull the probe beyond the single-semicircle reach before calling a peak resonant beam, and treat a peak that tracks sqrt(U0) as a direct-ion suspect - a clue, valid where the direct ions' starting energy actually scales with dee voltage.
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Interpreting the smaller peaks 'is not always possible nor simple' (the book's own caution): the sinusoidal RF spreads effective accelerating voltage and arrival velocities, broadening the response - one contributor among several to the forest of small unassigned peaks.
Source quote & editorial note
Die Deutung der anderen, kleineren Peaks [...] ist nicht immer möglich und auch nicht ganz einfach [tr.: interpreting the other smaller peaks is not always possible nor simple]
Editorial note, tabletop extrapolation: Keep a running peak ledger (B, f, U0, gas flow, probe radius) across runs. Persistence at fixed B across U0 and flow changes is EVIDENCE toward species/harmonic assignments, and motion is evidence toward phase-spread or direct-ion artefacts - evidence, not a classification: confirm with frequency scaling and probe-radius scans (dg-1422, dg-1425).
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Water-cool a kW-class laboratory magnet with a closed loop, as COLUMBUS's student-built system does: a central-heating circulator providing ~10 l/min, an expansion vessel holding ~1 bar operating pressure, and a cooling-failure interlock that switches the magnet off via an emergency switch.
Source quote & editorial note
Im Betrieb müssen die Spulen des Magneten mit Wasser gekühlt werden. Dies geschieht durch ein (von Schülern selbst entwickeltes) Kühlsystem, das mit Hilfe einer Heizungspumpe für den notwendigen Durchfluss von ca. 10 l/min sorgt. Ein Druckausgleichsgefäß stellt den notwendigen Betriebsdruck von ca. 1 bar während des Betriebs her. Sollte das Kühlsystem einmal ausfallen, so wird der Magnet über einen Notschalter abgeschaltet. [tr.: in operation the magnet coils must be water-cooled, by a student-built cooling system whose central-heating circulator provides the necessary ~10 l/min flow; an expansion vessel maintains the ~1 bar operating pressure; should the cooling fail, the magnet is switched off by an emergency switch]
Editorial note, tabletop extrapolation: Size cooling from the measured coil loss, allowable winding temperature and coolant temperature rise - the 10 l/min is this magnet's number. A fail-safe interlock (flow AND winding temperature, arranged so failure trips rather than merely alarms) is cheap against a coil rewind; whether an air-cooled coil set needs duty cycling depends on its thermal design, not its power class.
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Instrument the guide field with a fixed Hall probe whose controller outputs a voltage proportional to B, used directly for evaluation - on COLUMBUS the probe sits at the chamber-lid centre (in the pole recess, dg-1381) and the proportional output drives the I(B) recording.
Source quote & editorial note
Ein Steuergerät liefert eine zur Flussdichte proportionale Spannung, die für die weitere Auswertung verwendet wird [tr.: a controller supplies a voltage proportional to B used for evaluation]
Editorial note, tabletop extrapolation: A fixed probe reads ITS OWN location's field, not the median plane's: map the probe output against a median-plane measurement across the full operating range and both ramp directions (saturation and hysteresis bend the relation), fit the transfer curve, and carry its uncertainty into every specific-charge assignment - a one-point offset calibration is the minimum, not the goal.
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The book states that physics and mathematics at class-11 (upper-secondary) level 'should be sufficient' to follow its presentation - each subsystem chapter opening with a student-teacher dialogue and closing with the quantitative dimensioning and a worked numbers table.
Source quote & editorial note
Physik- und Mathematik-Kenntnisse auf dem Level der 11. Klasse der Oberstufe sollten ausreichend sein [tr.: physics and maths at class-11 level should suffice]
Editorial note, tabletop extrapolation: The chapter template (dialogue, then formula, then a per-subsystem results table) is a ready-made lesson structure for an educational accelerator - our reading of the book's organization, worth copying deliberately; the author's 'should suffice' keeps its hedge.
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The educational case for a real cyclotron: it appears in nearly every upper-secondary textbook, students can calculate it in detail, yet almost none has seen one - and the book's stated challenge was getting a cyclotron running in exactly this low-energy range so students can study it while it runs.
Source quote & editorial note
Die Herausforderung dieses Projekts bestand demnach darin, ein Zyklotron in diesem niedrigen Energiebereich zum Laufen zu bringen [tr.: the challenge was to get a cyclotron running in this low energy range]
Editorial note, tabletop extrapolation: Define the teaching machine's safety envelope explicitly rather than declaring it hazard-free: maximum electrode potential (X-ray endpoint), ion species and energy (reaction thresholds - remembering exothermic channels like D-D have none, so deuterium is a different machine), beam current, target and contaminant composition, plus the ordinary electrical, RF, vacuum and stored-energy hazards that exist at ANY energy. Survey, don't assume; the low-energy regime shrinks the radiological terms, not the list.
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A teaching machine need not extract the beam - the book's point exactly: 'the particle beam does not even need to be extracted' - an internal probe, species identification by specific charge, and a visible running accelerator met the project's pedagogical objectives.
Source quote & editorial note
Der Teilchenstrahl braucht dabei nicht einmal ausgelenkt zu werden [tr.: the particle beam does not even need to be extracted]
Editorial note, tabletop extrapolation: A radial probe drive with a Faraday cup is the first detector to build on any small machine, and extraction is properly a separate later project - which, when undertaken, teaches its own lessons (septum design, transport, external diagnostics; the COLUMBUS Wien-filter plan, dg-1512, is that next chapter). Wait until internal beam is reproducible across days.
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Frame the first beam experiment as a replica of the classic specific-charge measurement - 'the specific charge is a particle's identity card' - measuring q/m = 2*pi*f_RF/(h*B) on the internal beam at known RF frequency (h the harmonic, 1 for fundamental).
q/m = 2*pi*f/BSource quote & editorial note
Die spezifische Ladung ist sozusagen der Personalausweis eines Teilchens. Wenn wir diese kennen, kennen wir auch das Teilchen [tr.: specific charge is a particle's identity card]
Editorial note, tabletop extrapolation: Connecting to the e/m fine-beam tube students already know turns first beam into an assessable experiment with a literature value and a computable error - the PROTON value being 9.58e7 C/kg. Teach the degeneracy honestly: q/m alone does not name the particle (D+, H2+ and He2+ all sit near 4.8e7 C/kg), so the identity card needs the source-gas and charge-state context too (dg-1422's candidate discipline).
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Measure a pedagogical build by what follows first beam - the book poses its own test ('when would COLUMBUS not have been worth it?') and answers: 'certainly the project would not have been worth it had it ended after the successful conclusion in 2014' - the value lying in the years of workshops, teacher training, and continuous improvement since.
Source quote & editorial note
Sicher hätte sich das Projekt nicht gelohnt, wenn es nach dem erfolgreichen Abschluss im Jahre 2014 beendet worden wäre [tr.: the project would not have been worth it had it ended in 2014]
Editorial note, tabletop extrapolation: The listed follow-on improvements (magnet stand, acceleration simulation, probe translator, mechanical model) are the kind of second-year items a small-machine program should schedule rather than improvise - as this case study's pattern, adapted to local aims, not a universal checklist.
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The COLUMBUS authors could draw only partly on earlier amateur and student cyclotrons (Niell, Dewan, Steiger, Baumgartner/Heuer, Koeth's Rutgers work) - 'the boundary conditions were too different'.
Source quote & editorial note
Trotzdem konnten wir nur bedingt auf bereits gemachte Erfahrungen zurückgreifen. Zu unterschiedlich waren die Voraussetzungen [tr.: prior experience was only partly usable; conditions were too different]
Editorial note, tabletop extrapolation: The transferable layer across amateur machines is the METHOD - dependency diagram, rigidity sizing, vacuum chain, species-by-q/m - not the numbers: copy the method, recompute every quantity for your own boundary conditions. (Which differences blocked reuse here isn't itemized in the quote; the lesson survives without the itemization.)
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The spiral path-length formula assumes a homogeneous field perpendicular to the orbit plane and zero field in the gap (straight crossings): radii scale as r_i = r1*sqrt(i), giving s_ges = r1*pi*sum(sqrt(i), i=1..k) + k*gap.
s_ges = r1*pi*sum(sqrt(i)) + k*gap; approximation sum(sqrt(i)) ~ (2/3)k^1.5 + (1/2)k^0.5 (the bare (2/3)k^1.5 underestimates); compute k from the actual energy gain per crossingSource quote & editorial note
Diese Gleichung gilt allerdings nur unter folgenden Voraussetzungen [tr.: this equation holds only under the following assumptions]
Editorial note, tabletop extrapolation: Evaluate the sum numerically for your actual k (from injection energy, final energy and effective gain per crossing - higher voltage means FEWER crossings for the same energy); phase slip and gap curvature make the real path longer than the formula, so add margin before comparing with the mean free path.
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Resonant acceleration requires omega_RF = k*omega_cyc with k odd (1, 3, 5, ...); the fixed-frequency property (period independent of radius and velocity) holds while the accumulated phase slip from gamma - 1 stays acceptable for the chosen turn count and phase window - at 0.1c the frequency is already ~0.5% low, which may or may not matter depending on turns.
T = 2*pi*m/(q*B) ; omega_RF = k*(q/m)*B, k = 1, 3, 5, ...Source quote & editorial note
ωHF = k · ωZyk = k · v/r = k · (q/m) B mit k = 1; 3; 5; ... [tr.: RF frequency equals an odd multiple of the cyclotron frequency]
Editorial note, tabletop extrapolation: Third-harmonic operation (k = 3) lets a 0.2 T magnet accelerate protons with a 9 MHz resonator, at the cost of a narrower phase window per crossing; it is the formal basis of the sub-harmonic peaks in I(B) spectra (dg-1424).
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Data-sheet benchmark for a surplus laboratory electromagnet of the class suited to a few-keV teaching cyclotron (per the reproduced Bruker BE-15 table - bitmap, not text-verifiable): 150 mm pole diameter, 5-100 mm adjustable gap, 430 kg, 2 x 800 turns at ~1.4 ohm per coil. Consistent series-connection operating points: 20 A gives 32 kAT and ~1.1 kW (cold); 15 A gives 24 kAT and ~0.6 kW; the book reads 300-400 mT off its chart at its operating current with the 75 mm gap.
series coils: NI = 1600*I; P = I^2*(2*1.4 ohm) cold. Ideal gap-MMF lower bound: B*g/mu0 = 22 kAT for 370 mT across 75 mm - a floor, real magnets need more; the chart, not the formula, is the datumSource quote & editorial note
Aus dem Diagramm 5.1 liest man für diesen Strom einen Wert zwischen 300–400 mT für die Flussdichte ab [tr.: for this current one reads 300-400 mT off Chart 5.1]
Editorial note, tabletop extrapolation: A home H-frame with 20 cm poles and a 3 cm gap reaches ~0.6 T with 15-20 kAT, so this surplus-magnet class is a legitimate alternative to winding your own - check the actual coil topology (series vs parallel feeds change the current arithmetic) and take B from a measurement or the manufacturer's chart at YOUR gap.
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Use a mass-flow-controlled feed and the steady-state pressure as a CONSISTENCY check of the vacuum model: COLUMBUS's measured chamber pressure agreed well with p_H2*V_G/S_eff at its operating point.
S_eff(in-situ) = delta-q / delta-p: step a calibrated throughput onto a steady baseline, apply the gauge's hydrogen correction, and divide - a differential measurement that separates the background termSource quote & editorial note
ein Wert der in guter Übereinstimmung mit dem gemessenen Druck steht [tr.: a value in good agreement with the measured pressure]
Editorial note, tabletop extrapolation: One-point agreement checks consistency; to actually MEASURE the pump stand's hydrogen speed at the chamber, do the differential version (baseline, step the flow, gauge-corrected delta-p) and repeat after every plumbing change or pump swap, logging the result.
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El Cerrito's chamber history: the first chamber - curved copper sheets clamped and gasketed around the magnet poles - made 1.5 uA but could not maintain vacuum; the replacement was a rigid ring, 16.5 cm brass tubing with two 0.3 cm steel plates, bottom soldered, top screwed down onto a rubber gasket - and with it the beam reached 7 uA.
Source quote & editorial note
The first attempted vacuum chamber was made of curved sheets of copper that clamped around the magnet's poles. Using gaskets to seal the chamber, the machine produced a beam current of 1.5 microamperes. However, the system could not maintain vacuum and a new design was sought. The modified chamber consisted of a section of 16.5 cm brass tubing used as the wall of the chamber, and two 0.3 cm thick circular steel plates as the top and bottom. The bottom plate was soldered to the brass, the top plate was screwed to the bottom plate with a rubber gasket between the brass and steel to form a seal.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 15
Editorial note, tabletop extrapolation: A rigid soldered ring with one permanently sealed plate and one demountable gasketed plate is a simple chamber architecture with this documented precedent; the conformal clamp-around-sheet chamber has a documented vacuum-failure precedent. (The survey doesn't cost either build - 'low-cost' is our reading of brass tube and hand tools.)
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A cyclotron can run with a single dee and no dummy dee, using the grounded chamber itself as the counter-electrode: El Cerrito did so and, with its second chamber, produced a 7 uA proton beam at 1,600 W operating RF power (2,000 W maximum available to the electrodes).
Source quote & editorial note
The El Cerrito Cyclotron used only one dee, and did not employ a 'dummy dee,' but rather held the chamber itself at ground. ... The system was operated at 1,600 watts and could provide a maximum of 2,000 watts to the electrodes. ... with the new vacuum chamber a beam of 7 microamperes was produced.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 15
Editorial note, tabletop extrapolation: Deleting the dummy dee simplifies the in-chamber assembly at the cost of a less-defined gap field; the precedent documents that the geometry can work at the microampere scale - it does not promise that current class, which came from the whole machine, not the electrode choice alone.
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Coil-winding scale datum for a small cyclotron magnet built by hand, approximately 8 km of 13-gauge copper wire wound on six-inch (15.2 cm) pole pieces (El Cerrito, reported built 1947 by high-school students).
Source quote & editorial note
Approximately 8 kilometers of 13 gauge copper wire were wound around the six inch pole pieces for the electromagnet.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 15
Editorial note, tabletop extrapolation: A concrete scale anchor - kilometre-class wire on a hand-wound magnet is real, with the resistance and cooling that implies - but budget a NEW magnet from its own ampere-turn requirement, winding window, current density and duty cycle; pole diameter alone doesn't set wire length.
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The Cyclotrino team considered a permanent magnet and chose an electromagnet 'because the field could be tuned'.
Source quote & editorial note
although a permanent magnet was considered for the Cyclotrino, it used an electromagnet because the field could be tuned
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Field tunability is a resonance-hunting knob a permanent-magnet machine gives up - which it can buy back through RF adjustment, measured-field frequency selection, shims or trim coils; the precedent documents the convenience of the tunable field, not a prohibition on permanent magnets.
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Surplus NMR-type laboratory electromagnets are a documented magnet source for small cyclotrons: Cyclotrino used a 30.5 cm Varian NMR type electromagnet consuming 500 W at approximately 1 T (1987), and Knox College used an NMR magnet with 2 T maximum field and approximately 20 cm pole faces (2000-01).
Source quote & editorial note
The magnet used was a 30.5 cm Varian NMR type electromagnet, which consumed 500 watts during operation at approximately 1 T. ... [Knox College:] The magnet was a nuclear magnetic resonance magnet with a maximum field of 2 T and approximately 20 cm diameter pole faces.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: NMR magnets bring high field uniformity - their design point - and the Cyclotrino figure (500 W at ~1 T on a 30.5 cm machine; the survey does not specify whether 30.5 cm is the pole diameter) is strikingly low power for the field. Compare against a hand-wound H-frame only with gap, field volume and cooling on the table; the shopping advice that survives any comparison: check surplus NMR listings before winding coils.
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A ham radio transceiver with an oven-controlled crystal served as the RF source for the working Cyclotrino (1987).
Source quote & editorial note
The RF was provided by a ham radio transceiver, using an oven controlled crystal.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Oven-controlled crystal stability addresses the drift side of resonance keeping, and ham gear is well-documented and repairable - as the frequency-stable SOURCE/exciter; what amplification, matching and electrode voltage sat downstream isn't in this sentence, so size the rest of the chain from its own requirements before crediting amateur gear with the whole job.
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Electrode-gap datum, the Cyclotrino (30.5 cm poles, approximately 1 T, 1987) used a dee and dummy-dee pair separated by approximately 1 mm, an extremely narrow accelerating gap on a low-energy mass-spectrometry cyclotron.
Source quote & editorial note
A dee and dummy dee system was used with the electrodes separated by approximately 1 mm.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: A millimetre-class gap maximizes gap FIELD per volt and can improve the transit-time factor - the ideal energy gain per crossing stays q*deltaV regardless - while tightening alignment, flatness and holdoff tolerances (field enhancement rises as the gap closes). One documented small end of the range, not an established bound; choose the gap from the transit-time and holdoff calculation (dg-1396).
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Chamber lids of annealed glass plates held on by external air pressure alone, sealed with vacuum grease against a stainless-steel ring, worked on Niell's high-school cyclotron (1994-95); Knox likewise used external air pressure to seal its top plate.
Source quote & editorial note
The faces of the chamber were annealed glass plates, with the external air pressure used to clamp them to the stainless steel ring, with vacuum grease to ensure a seal. ... [Knox:] like Niell, the external air pressure was used to seal the top plate to the rest of the chamber.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Atmosphere supplies ~10 N/cm2 of clamping - and the same pressure is an implosion load (~1.5 kN on a 15 cm glass lid). Historical construction, not a qualified design: before copying it, check plate stress and deflection for the actual glass and span, support the edges, retain the lid positively against venting transients, and put an implosion shield between glass and students. The visual access is real; so is the failure mode.
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Two brass dees of differing radii created the ion extraction path on Niell's machine, with a small copper sheet set into the path of ions leaving the larger dee as the collector.
Source quote & editorial note
A system of two brass dees with differing radii allowed for ion extraction. ... For a collector, a small copper sheet was set into the path of ions leaving the larger dee, which drew electrons to itself when the ion beam was incident.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: An asymmetric dee pair is a construction-level extraction trick published almost nowhere else - the radius step letting outward-spiraling ions escape the smaller electrode's envelope is the natural geometric reading (our reconstruction; the survey states the arrangement and the collector, not the mechanism), and no deflector is mentioned for this machine.
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To accelerate metal ions without a gas feed, either fabricate the filament from the desired metal or coat a nichrome wire with it, and hold it at negative potential; this solid-source technique ran on the Niell cyclotron (1994-1995).
Source quote & editorial note
either a filament was created from that metal, or a nichrome wire was coated with the metal, and raised to a negative potential
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: A coated-filament thermal source avoids the PROCESS-GAS feed for suitable metals - suitability turning on the metal's vapor pressure, filament compatibility and ionization efficiency - trading species flexibility and current for vacuum simplicity. A candidate for minimal first-beam configurations, evaluated per metal rather than assumed.
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Niell's machine is recorded as evacuated by a mechanical roughing pump with a cold trap, the vacuum monitored by a thermocouple gauge and an ion gauge - the survey names no high-vacuum pump for it.
Source quote & editorial note
A mechanical roughing pump with a cold trap were used to evacuate the chamber
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Read as recorded history, not a pumping recipe: a cold trap captures condensables, not hydrogen or air, so rough-pump-plus-trap has no general sufficiency - what made this credible is the solid coated-filament source (no continuous gas load). For any repeat: measure base and operating pressure under load and check mean free path against the spiral; the same survey's gas-fed machines carry diffusion pumps.
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Bent glass rods served as combined mechanical supports and electrical insulators for the dees, holding them in position and standing both dees off the grounded bottom plate (Niell cyclotron, 1994-1995).
Source quote & editorial note
The dees were held in place with bent glass rods, which also raised both dees off the bottom plate.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Flame-bent glass rod is cheap, vacuum-compatible standoff stock with a real precedent (and the same survey shows glass slides used similarly) - as HISTORICAL construction: for a new build, treat surface flashover, creepage geometry, cleaning, and flame-bending residual stress as the qualification items; bulk dielectric strength is the one property that was never the problem.
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Build the prototype's vacuum chamber to the final machine's requirements where the roadmap is firm: Rutgers' 22.9 cm prototype (0.889 T) deliberately used a stainless chamber - ports and flanges included - sized for the ultimate 30.5 cm machine (finished 2001, operated in excess of 1.0 T), which then reused the same chamber with only a different ion source.
Source quote & editorial note
one a 22.9 cm diameter prototype and the other was the final 30.5 cm diameter machine, finished in 2001. The prototype operated at 0.889 T, using a dee and dummy dee design. The prototype chamber was constructed for use in the 30.5 cm cyclotron that was the ultimate goal of this project, and so was much larger than required. It was stainless steel, as were the ports and flanges. ... The larger machine used a 30.5 cm pole face electromagnet that operated in excess of 1.0 T, with the same chamber as the 22.9 cm cyclotron but with a different ion source.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Oversizing the first chamber lets the highest-labor component survive the upgrade - a trade, not a law: a larger chamber costs pumping speed, gap (if it sits in the magnet) and money now against rework later; the same survey documents the opposite staging too, so decide from where the rework hurts most on YOUR roadmap.
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A single 1.3 cm thick copper rod both mechanically supported the dee assembly and carried the RF connection from the dee to the matching transformer (Rutgers cyclotron, finished 2001).
Source quote & editorial note
the assembly was supported by a 1.3 cm thick copper rod that also connected the dee to the RF matching transformer
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Making the RF feed a structural member gives a rigid connection and can save a penetration - count your own: an internal support needn't pierce the wall at all, and low loop inductance comes from the LENGTH and return-path geometry, not rod thickness. The 1.3 cm is Rutgers' as-built datum; size a new rod from RF current, mechanical load and the actual loop.
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Keep the ion-source filament electrically isolated from ground so it can be negatively biased to raise the energy of its emitted electrons (Rutgers, per the survey).
Source quote & editorial note
The filament was kept isolated from ground so it could be negatively biased to increase the energy of the emitted electrons.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Filament bias is the cheapest ionization-rate knob, but it forces the heater supply off any grounded control bus: the supply must be galvanically isolated and float AT the filament's NEGATIVE bias relative to the chamber (the Houghton machine floats its filament near -90 V, dg-310), with insulation rated for the full bias plus coupled RF and transients. And bias raises electron energy, not necessarily ion yield monotonically - scan it (dg-402).
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Enclosed differential-pressure ion source on the Rutgers 30.5 cm machine: the negatively biased filament sat in a ceramic block fed hydrogen through a small hole, capped by a ceramic plate with an aperture - letting a cone of protons stream out into the evacuated chamber while maintaining higher hydrogen pressure around the filament.
Source quote & editorial note
The negatively biased filament was mounted in a block of ceramic material to which hydrogen gas was supplied through a small hole. The ion source was then covered with a ceramic plate with an aperture ... [allowing] a cone of protons to stream out in the center of the evacuated cyclotron chamber, while maintaining a higher pressure of hydrogen around the filament
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: A drilled ceramic block with an aperture is a buildable chimney-style source. The pressure decoupling it delivers is set by the aperture conductance against the gas throughput and chamber pumping - match those (the dg-409/dg-1400 balances) rather than expecting the geometry alone to do it.
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RF power operating-point datum: the Rutgers machine's ENI NMR-300L solid-state amplifier (driven by an HP8656B signal source) could deliver 2,500 W maximum but was usually operated at 50 W with satisfactory results; the earlier prototype used an ENI350L 100 W solid-state amplifier.
Source quote & editorial note
[The RF] signal was produced using a HP8656B signal source, which had greater frequency resolution than the HP8165, and an ENI NMR-300L solid state amplifier. Its maximum output was 2,500 W, but was usually operated at 50 W with satisfactory results.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Tens of watts sufficed for a 30.5 cm, above-1-T machine with a resonant matching network - at ITS reported operating conditions; the 50x headroom was available, and whether more drive would have bought more beam is not in the record. A useful anchor for amplifier shopping: buy the headroom, expect to run far below it.
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A digital programmable RF signal source was chosen as the oscillator because it made frequency tuning easy (HP8165), later replaced by an HP8656B 'which had greater frequency resolution than the HP8165' (Rutgers).
Source quote & editorial note
The oscillator used an HP8165 digital programmable RF signal source, which offered an easy method of tuning the frequency. ... [Later the] signal was produced using a HP8656B signal source, which had greater frequency resolution than the HP8165.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Resonance hunting rewards fine, repeatable frequency steps - the documented upgrade was FOR resolution, so check any candidate source's step size against the measured resonance width (Q of the loaded resonator) before buying; whether the first unit's resolution actually limited tuning is our inference from the upgrade, not the thesis's statement.
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Faraday-collector RF shielding on the El Cerrito-era Niell machine: the collector sat inside a copper tube, cut open on one side with the opening faced toward the ion beam - the tube shielding the collector from the RF signal.
Source quote & editorial note
The copper tube also shielded the collector from the RF signal.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: A grounded slotted shield around the pickup is a sound and documented defense for beam readings taken inside a dee-drive RF field - one layer of several: pair it with shielded signal cable, verify the grounding actually sinks the induced current, and do a beam-off RF-only background run (dg-689's discipline) before crediting the residual as beam.
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An insertable phosphorescent screen on the Rutgers machine could show the vertical position of the beam inside the chamber.
Source quote & editorial note
A phosphorescent screen could be inserted into the chamber in order to determine the vertical position of the beam.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: A movable phosphor gives spatial (especially vertical) information a Faraday cup cannot - position and profile OBSERVATIONS that feed a focusing or median-plane diagnosis without uniquely proving one; pairs naturally with a viewport, and with the segmented-probe alternative (dg-790).
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Knox's dees: two copper dees mounted on blocks of insulating dielectric so each could be moved independently, operated at 3,750 V with a manually adjustable resonating circuit (as-built values; the machine had not been successfully tested by its publication, dg-1463).
Source quote & editorial note
Two dees were constructed of copper and were mounted with blocks of insulating dielectric material such that they could be moved independently of each other. ... The dees were operated at 3,750 V, using a manually adjustable resonating circuit.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: Independently adjustable dee mounts let gap and centering be tuned after assembly rather than machined perfectly the first time - the transferable idea. Treat 3.75 kV as reported without a stated convention (peak vs RMS, dee-to-ground vs gap not specified in the survey), i.e. a datum with an asterisk, not calibration.
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Because the Knox ion source was considered experimental and a weak design aspect, it was made completely removable.
Source quote & editorial note
As the ion source was considered experimental and a weak design aspect, it was made to be completely removable.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: Design for swap-out on the least-trusted subsystem - mount whatever you expect to iterate for convenient replacement. Ion sources are a common iteration target in this literature (COLUMBUS's Penning investigation, Rutgers' source change between machines), though no count across the survey backs a strongest-claim ranking.
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Knox's improvised vacuum penetrations, as recorded: electrical feedthroughs from nylon plugs, O-rings and brass screws held in place with Plumber's Goop; gas and collector penetrations sealed by rubber stoppers with holes drilled along their axes.
Source quote & editorial note
The electrical feed-throughs were made from nylon plugs, o-rings, and brass screws and were held in place with Plumber's Goop
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: Historical construction with NO implied qualification - the machine never ran to publication. For anything carrying voltage, RF or bias, use vacuum-rated feedthroughs selected for creepage, clearance, outgassing and the actual electrical ratings; improvised polymer-and-sealant penetrations are leak, tracking and outgassing liabilities that a leak-checked commercial part retires for tens of dollars.
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Measure the dee-plus-chamber capacitance before designing the resonant circuit: Knox skipped it and had to tune by trial and error; Houghton measured 79 pF for its dee-and-chamber and designed from f = 1/(2*pi*sqrt(LC)).
Source quote & editorial note
The capacitance of the dee's was not measured before building the resonating circuit, rather trial and error was used to tune the circuit. ... [Houghton:] The capacitance of the dee and chamber of the Houghton College cyclotron has been determined to be 79 pf.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: A capacitance measurement on the assembled stack converts resonator design from blind cut-and-try into calculation-plus-trim: include estimated lead/feedthrough parasitics (tens of pF scale means they matter), choose the initial inductance from the formula, and still provide adjustment range - installed resonance always lands off the paper value.
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Documented failure mode: the Knox cyclotron 'was not successfully tested by the publication' of its reference, 'the problem being' that the magnetic field moved the unsecured wires powering the ion source until they shorted the dees.
Source quote & editorial note
The cyclotron was not successfully tested by the publication of Ref [20], the problem being that the magnetic field caused the wires that powered the ion source to move and short the dees.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: Every lead inside the field carrying current TRANSVERSE to B feels F = I*L x B (a lead parallel to B feels none - route accordingly); anchor every in-field conductor mechanically with vacuum- and temperature-compatible restraint, keep leads short and stiff, and check them against the worst-case field and current before closing the chamber. The specific cures (soldered stiff leads, potted connectors, sheathed mounts) are our engineering reading, not the survey's.
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First-cyclotron filament mounting (1931): the electron source was a radio-tube filament - tungsten running through a ceramic cylinder surrounded by an oxide-coated nickel sheath - a system that 'prevented the fragile filament from destructive movement under the influence of the magnetic field'.
Source quote & editorial note
The electron source was a filament taken from a radio tube, and consisted of a tungsten filament running through a ceramic cylinder around which was an oxide coated nickel sheath. This system prevented the fragile filament from destructive movement under the influence of the magnetic field.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 12
Editorial note, tabletop extrapolation: The oldest working machine already engineered against filament motion in the field - the same fault that stopped the unbraced Knox design seventy years later (dg-1463). A rigid sheathed-cartridge mounting is the documented pattern; qualify materials for the actual thermal and vacuum environment.
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Smallest-scale existence proof: the first operational cyclotron (1931) used a 0.55 T electromagnet with 10.18 cm pole faces and approximately 2,000 V of oscillating potential to produce hydrogen ions of about 80 keV.
Source quote & editorial note
This cyclotron utilized a 0.55 T electromagnet with pole faces 10.18 cm in diameter, and with an oscillating potential of approximately 2000 V, it produced hydrogen ions with kinetic energies of around 80 keV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 11
Editorial note, tabletop extrapolation: A 10 cm, half-tesla, 2 kV machine made beam - these numbers CALIBRATE one demonstrated design point; they are not independent minima (resonant acceleration works at lower field or voltage with corresponding changes in frequency, radius and turn count), so use them as an anchor for expectations, not a floor for feasibility.
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In a collected-current-versus-field scan, expect possible structure beyond the fundamental: the first cyclotron's scan showed a quarter-cycle peak, a third-harmonic peak of resonant ions, and a secondary-collision peak - as identified by its builders.
Source quote & editorial note
Peak A was a result of the quarter cycle effect, B was the third harmonic of resonant ions, C was caused by secondary collisions
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 12
Editorial note, tabletop extrapolation: When sweeping for first beam, a peak is not proof of fundamental resonance: check its position against prediction, look for companions (one-third field would support a harmonic assignment - absence doesn't refute the fundamental, since harmonic visibility depends on capture and geometry), and use a retarding potential or energy-sensitive check where possible (dg-502's discipline).
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Focusing performance datum from the second cyclotron (11-inch, 1932), as the thesis reports it: the electrode was 1 cm thick and the ion beam produced was less than 1 mm wide, attributed to the combined electric and magnetic focusing.
Source quote & editorial note
the electrode was 1 cm thick, and the ion beam produced was less than one mm wide
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 26
Editorial note, tabletop extrapolation: Passive fringe-field focusing compressed a working machine's beam to millimetre scale - encouraging, but don't divide the two numbers: the 1 cm is the electrode's THICKNESS, not necessarily the clear aperture, and the survey doesn't give the beam-width direction. Whether a centimetre-class dee aperture bottlenecks a new machine is an envelope/acceptance calculation, not this datum.
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The thesis's computed fixed-frequency relativistic energy limits for deuterons in a uniform field (pi/2 total phase slip): 1.94 MeV at 1,000 V accelerating potential, 6.13 MeV at 10,000 V, 8.67 MeV at 20,000 V - and the thesis itself notes field shaping mitigates relativity beyond voltage alone, putting the practical proton limit for magnetic resonators nearer 25 MeV.
phase-slip criterion 2*pi*(f - f_rel)*t = pi/2 with the thesis's conventions. Caution: a straightforward re-derivation (energy gain 2qVf per unit time, f_rel ~ f(1-T/m0c^2)) gives ~0.97/3.06/4.33 MeV - half the tabulated values - so the thesis's V convention (dee amplitude vs gap gain) is load-bearing and unstated; reproduce its numbers only with its Eq. (19), not from this sketch.Source quote & editorial note
For a deuteron in an accelerating potential of 1,000 volts, the energy limit is 1.94 MeV, for an accelerating potential of 10,000 volts, the limit is 6.13 MeV, and for an accelerating potential of 20,000 volts, the limit is 8.67 MeV. ... the effects of relativity can be countered by more than just increasing the electrode voltage, it can also be mitigated by adjusting the shape and strength of the magnetic field. The actual relativistic limit for magnetic resonators accelerating protons is closer to 25 MeV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 28
Editorial note, tabletop extrapolation: For sub-MeV machines relativity is far from limiting even at 1 kV dees on any convention - both the thesis's numbers and the halved re-derivation agree on that. If energies ever approach the MeV scale, dee voltage and field shaping are BOTH levers, per the thesis's own remark.
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Field-index sizing guidance adopted in the thesis: large accelerators want only a small radial field decrease to preserve resonance over many turns, while for smaller machines 'a larger increase index is more appropriate, to provide stronger focusing'.
n = -(r/Bz)*(dBz/dr)Source quote & editorial note
for smaller machines a larger increase index is more appropriate, to provide stronger focusing
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 24
Editorial note, tabletop extrapolation: Budget the resonance-versus-focusing trade against the planned turn count quantitatively: integrate phase slip through the proposed B(r) for your turn count rather than assuming percent-level falloff stays cheap, and keep the index inside the weak-focusing stability window (0 < n < 1) everywhere the beam runs.
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Operating recipe for the gas-fed Houghton machine: rough to ~1e-3 torr, engage diffusion pump and LN2 cold trap to ~5e-6 torr base, then bleed working gas up to the operating point - at which, the thesis notes, at least 90% of the chamber gas has been purposefully introduced.
Source quote & editorial note
At this level at least 90% of the gas in the chamber has been purposefully introduced
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 30
Editorial note, tabletop extrapolation: The ten-to-one operating/base ratio estimates the intended-gas fraction ONLY if the background stays at its base value - hot filaments, desorption and species-dependent pumping can break that, so verify with an RGA where purity matters. And lambda exceeding the orbit length is survival-of-order-e^-1, not adequacy: use the loss-fraction calculation (dg-1398) for the actual criterion.
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Place the liquid-nitrogen cold trap directly above the diffusion pump, as the thesis does, so it acts as a baffle against backstreaming pump oil in the shortest, highest-conductance position.
Source quote & editorial note
act both as a baffle to contamination from backstreaming diffusion pump oils
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 31
Editorial note, tabletop extrapolation: Stacking trap over pump buys line-of-sight oil baffling with minimal conductance loss - the real benefits. Gravity is not one of them: at apparatus scale, gravitational energy is utterly negligible against thermal molecular energy, so molecules do not 'fall' into the pump. Compare side-mounting by conductance and line-of-sight geometry.
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Vent the vacuum system to atmosphere through a desiccant, as the thesis does, so the inrushing air carries less water vapor into the chamber and lines.
Source quote & editorial note
air is allowed into the system through the dessicant to reduce water vapor levels in the system
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 30
Editorial note, tabletop extrapolation: Adsorbed water is OFTEN the dominant gas load of an unbaked, frequently opened system - when it is, a desiccant vent or dry-nitrogen backfill is near-zero-cost mitigation; where pumpdown is limited by conductance, permeation or trapped volumes instead, drying the vent air buys little. A rate-of-rise curve says which regime you're in (dg-447).
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Gauge-role allocation on the Houghton machine: its thermocouple gauges were treated as reliable only above about 1e-3 torr and used for foreline monitoring and pump-changeover; the ion gauge (and RGA) read the high-vacuum side.
Source quote & editorial note
thermocouples are only reliable at pressures above about 10-3 torr
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 32
Editorial note, tabletop extrapolation: The allocation pattern transfers; the thresholds don't - take each gauge's usable range from its own manual. The placement lesson is real at small-machine conductances: measuring at the pump and inferring at the chamber can misstate the pressure the beam sees, so put the high-vacuum gauge where the answer matters (dg-475).
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Reading the thesis's RGA scan (helium deliberately admitted): the observed peaks were hydrogen - attributed by the thesis to outgassing from the stainless components - the admitted helium, and air-signature peaks.
Source quote & editorial note
The first peak is due to molecules of hydrogen, which is outgassed by the stainless steel components of the vacuum system.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 34
Editorial note, tabletop extrapolation: An RGA gives INDICATORS, not verdicts: paired N2/O2 (with Ar) in air ratios is consistent with an air leak (or residual air), and a dominant mass-2 peak in a stainless system is commonly outgassing - but mass 2 has multiple origins, so confirm attributions with isolation tests and rate-of-rise (dg-449's discipline) before acting on a single scan.
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Small commercial diffusion pump as-built datum (Innovac R220), Dow Corning 704 silicone oil heated by a 120 VAC element with the pump wall chilled by a water-cooled copper tube wrapped around the outside, supplied with 0.75 L/min of chilled water; the printed heater draw of about 0.5 A (roughly 60 W) is image-verified as what the thesis prints, but is anomalously low for a diffusion pump heater and is best read as a source-level misprint.
Source quote & editorial note
silicon oil is heated by an electrical heating element at 120 VAC, drawing about .5 A
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 31
Editorial note, tabletop extrapolation: The external wrapped-coil water jacket and DC-704 fill are transferable STARTING points for a self-built vapor pump (validate boiler power and temperature for the actual geometry - the diff_pump project's own design work governs there). The printed '.5 A' at 120 VAC implies ~60 W, low for this pump class: REPORTED BUT UNVERIFIED - check the R220 manual or a nameplate before treating it as datum or misprint.
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Cooling and protection budget for a 1.1 T-class magnet plus diffusion pump on one small chiller (3.8 L/min at 20 C total), 3 L/min to the magnet at 50 A (6 L/min would be needed at the 70 A rating) and 0.75 L/min to the diffusion pump, with an interlock that powers down the magnet below 2.5 L/min of flow or above 50 C on any coil.
Source quote & editorial note
an interlock which shuts down the magnetic if less than 2.5 liters per minute of chilled water are supplied
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 36
Editorial note, tabletop extrapolation: The transferable pattern is the method, not the numbers: independent low-flow and over-temperature interlocks wired to POWER DOWN the load, with trip points derived from the coil's insulation limits or measured thermal performance (including sensor lag) - Houghton's 2.5 L/min floor and their coil ceiling are that machine's settings, not defaults.
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Commercial laboratory electromagnet datum: the GMW model 3473-70 with 15.2 cm pole faces and 0-9.9 cm adjustable gap draws up to 70 A (4.1 kW); the machine's Powerten R62B-4050 supply supports only 50 A, at which the field is 1.127 T - the supply, not the magnet, binding the field.
Source quote & editorial note
The magnet, shown in Figure 20, is a GMW model 3473-70 with 15.2 cm pole faces and an [adjustable] pole gap of 0 to 9.9 cm ... The maximum current useable with the magnet is 70 A and at that current the magnet consumes 4.1 kW of power. The power supply however, a Powerten R62B-4050, can only support a maximum of 50 A, at which the magnetic field strength is 1.127 T
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 36
Editorial note, tabletop extrapolation: Anchors the mass/power/gap scale for buying rather than building a 15 cm magnet, and illustrates a procurement lesson worth internalizing: spec the supply WITH the magnet - a 70 A magnet behind a 50 A supply is a 50 A magnet.
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Cheap polar-coordinate field-mapping jig, as built: an acrylic disc taped to the lower pole face, milled to carry a free-rotating aluminum disc marked with 360 degrees, itself milled so the F. W. Bell 5070 Teslameter probe slides radially - and the thesis's own verdict that its map disagreed with the manufacturer curve 'because of the flaws in the Houghton College mapping apparatus and the probable misuse thereof'.
Source quote & editorial note
The field was mapped using an acrylic disc, an aluminum disc that was marked with the 360 degrees of a circle, and a F. W. Bell 5070 Teslameter. The acrylic disc was milled to fit the aluminum disc such that they shared the same axis of symmetry, and so that the aluminum disc could rotate freely. The acrylic disc was attached to the lower pole face with tape ... The aluminum disc was milled to hold the Teslameter so that the probe could slide radially. ... because of the flaws in the Houghton College mapping apparatus and the probable misuse thereof
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 37
Editorial note, tabletop extrapolation: A two-disc rotary jig is an afternoon's shop work with systematic polar coverage - and this documented failure is the caution: validate the jig against a reference (manufacturer curve for the centre field; separate checks for probe calibration, angular registration, orientation and repeatability - the centre curve alone cannot validate the coordinates).
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Field-measurement economy method, measure the center field as a function of coil current, map the field spatially at a single current, and assume the field at all points scales linearly with the center-field value to obtain the field anywhere at any current (thesis as-built procedure; its own B-versus-I curve visibly rolls off near the 1.1 T top end, where iron saturation weakens the linear-scaling assumption).
Source quote & editorial note
It was assumed that the magnetic field strength at all points would scale linearly with the magnetic field at the center.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 36
Editorial note, tabletop extrapolation: One map plus one excitation curve replaces a full map at every operating point, a large time saving; the shortcut degrades as iron saturates, so maps taken near maximum excitation should be spot-checked rather than scaled.
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Measured field-index profile of an unshimmed 15.2 cm laboratory magnet at a 3.9 cm gap, n near zero from the center out to roughly 6 cm radius (manufacturer data over 0.5 to 5 cm gives nearly constant zero) rising to almost 3.5 in the fringe field near the 7.62 cm pole edge; the planned fix is reshaping the field with ferromagnetic shims toward the desired linear increase.
n = -(r/Bz)*(dBz/dr)Source quote & editorial note
It ranges from zero in the center of the magnet to almost 3.5 in the fringe field.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 38
Editorial note, tabletop extrapolation: This magnet's measured profile - n near zero over most of the radius, rising steeply in the fringe - is what motivates shimming or pole shaping on flat-pole stock generally: no vertical magnetic focusing where n=0, local radial defocusing where n>1. Whether a given profile actually loses the beam is an orbit/tune calculation, not a glance at the n curve - run it before cutting shims.
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Eight-port ring chamber construction, a 0.9 mm thick by 2.5 cm wide brass strip soldered inside two 0.6 x 0.6 cm brass rings (inner diameter 15.2 cm, rings spaced 1.3 cm apart), with eight 1.3 cm holes drilled through the strip at 45-degree intervals and brass quick-flanges soldered into each; lids are 0.64 cm thick 6061-T6 aluminum discs, 17.1 cm diameter, clamped by eight 8-32 brass screws passing through clearance holes in the top plate into tapped holes in the bottom plate.
Source quote & editorial note
a .9 mm thick by 2.5 cm wide strip of brass soldered to the inside of two 0.6 cm by 0.6 cm rings of brass
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 38
Editorial note, tabletop extrapolation: Putting every service penetration on the cylinder wall leaves the removable lids free of vacuum-service ports - apart from seal grooves, fastener holes and any needed clearance reliefs - which is what makes them simple to re-machine or replace; the build is lathe-mill-drill-and-solder work, all within a hobby shop.
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Chamber lid sealing details, each aluminum lid carries a milled O-ring groove of 0.25 cm depth (inner diameter 15.24 cm) for a 0.32 cm thick Viton O-ring, giving roughly 22 percent cord compression; the top plate is additionally relieved with a shallower milled section in the center to clear the filament, the tallest element in the chamber, and prevent shorting against the plate.
Source quote & editorial note
by 0.25 cm deep groove with an inner diameter of 15.24 cm to accommodate a 0.32 cm thick Viton O-ring
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 39
Editorial note, tabletop extrapolation: The ~22% nominal squeeze is this design's number and in the normal static-seal band - but size a new gland from a current O-ring manufacturer's vacuum face-seal table (depth AND width, gland fill, tolerances, stretch), not from one thesis dimension. The printed 3.28 cm groove width is image-verified as printed and geometrically impossible on the 17.1 cm plate - an unresolved source misprint, flagged do-not-copy; the plausible 0.328 cm reading is a guess, not a correction.
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Eight-port budget for a minimal gas-fed machine with internal target diagnostics, two glass viewports (QF16-075-VP), one power feedthrough for the dee (Lesker EFT1213258), one multi-conductor feedthrough shared by the filament and the dummy-dee ground (Lesker EFT0082038), one Faraday collector port, one gas-inlet port with needle valve, one ion-gauge port, and one pumping port.
Source quote & editorial note
two QF16-075-VP Kurt J. Lesker glass viewports, one Kurt J. Lesker EFT1213258 power feed-through for the dee
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 39
Editorial note, tabletop extrapolation: The cited machine's eight-port budget with named catalog parts is a concrete STARTING template - port count and ratings are functions of your source biasing, RF monitoring, cooling and diagnostics, so derive your own list and check current catalog substitutes' voltage/current/vacuum ratings. One specific: a dummy dee wanting RF ground usually needs a short low-inductance chamber bond, not a shared multi-pin conductor - verify which this machine's sharing actually implies before copying it.
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Hollow dee fabrication from sheet, two equal semicircular plates of 0.9 mm copper cut from a 145 mm diameter disc are soldered to an edge strip of the same stock to form the hollow electrode, then the open face is squared on a milling machine to final dimensions of 14.3 mm thick, 142.4 mm front-to-back, and 68 mm side-to-side; a single 8-32 brass screw through the back fastens the dee to its feedthrough, with a locking washer to keep the screw tight and the dee from rotating.
Source quote & editorial note
The open face of the dee was squared using a milling machine, to give the final dimensions of 14.3 mm thick
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 40
Editorial note, tabletop extrapolation: Soldered thin-sheet construction plus one milling pass on the gap face gives a straight accelerating edge without hogging a cavity from solid - the transferable fabrication move. The single-screw-plus-lock-washer mount is the historical retention only: for a new build add a positive anti-rotation feature (key, second fastener) and a qualified RF contact, since a lock washer neither prevents rotation reliably nor makes a stable RF joint.
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The grounded dummy dee need not be a cavity at all, it was built as an open rectangular frame from two 0.9 mm thick by 5 mm wide copper strips (one 171.5 mm long bent into three sides, one 142.9 mm straight piece on top), grounded through a soldered fine copper wire (MDC KAP2) and a barrel connector to the feedthrough.
Source quote & editorial note
The dummy dee is made from two 0.9 mm thick by 5 mm wide strips of copper
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 40
Editorial note, tabletop extrapolation: Reducing the grounded electrode to a strip frame saves material, mass, and pumping-shadow volume while still defining the accelerating gap; the precedent indicates only the driven electrode needs an enclosed field-free interior.
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Houghton's dee-gap fixture as built: three insulating glass microscope slides glued across both electrodes with Loctite 1C Hysol vacuum epoxy hold the pair as one rigid assembly at fixed spacing.
Source quote & editorial note
held together by three insulating glass microscope slides, which were glued to the copper with Loctite 1C Hysol vacuum epoxy
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 41
Editorial note, tabletop extrapolation: The idea worth keeping is fixing the alignment-critical gap OUTSIDE the chamber, as one assembly. Glass slides are flat and cheap but not vacuum-qualified as supplied: clean and bake them, use a low-outgassing adhesive with a controlled bond line, check creepage across the glass between driven and grounded copper, and test the assembly at full RF voltage under vacuum before trusting it - insulator surfaces spanning electrodes are where flashover lives.
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Ion-source operating point, as built: a filament salvaged from an AET EM6G electron microscope runs at 1.5 V and 2.3 A, floating at least 100 V above ground 'to produce energetic electrons capable of ionizing the gas', and was found strong enough to resist the Lorentz forces even at maximum magnetic field.
Source quote & editorial note
Some of these gas molecules will be ionized by a filament from an AET EM6G electron microscope. A potential across the filament of 1.5 V, results in a current of 2.3 A and the filament floats at least 100 V above ground to produce energetic electrons capable of ionizing the gas. It was found that even with the maximum magnetic field the filament was strong enough to effectively resist the Lorentz [force]
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 42
Editorial note, tabletop extrapolation: Electron-microscope filaments are rigid, pre-mounted, cheap thermionic sources with this documented in-field survival. Note the physics carefully: the IONIZING energy is set by the filament-to-anode/plasma potential difference and sheath, not by the float relative to chamber ground per se - measure or model the local potentials rather than reading electron energy off the bias supply.
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Gas-line purge procedure, as built: with the Edwards LV10K needle valve (mounted directly on the chamber) closed, opening the helium flush valve lets higher-pressure cylinder gas force the accumulated line air out to atmosphere so it cannot contaminate the feed; needle valve plus regulator then control chamber helium in the 1e-6 to 1e-5 torr range.
Source quote & editorial note
the Edwards LV10K needle valve attached directly to the vacuum chamber with a quick flange. The system can be flushed with the gas from the cylinder by closing the needle valve and opening the helium flush valve. The higher pressure helium will force the air in the line into the atmosphere, so that it does not contaminate the gas. By using the needle valve and the regulator control, the pressure of helium in the vacuum chamber can be controlled in the 10-6 to 10-5 torr range.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 43
Editorial note, tabletop extrapolation: A tee with a flush valve upstream of the metering valve is the core of the purge system - dead legs and line volume set how long a real purge takes, so verify with the RGA or gauge rather than assuming any fixed duration; without a purge path, line air feeds the chamber at every startup for as long as the line holds.
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Radially scanning Faraday collector from a salvaged right-angle brass Veeco valve: the valve bellows gives 1.4 cm of in-vacuum travel (the figure annotates 1.36 cm), a 9.7 cm glass tube on the bellows screw insulates the collector from ground, and a shielded MDC KAP3 high-vacuum coaxial cable carries the signal - the thesis's own rationale being insulation from ground and RF-interference rejection.
Source quote & editorial note
a Faraday collector has been built using the bellows and housing of a right angle brass Veeco valve ... The bellows can be moved 1.4 cm in and out, allowing to measurement of the beam current in the [chamber] ... On this screw was glued a 9.7 cm length of [glass tubing] ... [through the] hole was threaded a shielded MDC Vacuum Products KAP3 high vacuum coaxial cable that carried [the signal] ... The long glass tube insulates the collector from ground, while the wire used is shielded coaxial cable to prevent RF voltage from interfering with the current reading. (Fig. 29 caption; the figure annotates the travel as 1.36 cm where the text says 1.4 cm)
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 43
Editorial note, tabletop extrapolation: A valve body is a ready-made vacuum-tight linear feedthrough, so current-vs-radius comes nearly free. The glass standoff and grounded-shield coax address leakage and RF pickup - two major error sources; secondary-electron loss and interception geometry are separate ones, so treat the reading per dg-524/dg-508 before calling it beam current.
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Vent trapped volumes inside the vacuum, the small brass screw holding the collector's glass support was bored through along its axis specifically so air could escape the screwhole instead of remaining as a trapped volume.
Source quote & editorial note
A small brass screw was bored through its axis to allow air to escape the screwhole
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 43
Editorial note, tabletop extrapolation: Blind tapped holes under screws are classic virtual leaks that masquerade as outgassing for hours. The cure is venting wherever a fastener seals a blind volume - a bored screw (as here), a vented screw, a groove, or a through-hole - chosen per joint; drilling every in-vacuum fastener indiscriminately weakens screws that never needed it.
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Faraday cup geometry against charge-loss errors, as built: a small copper box whose top slopes down from 7.0 mm to 5.0 mm toward the glass rod, the slope intended to discourage particles bouncing straight back out.
Source quote & editorial note
The top of the box slopes down, from 7.0 mm to 5.0 mm towards the glass rod
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 44
Editorial note, tabletop extrapolation: A sloped pocket can retain some backscatter but is NOT a substitute for a suppressor: secondary electrons leave at eV energies in all directions, so for quantitative current either bias a suppressor (dg-524's +9 V pattern), verify a current-vs-bias plateau, or carry a stated uncertainty. The thin-foil face acknowledging orbit shadowing is a real consideration for any cup parked in the beam plane.
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Resonator design from measured capacitance (design calculation; circuit not yet built at writing): dee-plus-chamber measured at 79 pF; at the 1.127 T maximum field, He+ orbits at 4.32 MHz requiring L = 17.2 uH, He2+ at 8.63 MHz requiring 4.29 uH - with maximum energies 77.2 and 309 keV respectively.
f0 = 1/(2*pi*sqrt(L*C)); with C = 79 pF, L = 17.2 uH at 4.32 MHz and 4.29 uH at 8.63 MHzSource quote & editorial note
The capacitance of the dee and chamber of the Houghton College cyclotron has been determined to be 79 pf. If the maximum magnetic field of 1.127 T is used then the frequency of orbit for singly ionized helium is 4.32 MHz, and thus the inductance, using (23), must be 17.2 uH. In this system the maximum energy for singly ionized helium is 77.2 keV. For doubly ionized helium, the frequency in the same magnetic field is 8.63 MHz, so the inductance is 4.29 uH, and the maximum energy is 309 keV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 46
Editorial note, tabletop extrapolation: A rare published electrode-system capacitance anchor for microhenry-scale resonator sizing at this machine class - noting the energy quadrupling with charge state at fixed field (the implied orbit radius is ~7.1 cm), that 79 pF is build-specific, and that the installed resonance still needs the parasitics-and-trim treatment (dg-1462).
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Set the amplifier drive from the spark limit: the thesis's design logic is that dee voltage follows from drive current through the resonant circuit, so the supplied current must be chosen to keep the dee below breakdown - with V = I*X_C valid only for I the CAPACITOR-BRANCH current, not the amplifier output current.
V_dee,peak = I_C,peak * X_C, X_C = 1/(2*pi*f*C), I_C the capacitor-branch (circulating) current; amplifier-to-dee transfer depends on coupling and loaded Q - measure itSource quote & editorial note
In order to avoid sparking in the gaps in the cyclotron chamber, the voltage supplied by the amplifier must be carefully chosen.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 45
Editorial note, tabletop extrapolation: With a high-Q resonator the dee voltage is set indirectly, so the spark limit must be designed in rather than discovered: use the measured or modeled loaded transfer function from amplifier to dee, verify with a calibrated pickup (dg-307/dg-1356), and back it with arc detection - the branch-current subtlety is exactly where a naive I*X_C sizing goes wrong.
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Species staging for commissioning (the thesis's stated plan): first accelerate helium nuclei to test the machine, then switch to deuterons for neutron production; expected energies 0.15 MeV for deuterons, 77.2 keV for He+ and 309 keV for He2+ (0.08 MeV appearing as the p.2 summary figure).
Source quote & editorial note
The immediate objective is to accelerate Helium nuclei to test the machine, and the ultimate is to accelerate deuterons to produce neutrons ... The expected energy for deuterons is 0.15 MeV, and 0.08 MeV for Helium nuclei. ... the maximum energy for singly ionized helium is 77.2 keV. For doubly ionized helium, the frequency in the same magnetic field is 8.63 MHz ... and the maximum energy is 309 [keV]
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 2
Editorial note, tabletop extrapolation: Debugging resonance, focusing and diagnostics on helium defers the deuteron-specific neutron/activation source term - NOT all radiological consequences: RF/HV dark current makes bremsstrahlung with any gas, and He2+ is an alpha that can drive exothermic reactions on light contaminants (Be-9, C-13). Survey from first powered operation; the staging defers the big term, not the survey.
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Self-loading neutron target scheme (the thesis's stated plan): a copper target in the chamber becomes impregnated with beam deuterons; further beam drives d(d,n)3He and d(d,p)3H on the embedded deuterons; 'since neutrons are the desirable result, no extraction system will be required' - the thesis giving 2.8 MeV for the outgoing neutrons, which pass through the chamber walls.
Source quote & editorial note
A copper target will be placed in the chamber, which will as a result of the beam be impregnated with deuterons. More ions from the beam will collide with the trapped deuterons, undergoing one of two reactions, d(d,n)3He or d(d,p)3H. Since neutrons are the desirable result of the reaction, no extraction system will be required. ... the outgoing neutrons will be produced with 2.8 MeV. The electrically neutral neutrons will pass through the chamber walls and can then be used for inelastic scattering measurements.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 48
Editorial note, tabletop extrapolation: A beam-loaded (drive-in) copper target avoids separately fabricating a deuterated target and removes extraction from the critical path. Physics notes on the thesis's numbers: D(d,n)3He neutrons at ~150 keV bombarding energy are angle-dependent, roughly 2.1-3.0 MeV in the lab - 2.8 MeV is one point on that curve, not the spectrum - and the thesis does not analyze dose or shielding beyond its concrete room, so the radiological planning is entirely on the builder.
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Personnel protection as built: the accelerator sits in a concrete brick room with an interlock control system preventing the machine from being turned on while a person is in the room.
Source quote & editorial note
in a concrete brick room with an interlock control system to prevent the accelerator from being turned on when a person is in the room
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 29
Editorial note, tabletop extrapolation: The documented access-control arrangement of the source machine - occupancy interlock plus (per its electronics chapter) remote operation - is a COMPONENT of protection, not a certified minimum: shielding calculations, surveys, monitors, fail-safe interlock design and applicable regulatory requirements decide sufficiency for any neutron-capable machine, and the thesis presents no dose analysis.
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Remote-control architecture, as documented: all electronics except the floating filament power supply are monitored and controlled remotely over GPIB, reaching the network through a National Instruments GPIB-enet; gauges concentrate through an SRS FGC 100 controller, the RGA joins via an RS232-GPIB converter, the Powerten magnet supply connects natively - and the filament floats on a 0-100 V supply.
Source quote & editorial note
All of the electronics, with the exception of the floating filament power supply, are monitored and controlled remotely through the general purpose interface bus. The National Instruments GPIB-enet allows these instruments to be controlled through an Ethernet network. ... The 1-100-K Ion gauge and CVT-272-101 Convectron gauge are connected to an SRS FGC 100 Ion Gauge Controller ... The SRS RGA 100 connection is RS232, and so it needs the National Instruments RS232-GPIB Converter ... The Powerten R62B-4050 magnet power supply supports a GPIB connection ... The voltage on the filament floats on the voltage provided by 0-100V power supply
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 47
Editorial note, tabletop extrapolation: Full remote operation is what makes an occupancy interlock workable. The floating-filament exception carries the real lesson: a floated circuit must not connect directly to ground-referenced instrumentation - it needs an isolated interface (or manual presetting outside the run), which is an implementation choice, not an impossibility.
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Staged chamber sizing in the other direction, the as-built chamber and electrodes do not use the magnet's full pole diameter, and the stated longer-range plan is to build a larger vacuum chamber and electrodes later to take full advantage of the field diameter, along with ferromagnetic shimming of the field.
Source quote & editorial note
Longer range plans include building a larger vacuum chamber and electrodes
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 48
Editorial note, tabletop extrapolation: Starting with an undersized chamber inside a full-size magnet is the documented counter-strategy to Rutgers' build-the-final-chamber-first (dg-1451) - the stated plan here being a larger chamber and electrodes later. Faster first beam and deferred precision work are the plausible payoffs to EVALUATE, not documented outcomes; either staging is defensible depending on where rework hurts.
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Scrapyard magnet construction on Niell's machine: the yoke was soft iron scrap, the pole pieces 11.4 cm steel round stock wound with 13.5-gauge wire.
Source quote & editorial note
The magnet yoke was soft iron scrap, and the pole pieces were 11.4 cm steel round stock which were then wound with 13.5 gauge wire.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: A documented precedent that scrap return-path iron plus machined round-stock poles can serve a small machine - the machine as a whole made beam, though the survey doesn't isolate the magnet's contribution. For a new build, characterize candidate scrap (saturation, consistency, joints) and remember the return path needs cross-section, not pedigree.
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The Cyclotrino's vacuum, per the survey: produced by a vacuum reservoir with a cryopump system.
Source quote & editorial note
The vacuum was produced by a vacuum reservoir with a cryopump system.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Read carefully: a cryopump IS a pump (it keeps pumping while cold), so this is oil-free, low-vibration pumping plus buffer capacity - not a pumpless machine. The architecture suits a source with little gas load (Cyclotrino's cesium-sputter source); the reservoir buys hold time against transients, not indefinite operation. Get the actual cryogenic arrangement before copying claims about power or vibration at the machine.
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Deflector-plus-probe pairing at Knox: an extractor system was DESIGNED with a negatively charged deflection plate, while the machine also carried a Faraday collector - a small metal plate insertable into the beam; the cyclotron was not successfully tested by its publication.
Source quote & editorial note
An extractor system was designed with a negatively charged deflection plate, but the cyclotron also had a Faraday collector that was a small metal plate that could be inserted into the beam. ... The cyclotron was not successfully tested by the publication of Ref [20]
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: The design logic worth keeping: pair any extraction ambition with an internal probe so beam existence is confirmed independently of extraction working. 'Designed' documents intent - the extractor was never demonstrated (the machine never ran), so this is a proposed geometry, not a precedent.
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Filament mounted directly on the dummy dee (Rutgers prototype), powered through two diametrically placed feedthroughs - the filament kept isolated from ground so it could be negatively biased to raise its electrons' energy.
Source quote & editorial note
The filament was mounted on the dummy dee, and was powered by wires that entered and exited through two diametrically placed feed-throughs. ... The filament was kept isolated from ground so it could be negatively biased to increase the energy of the emitted electrons.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Using the dummy dee as the source's mechanical platform puts the emitter at the gap with no extra standoff hardware - the documented arrangement; whether the two-feedthrough run keeps the loop taut against Lorentz forces is our engineering reading, so anchor the leads deliberately either way (dg-1463's lesson).
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As-built RF drive chain with named commodity parts: an HP 33120A function generator feeds an ENI 155LCRH RF power amplifier into the transmatch, with the transmatch-primary power monitored by a Bird 43A RF power meter.
Source quote & editorial note
The power in the primary coil of the transmatch is monitored by a Bird 43A RF power meter, and supplied by the ENI 155LCRH RF power amplifier. The RF signal is provided by the HP 33120A function [generator]
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 47
Editorial note, tabletop extrapolation: A bench function generator + lab RF amplifier + ham-style through-line wattmeter is a complete drive-and-monitor chain from commodity gear. Meter honestly: a directional wattmeter at the transmatch primary reads forward power at that point - net delivered power is forward minus reflected, and network losses sit downstream of the meter, so pair it with the dee-voltage pickup (dg-1392's two-readout rule).
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Choose design beam energy from the reaction excitation curve: the thesis justifies its 150 keV deuteron design energy by placing the d(d,n)3He cross-section 'near the maximum' of its plotted curve, calling the reaction exothermic with - as printed - '2.227 MeV released for each deuteron pair'. [Source-internal error, surfaced: 2.227 MeV is approximately the DEUTERON BINDING energy; the D(d,n)3He Q-value is 3.27 MeV and D(d,p)3H is 4.03 MeV. And the D-D cross-section keeps rising well beyond 150 keV - 'near the maximum' holds only within the thesis's plotted range.]
Source quote & editorial note
The maximum energy of the current cyclotron, using (6), is 150 keV for deuterons, which puts the cross section near the maximum. ... [the d(d,n)3He reaction is] exothermic with 2.227 MeV released for each deuteron pair.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 49
Editorial note, tabletop extrapolation: Working back from the excitation curve converts machine energy from a bragging number into a requirement - the transferable design move. D-D is the standout low-energy neutron reaction because its cross-section is already usable near 100 keV; take Q-values and cross-sections from live evaluated data (per site policy), not from the thesis's figures.
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Practical relativistic ceiling as the thesis cites it: beyond raising electrode voltage, relativity can be countered by shaping the magnetic field, and 'the actual relativistic limit for magnetic resonators accelerating protons is closer to 25 MeV' - a historical (Rose-era) estimate for that machine class, not a universal constant.
Source quote & editorial note
The actual relativistic limit for magnetic resonators accelerating protons is closer to 25 MeV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 28
Editorial note, tabletop extrapolation: Contextualizes the phase-slip table (dg-1468): field shaping buys real headroom beyond the uniform-field estimate - how much depends on the field design, so don't carry a fixed multiplier. For any machine, calculate cumulative phase slip from the actual energy gain per turn and B(r) rather than trusting an energy-class exemption; slip can bite below 1 MeV when the gain per turn is small.
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A school-scale teaching cyclotron's documented timeline: the COLUMBUS project started in 2012 (FZ Juelich provided the magnet, VACOM sponsored the chamber), registered first beam in April 2014, held its first student workshop that autumn, and - in the authors' 2022 retrospective - 'has developed very positively in the last 10 years' of continuous incremental improvement.
Source quote & editorial note
After the FZ Juelich provided a magnet, VACOM, a company for vacuum components, sponsored a suitable vacuum chamber ... the cyclotron COLUMBUS began in 2012. ... The first beam was registered in April 2014 (see Fig. 2), which was followed by the first workshop with students in autumn of the same year. ... The COLUMBUS project, started in 2012, has developed very positively in the last 10 years.
Editorial note, tabletop extrapolation: A realistic schedule anchor for the plan's teaching-machine ambitions: two years start-to-beam WITH a donated magnet and sponsored chamber - the in-kind support is part of the datum. And the methodological point stands: a conference paper's year dates the claim; prefer the builders' own retrospective dates when reconstructing a machine's history.
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A retuned matching network ('improved matchbox') made two cyclotron frequencies - 2.82 and 5.64 MHz, an octave apart - available from one RF chain on COLUMBUS. [Source-internal discrepancy, flagged: Table 1 prints 2.85 MHz where the body text and the cyclotron relation at the stated 185 mT give 2.82 MHz - do not copy the table value.]
Source quote & editorial note
With an improved matchbox, two cyclotron frequencies of 2.82 MHz and 5.64 MHz are available.
Editorial note, tabletop extrapolation: Two-frequency matching lets a small machine serve a light ion and its molecular ion, or run one ion at half field: at the fundamental, 2.82 MHz pairs with H+ at 185 mT or H2+ at 370 mT, 5.64 MHz with H+ at 370 mT (f = qB/2*pi*m). The paper states availability; which pairings were demonstrated as beam operating points, and the switching mechanics (COLUMBUS's own book documents a vacuum-relay inductor switch, dg-1393), need their own evidence per machine.
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2022 operating configuration per THPO001's Table 1 and text: 140 mm (5.5 in) dee diameter in a chamber 200 mm diameter x 75 mm high; flux density 185 mT (H+) / 370 mT (H2+); dee voltage 0.5-3.0 kV; final energy ~4.1 keV (H+) / ~7.5 keV (H2+).
Source quote & editorial note
[a] chamber with a diameter of 200 mm and a height of 75 mm. ... Diameter of the Dees 140 mm (5.5 in) Flux density 185 mT (H+) | 370 mT (H2+) ... Dee Voltage 0.5 - 3.0 kV Final Energy ~ 4,1 keV (H+) | 7,5 keV (H2+)
Editorial note, tabletop extrapolation: A long-serving teaching machine running protons at half its field capability eases magnet, RF and matching demands at the cost of energy. The quoted energies imply a ~48-50 mm detection radius (nonrelativistic equilibrium-orbit calculation at the stated fields - a derived number, not a printed one); treat the table as the published 2022 configuration without assuming every entry is a measured operating value.
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Operating-point vacuum budget with an internal hydrogen-fed source — 1e-6 mbar base pressure in the chamber, rising one decade to 1e-5 mbar with H2 gas flowing; beam production and detection function in that regime.
Source quote & editorial note
Vaccum in the chamber 10-6 mbar dto with H2 10-5 mbar
Editorial note, tabletop extrapolation: Plan pumping capacity for the gas-on state, not the base pressure; a decade of pressure rise under source gas load is the demonstrated working regime for a keV-class internal-source machine at this scale. (Quote reproduces the table verbatim including its spelling; exponents are superscripts in the original.)
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Beam-species spectroscopy by field sweep, as COLUMBUS practices it: fix the detector position and RF frequency, continuously increase the magnetic field, and log beam current - peaks appear at very specific fields, from which q/m follows via q/m = 2*pi*f/(h*B).
q/m = 2*pi*f / B (peak assignment from known f and measured B)Source quote & editorial note
the detector is set to a specific position and the magnetic field is continuously increased. With very specific magnetic fields, there are peaks in the beam current
Editorial note, tabletop extrapolation: A B-sweep at fixed frequency is a q/m RESONANCE SURVEY - the cheapest species diagnostic a small machine has, not a full mass spectrometer: state the harmonic number, calibrate the field reading (dg-1428), and resolve the q/m degeneracies and harmonic ambiguities by field-ratio checks or frequency scaling (dg-1422/dg-1423) before naming species.
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Beam-current spectra of a fixed-frequency machine show secondary peaks from ions circulating at one-third and one-fifth of the nominal velocity - odd-subharmonic acceleration - alongside the main species peaks; the COLUMBUS workshop analyses them deliberately.
Source quote & editorial note
the two-day workshop can also analyse other peaks e.g., the peaks that correspond with the third or fifth of the nominal velocity.
Editorial note, tabletop extrapolation: When a field-sweep spectrum shows unexplained minor peaks, check near ONE-THIRD and ONE-FIFTH of the main peak's field (f_RF = h*f_c, so B_h = B_1/h for the same species - lower field, not higher) as the odd-harmonic hypothesis, alongside contaminant-species and instrument checks; a matching position is a candidate assignment, not proof (dg-502's discipline).
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An extraction upgrade for a keV-class machine can pair a deflection system with a Wien filter, as the COLUMBUS project aims to, guiding the extracted beam through the filter 'to measure the speed and energy of the ions' - the filter selecting velocity (v = E/B), from which energy follows for a known species.
Source quote & editorial note
The aim of this project is to deflect the ion beam and guide it through a Wien Filter to measure the speed and energy of the ions.
Editorial note, tabletop extrapolation: A Wien filter is a realistic first external beamline element for a low-energy machine: it measures VELOCITY directly and yields energy only once the species is known (or paired with a separate analyzer) - which is exactly why it also cross-checks species assignments. It needs crossed electric AND magnetic fields; at keV energies both are modest, but 'electrostatic-only' it is not.
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Evolution path for the ion source — the machine runs a hydrogen filament source, and a Penning ion source is under investigation (as a student internship project) with the aim of installing it in the accelerator; source replacement is treated as an incremental upgrade, not a redesign.
Source quote & editorial note
or investigate a Penning ion source with the aim of using it for the installation in the accelerator.
Editorial note, tabletop extrapolation: A filament source reached first beam here and a candidate Penning source is being investigated as a student project - the sensible pattern being to characterize any replacement source off-machine, then verify its mechanical, vacuum, electrical, gas-feed and central-region interfaces before installation; a source swap touches more of the machine than the source (recommendation, not the paper's documented method).
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The cyclotron was continuously improved and expanded with the involvement of pupils and students - the paper's own history listing the magnet cooling system, detector linear translator, mechanical model and simulation, and the first 3D-printed vacuum chamber among the student-era improvements.
Source quote & editorial note
The cyclotron was continuously improved and expanded with the involvement of pupils and students.
Editorial note, tabletop extrapolation: An educational machine CAN make learner projects its upgrade workforce when they are scoped as real subsystem work - a Faraday-cup translator or a field map is simultaneously curriculum and infrastructure; whether that is the fastest improvement route is a program-design judgment, not this paper's measurement.
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The COLUMBUS workshop format as adopted: groups of up to 6 participants; up to 12 accepted and split into two groups; offered as two-day, one-day, and online (three remote sessions plus one lab session) variants.
Source quote & editorial note
A workshop takes place in groups with up to 6 participants. If more people register, up to 12 persons can be accepted, who will then be divided into two groups.
Editorial note, tabletop extrapolation: Six-per-group is the format the team settled on for one machine - a reasonable planning anchor for hands-on accelerator teaching, not a demonstrated pedagogical ceiling; whether hybrid delivery preserves learning quality is an outcomes question the paper doesn't measure. Copy the structure, evaluate your own.
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State a teaching cyclotron's requirements as two conditions before any dimensioning, per the 2013 design account: every operating parameter (vacuum, magnetic field, frequency) kept low enough that standard commercial components suffice, and the final energy kept small enough that no harmful radiation can arise, so that students can experiment at the running machine; the whole parameter table is then presented as the consequence of these two conditions.
Source quote & editorial note
In order to build such a small cyclotron one has to meet two conditions: Vacuum, magnetic field, frequency etc. must be so low that one can use standard components as far as possible, otherwise the costs will go to infinity; The final energy of the cyclotron must be small enough so that no harmful radiation can arise, so that the students can do experiments with the cyclotron. Table 1 shows the technical data of COLUMBUS. One can easily recognize that COLUMBUS meets all the conditions mentioned above.
Editorial note, tabletop extrapolation: A hobby-scale build benefits from the same requirements discipline; writing the cost condition and the radiation condition down first turns every later component choice into a check against them. The radiation condition itself needs its own verification, not just an energy number: whether 'no harmful radiation can arise' at a given operating point is the paper's claim for its machine, and X-rays begin when high voltage or RF is energized, before any beam.
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Preserve the pre-beam design snapshot as its own dated record. The 2013 conference table (design calculation, 2013) lists 140 mm dee diameter, 0.38 T flux density, 5.63 MHz, 2.0-3.0 kV between the dees, 6-8 revolutions, 24-48 keV expected final proton energy, and 1e-5 mbar chamber vacuum rising to 1e-4 mbar with hydrogen feed. Editorial observation: the 24-48 keV span tracks dee voltage times gap crossings under ideal synchronous gain (2-3 kV over 6-8 revolutions, two crossings each), the project's 2016 paper records that no beam operation was possible in 2013 and first beam came in April 2014 (so the table is pre-beam), and later published accounts of the same machine report operation well below these design values - the snapshot is the anchor for a documented design-versus-operating-point contrast.
Source quote & editorial note
Table 1: Technical Data — Diameter of the Dees 140 mm (5.5 in); Flux-density of the magnetic field 0.38 T; Vacuum in the chamber 10-5 mbar; dto with H2 10-4 mbar; Cyclotron frequency 5.63 MHz; Number of revolutions 6-8; Voltage between the dees 2.0 -3.0 kV; Final energy 24 - 48 keV … The expected final energies of the protons are 24 - 48 keV after 6 - 8 revolutions. These energies don't produce any radiation outside the chamber.
Editorial note, tabletop extrapolation: A conference paper's date fixes the claim, not the beam; when reusing published small-cyclotron parameters, check whether the paper predates first beam and label such values as design predictions rather than demonstrated performance.
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The two hardest procurement items for a school-built cyclotron, a homogeneous-field magnet and a custom vacuum chamber, were both solved by donation, per the 2013 account: a research institute (Juelich, IKP) donated a Bruker BE-15 laboratory magnet, and a vacuum-component company (VACOM) fabricated the ten-port chamber free of charge, with further support from regional companies, foundations and a youth-science sponsor pool.
Source quote & editorial note
At the very beginning there were two big problems: How to get a magnet for the homogenous field and How to get a suitable vacuum-chamber. The first problem was solved by the Research Institute of Jülich. Prof. Dr. Maier and his team donated a Bruker BE-15. … The second problem was solved by VACOM, a company specialized in vacuum-components. VACOM built the vacuum-chamber, i.e. Fig. 1, for us free of charge.
Editorial note, tabletop extrapolation: For an educational build, soliciting institutional donations for the few components a home or school shop cannot make is a documented alternative to surplus-market hunting.
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An adjustable-gap laboratory electromagnet lets one magnet serve several field regimes: the donated machine's 150 mm poles with pole pitch adjustable over 50-120 mm reach up to 2 T at close spacing and up to 0.7 T at 100 mm spacing (design-era figures, 2013), so the pole spacing chosen around the chamber sets the field ceiling available to the coils.
Source quote & editorial note
The pole-diameter is 150 mm (~ 6 in). The pole pitch is adjustable from 50 - 120 mm (~ 2 - 5 in). The flux-density is up to 2 Tesla depending on the spacing of the poles. At a distance of 100 mm the flux-density is up to 0.7 Tesla.
Editorial note, tabletop extrapolation: When adopting a surplus laboratory magnet, the published pole diameter, pitch range and field-versus-spacing figures are the sizing inputs; the field available at the actual chamber-plus-walls spacing is the number that matters.
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The RF source specified at design time (2013) was a marine short-wave transceiver delivering 50-70 Veff across 500 kHz to 35 MHz with 120 W available power, feeding a matchbox that steps the output up to the 2000-3000 V needed between the dees.
Source quote & editorial note
The RF-power-source is a short-wave transceiver for marine radio. It provides an AC voltage of 50-70 Veff at frequencies from 500 kHz to 35 MHz. The available power is 120 W. … As well as an impedance converter the matchbox is also an RF-transformer transforming the 50 - 70 V output voltage of the power-source up to 2000-3000 V voltage, which is needed for the acceleration of the protons.
Editorial note, tabletop extrapolation: The transmitter's rated power is a design-era catalog figure; the usable continuous carrier in the modulation mode actually chosen should be verified on the bench before the RF power budget is frozen.
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Instrument the RF chain at both ends: a directional coupler in the matchbox input circuit to monitor and minimize the reflections back into the RF source, and a separate RF pick-up in the output circuit (a diode-detector probe feeding a meter) which the paper uses to check whether the machine is tuned to its 5.63 MHz cyclotron frequency.
Source quote & editorial note
A directional-coupler in the input-circuit of the matchbox makes it possible to control and minimize the reflections back into the RF-source and a RF pick-up, i.e. Fig. 6, in the output-circuit allows to check whether the cyclotron is tuned to the cyclotron-frequency of 5.63 MHz
Editorial note, tabletop extrapolation: Two independent indications, reflected power at the input and detected RF at the dee side, help separate matching problems from resonance problems during tune-up - though both respond to coupling and resonance, so neither is unambiguous alone, and the pick-up reads amplitude: the drive frequency itself should be known independently (a counter is cheap) and compared against qB/2πm.
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In a machine of very few revolutions (ten or fewer), the source deliberately departs from the normal centred mounting: its position is adjustable in the direction of the accelerating gap so the ideal starting position of the first path can be found by experiment; in the reference design the source is therefore not fixed-mounted but stuck under the dummy-dee (design decision, 2013).
Source quote & editorial note
For the setup of the ion source, it is considered that the ion source remains adjustable in direction of the gap, so that the ideal position can be found by experiments. Normally the ion source is centred in the cyclotron. However, in our case – with our small cyclotron and such a small amount of revolutions (≤ 10) - it is better to optimize the starting position of the first path. Due to this fact the ion source will not be fixed mounted but it will be stuck under the dummy-dee instead
Frank, Wolf & Held, COLUMBUS — A Simple Ion Source — WEPPT021, Proceedings of Cyclotrons2013 (2013) — p. 1
Editorial note, tabletop extrapolation: With only a handful of turns there is no adiabatic settling; an adjustable source mount converts a machining guess about the first half-turn into a tunable parameter, and the optimum need not be the centred position.
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Because ions leave a thermionic chimney source with very low energy, make the emission direction adjustable as well: a rotatable source-head lets the slit angle be optimized by experiment for better acceleration and to prevent the protons remaining in the gap between the dees (design decision, 2013, pre-beam).
Source quote & editorial note
the angle of emission shall be adjustable for a better acceleration and to prevent that the protons remain in the gap between the dees
Frank, Wolf & Held, COLUMBUS — A Simple Ion Source — WEPPT021, Proceedings of Cyclotrons2013 (2013) — p. 1
Editorial note, tabletop extrapolation: A rotatable head is a cheap second degree of freedom on top of source position; both exist because low-energy ions do not forgive alignment errors in the first gap.
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The school machine's ion source was built after the pattern Tim Koeth first used in the Rutgers 12-inch cyclotron (the paper's reference [1]); the project's own design effort went into what its few-revolution machine specifically required - adjustability of source position and emission angle.
Source quote & editorial note
The protons for our cyclotron are produced in the ion source which was built after the pattern of Tim Koeth [1], which he used first in his cyclotron. … A specific design of the ion source was required due to the cyclotron's small size and the low number of revolutions … It was designed for adjusting the position of the ion source itself and the proton's angel of emission. … [1] Tim Koeth, "The Rutgers 12-Inch Cyclotron Ion Source Studies Part I"
Frank, Wolf & Held, COLUMBUS — A Simple Ion Source — WEPPT021, Proceedings of Cyclotrons2013 (2013) — p. 1, 2
Editorial note, tabletop extrapolation: A documented precedent for reusing a published hobby-machine source design: here the ionization geometry was adopted whole and the adaptation effort spent on mounting and adjustability.
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When simulating orbits in a classical cyclotron, model the acceleration gap with the in-plane Lorentz force (coupled x-y differential equations with uniform Bz and gap field Ey, including the magnetic deflection during the gap crossing) instead of the textbook straight-line gap approximation; the paper's stated purpose for the more realistic picture is to help adjust the machine and explore the initial orbits.
m*a = q*(E + v x B); x'' = omega_ZF*y'; y'' = (q/m)*Ey - omega_ZF*x'; Ey = E_hat*cos(omega_RF*t - phi)Source quote & editorial note
In contrast to the simpler common school model that approximates the tracks in the acceleration gap by straight tracks, the presented simulation considers the deflection of the ions by the magnetic field in the acceleration gap. So a more realistic picture of the paths can be drawn, which will help to adjust the cyclotron and explore the initial orbits of the ions in detail.
Editorial note, tabletop extrapolation: Whether in-gap deflection matters scales with gap width against local gyroradius; on a small machine whose gap is a large fraction of the first-turn radius it shapes the first turns, which is exactly where this machine tunes. A home-built orbit code should integrate the coupled equations in the gap rather than assume straight crossings.
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Split the orbit computation into two piecewise regimes per half-turn — numerical integration of the coupled differential equations in the acceleration gap, then closed-form circular-arc equations inside the dee and dummy dee where no accelerating field exists — matching arc entry conditions from the gap-exit position and velocity.
x(t) = rho*cos(phi_in - omega_ZF*(t-t0)) + xM; y(t) = rho*sin(phi_in - omega_ZF*(t-t0)) + yM; phi_in = pi/2 + arctan(vy0/vx0); rho = sqrt(vx0^2 + vy0^2)/omega_ZF. Caution: the printed phi_in uses one-argument arctan, which loses the velocity quadrant and is singular at vx0 = 0 - source-internal limitation, do not copy; a quadrant-safe form (atan2 with consistent sign conventions) or a Cartesian closed-form arc avoids it.Source quote & editorial note
In the dee itself, or, in and behind the dummy dee there is no accelerating electric field so that the ion trajectories can be described by equations of a circle
Editorial note, tabletop extrapolation: The hybrid analytic-arc-plus-numerical-gap scheme is far cheaper than brute-force stepping the whole orbit and keeps the accelerating-field-free segments (uniform B, no E) exact; it suits a laptop-class tracker for a small machine.
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Terminate each simulated ion trajectory when it intersects a virtual obstacle — the ion source body, a shield, or the vacuum chamber wall — so the code naturally reproduces geometric losses instead of tracking unphysical survivors.
Source quote & editorial note
The change of differential- and circuit-equations is completed as long as the calculated ions meet a virtual obstacle. Such an obstacle can be the ion source, a shield or the vacuum chamber itself.
Editorial note, tabletop extrapolation: Encoding the source housing and chamber wall as kill surfaces in an orbit code is a cheap way to predict which starting phases survive the first turns and where lost beam lands.
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Structure a teaching-scale orbit simulation in three layers — an input layer holding three parameter groups (ion properties, experiment settings, machine geometry), a simulation engine, and a presentation layer whose plot modules (XY orbit plot, intensity plot, spectrometer plot) each also export data to file for external processing.
Source quote & editorial note
As shown in Fig. 1 the simulation consists of three sections, the input-layer, the simulation-layer and the presentation-layer. … The input-layer incorporates three groups of parameters which define the ions, the experiment and the geometry of the cyclotron. So the simulation can be easily adapted to different situations. … The simulation engine described above has three modules for the evaluation: XY-Plot, Intensity-Plot and Spectrometer-Plot. Every module - apart from the graphical output - allows also a data export to a file so that the measured values can be processed by external programs.
Editorial note, tabletop extrapolation: Separating ion, experiment, and geometry parameter groups lets one code serve several machine configurations and several experiments; the data-export hook is what allows direct overlay of simulated and measured detector scans.
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Measure early-turn beam structure with a Faraday cup on a linear translator that sweeps radially behind the dummy dee along a sensor line about 1 mm outside its edge, logging cup current together with cup x-position; on the reported machine the source sits at (-15, 5, 0) mm and the sensor line is y = -31 mm in chamber-centered coordinates.
Source quote & editorial note
a linear translator was developed in order to move the detector, a Faraday-cup in a radial direction behind the dummy dee. In addition to the registered ions the corresponding x-position of the cup is measured, too … The ion source is located at position (-15, 5, 0) (all figures in mm), a Faraday-cup as an ion detector moves along the line y = -31 mm, the so-called sensor-line. This line extends parallel to the lower edge of the dummy dee with a distance of about 1 mm.
Editorial note, tabletop extrapolation: A radially scanned cup with simultaneous position readout turns a single detector into a turn-structure probe, giving I(x) profiles that can be compared point-by-point against a simulated orbit bundle.
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A pronounced detector signal can be genuine yet not the intended species: at an operating point of B = 66 mT (RF 5.00 MHz per the figure), simulation predicted a bundle of closely spaced H2+ trajectories at one fifth of maximum speed, and the measured radial scan showed a matching pronounced peak.
Source quote & editorial note
If B = 66 mT, the simulation predicts a set of closely spaced trajectories of H2+ - ions that have 1/5 of the maximum possible speed. This meets the corresponding measurement
Editorial note, tabletop extrapolation: This sharpens the false-beam trap for I(B) sweeps on hydrogen machines: a strong cup signal at an unexpected field may be partially accelerated H2+ on closely spaced slow orbits, and a first-turns simulation predicts where such impostor peaks should appear. Treat the simulation as one hypothesis, not a verdict - a Faraday cup is not species-resolving, so confirmation needs a q/m-dependent field-frequency scan or another species-sensitive check before a peak is accepted or discounted.
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Expect the measured radial intensity profile I(x) of the inner turns to be nearly continuous rather than showing discrete turn peaks, because successive orbits lie close together; the paper reports this expectation qualitatively confirmed.
Source quote & editorial note
In the corresponding plot one can see how close the orbits are to each other. So it is obvious that at an Intensity-Plot I = I (x) in reality will be an almost continuous chart as shown in Fig. 6. This is qualitatively confirmed by the model, too.
Editorial note, tabletop extrapolation: Absence of clean turn separation in a radial probe scan is not by itself evidence of a fault: when turn spacing is small against beam width and probe resolution, a smeared continuous profile is the expected signature - though phase and energy spread, emittance and detector response smear it further.
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Operate the machine as a mass spectrometer for beam diagnosis by fixing the detector position and sweeping the magnetic field: peaks in current versus field identify the species present (the paper's Fig. 7 shows the measured spectrum), and the same experiment can be pre-computed with the orbit simulation's spectrometer module.
Source quote & editorial note
In this experiment the beam is measured in dependence of the magnetic field at a fixed position of the detector. Here one can identify the ions in the beam … The Spectrometer-Plot (Fig. 8) shows the caluculated probability as a measure for the beam-current vs. the magnetic field and allows to simulate this experiment.
Editorial note, tabletop extrapolation: A fixed-cup B-sweep is a species diagnostic using hardware a small hydrogen machine already carries, separating proton from molecular-ion contributions; simulating the sweep first tells the operator which peak to expect where. The assignment rests on rigidity plus the assumed charge and energy, so overlapping peaks can stay ambiguous.
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Treat first-turns simulations as qualitative until their idealizations are removed. Stated limitations of the reported model include an assumed constant ion beam, particle-number conservation despite no focusing, and neglect of parameter measurement uncertainty, so quantitative agreement with probe data must not be over-read.
Source quote & editorial note
the quantitative analysis of the results must be considered very carefully, because there are some assumptions in the simulation that are not met in reality, such as a constant ion beam or the conservation of particles, which is not satisfied, due to the lack of focusing. Finally, the measurement accuracy in the determination of some parameters was not considered in the simulation. Nevertheless, the present simulation offers qualitatively a good idea of the acceleration process
Editorial note, tabletop extrapolation: When a home-built tracker and a probe scan disagree in amplitude, the model's stated idealizations (constant current, no losses) are one candidate cause - so are field maps, geometry, RF phase and calibration; check both sides. Use the simulation for locations and trends, not absolute currents, and treat even peak locations as unvalidated until compared against measurement.
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Laser powder-bed metal 3D printing (LaserCUSING, stainless steel 1.4404, layer thickness 15-500 microns) can produce components that meet high-vacuum requirements; the reported validation was deliberately bounded to the high-vacuum range because the pump station used did not go below 10^-5 mbar, with ultra-high vacuum (below 10^-7 mbar) named as untested next territory.
Source quote & editorial note
This work is limited to the area of high vacuum. The limitation is due to the simple handling of the components and the existing pumping station, with which a minimum of 10-5 mbar is not undercut. … The present work shows that metal-based 3D printing can meet the requirements of vacuum technology in the area of high vacuum.
Editorial note, tabletop extrapolation: Printed 316L-class components are demonstrated at high vacuum down to the study's achieved 1.5·10-5 mbar; the 10-6 decade was not reached by its pump station and UHV is explicitly untested, so claims below the tested pressure are extrapolation, not evidence.
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Budget post-processing into any powder-bed metal print destined for vacuum service: in the reported process (LaserCUSING, 1.4404) the powder leaves an inherent surface roughness that must be smoothed by reworking, and overhangs shallower than 45 degrees need support structures that must be removed afterwards.
Source quote & editorial note
Due to the use of powder in the production, 3D-printed parts have a certain surface roughness, which must be smoothed by reworking. Another consequence of the layered structure is the fact that in overhangs with an angle smaller than 45° support structures - as shown in Fig. 2 - are necessary. They must be removed in the aftermath.
Editorial note, tabletop extrapolation: When designing a printable vacuum part, orient sealing faces and bores to respect the chosen printer's qualified support limits (45° in this process) and leave machining allowance on sealing surfaces; the print is a near-net blank, not a finished part.
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Printing standard vacuum components is hardly worthwhile - the paper's conclusion from the elaborate post-processing - so the economic pattern it demonstrates is hybrid construction: print only the geometrically complex body and complete it with conventionally manufactured standard parts (here by welding on flanges and tube).
Source quote & editorial note
Due to an elaborate post-processing, it is clear that the 3D printing of standard components will hardly be worthwhile. Consequently, in order to achieve an economic use of this technology, it is necessary to retrofit the printed components with standard parts from conventional manufacturing.
Editorial note, tabletop extrapolation: For a low-budget build the demonstrated pattern is catalog KF/CF hardware joined to a printed complex body; a plain straight connector is exactly the case the source found uneconomic to print. Compare current quotations - the economics move with the market.
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Conventionally manufactured stainless welding flanges can be welded to laser powder-bed printed stainless tube without difficulty and without subsequent rework; on the reported test article (printed tube, 41 mm OD, 38 mm ID) both welds were vacuum-compatible as made.
Source quote & editorial note
a simple tube with an outside diameter of 41 mm and an inside diameter of 38 mm was printed and completed on one end by a welding flange and on the other side by a flange with a tube … The two different welds could be attached without problems. This meant that no further reworking was required.
Editorial note, tabletop extrapolation: On this test article, printed 316L took conventional welds with no special procedure - encouraging for hybrid printed-plus-welded assemblies, but weldability and vacuum integrity move with print density, orientation, surface preparation and heat history, so a new printed assembly still earns its own weld procedure and leak qualification.
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A printed KF connector and a hybrid printed-tube-with-welded-flanges assembly (inner radius 19 mm, length 160 mm, volume 0.18 l, inner surface 0.019 m^2) both reached 1.5*10^-5 mbar without problems - the paper's pumpability demonstration at high-vacuum level; the quantitative gas-load comparison is the separate 24 h pressure-rise test.
Source quote & editorial note
With both parts a high vacuum of 1.5·10-5 mbar was reached without problems.
Editorial note, tabletop extrapolation: Mid-10^-5 mbar is already the working range of many small accelerator chambers, so this is a meaningful screening result - and only that: a reached pressure folds together pumping speed, outgassing and any leaks, so it proves the assembly pumpable on that stand, not leak-free. Cleaning and an acceptance test still precede installation.
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Qualify a vacuum component by a 24-hour pressure-rise test against a background run. Record the pressure increase of the pumped-down test chamber alone, then with the sealed-off specimen attached, and convert slope to leak rate via chamber volume with the background subtracted; the reported setup used a 3.6 l chamber with two membrane gauges of different ranges plus a hot-cathode gauge and a turbopump station.
Q = (dp/dt)*V - Q_background, with V the connected evacuated volume of the run being measuredSource quote & editorial note
Before the actual examination a background measurement of the chamber without specimen was performed. Here, as with the test objects, the pressure increase Δp was recorded over a period of Δt = 24 h
Editorial note, tabletop extrapolation: An amateur-affordable gas-load screening test: it bounds total leak-plus-outgassing without a helium leak detector, but it cannot distinguish real leaks from outgassing or localize anything, so helium detection keeps its place where a leak must be found or a specified limit certified. The background run is essential because chamber outgassing (reported background 1.00*10^-7 mbar*l/s) is the same order as the specimen signal being measured.
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An as-printed (uncleaned) hybrid printed-and-welded connector measured only slightly worse than a conventional stainless connector of the same type in a 24 h pressure-rise test — 7.39*10^-7 versus 5.25*10^-7 mbar*l/s combined leak-plus-outgassing rate — so print provenance is not, by itself, a vacuum disqualifier at high-vacuum level.
Source quote & editorial note
the 3D-welded KF-SC DN-40 in the uncleaned state behaves slightly worse than a conventionally manufactured component KF-SC DN40 made of stainless steel. … Table 2: Leakage Rates … 3D Welded KF-SC DN40 uncleaned … 7.39·10-7 … Edelstahl KF-SC DN40 … 5.25·10-7 [Leakage Rate column, mbar·l/s]
Editorial note, tabletop extrapolation: The penalty for a printed part fresh from post-processing is a factor of about 1.4 against wrought stainless in this 24 h test; whether that matters in a given system is a gas-load-budget question, not a constant.
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Clean printed vacuum parts in an isopropanol ultrasonic bath before service; in the reported test this cut the printed connector's measured rate from 7.39*10^-7 to 2.15*10^-7 mbar*l/s — better than the conventionally manufactured comparison part at 5.25*10^-7 mbar*l/s.
Source quote & editorial note
the influence of a pretreatment can be checked by cleaning the 3D-welded KFSC DN-40 with isopropanol in an ultrasonic bath and rerun the pressure increase measurement. … When cleaned, the 3D printed part is even better than the conventional one. … Table 2: Leakage Rates … 3D Welded KF-SC DN40 cleaned … 2.15·10-7 [Leakage Rate column, mbar·l/s]
Editorial note, tabletop extrapolation: A 3.4x improvement from one solvent ultrasonic cleaning makes validated cleaning one of the cheapest vacuum upgrades going; transferring it to other parts means checking solvent compatibility, trapped volumes, rinsing and complete drying rather than assuming the same factor.
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Exploit additive manufacturing's function integration for vacuum vessels by printing a network of flow channels directly into the chamber wall, shaped with a CFD program for good flow; the same channels heat the vessel during evacuation (bake) and cool it during later operation.
Source quote & editorial note
Through the flow channels, the recipient can be heated during evacuation and alternatively cooled when needed in operation. The exact shape of the channels was determined by a CFD-program to ensure optimal flow conditions.
Editorial note, tabletop extrapolation: Integrated wall channels give a small chamber bakeout and cooling with no external jacket or brazed lines - a capability that is expensive to add to a one-off machined chamber - at the price of fluid connections and a leak qualification of the channel walls against the vacuum volume.
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A complete working vacuum chamber can be built as a printed complex base body with integrated channels, finished by welding on standard commercial components; the approach avoids unnecessary rework, and its geometry can be re-adapted per build since no tooling or molds are involved.
Source quote & editorial note
Since no moldings and other tools are necessary for the production of 3D printed components, there are no further costs. … The basic body of the vacuum chamber was supplemented with a complex geometry and integrated flow channels and completed by welding standard components. In addition to a cost-effective production by avoiding unnecessary rework, this method also has the advantage of a flexible adaptation to different customer requirements.
Editorial note, tabletop extrapolation: For a multi-port chamber whose port pattern is unique to one machine, a printed body with welded catalog flanges is a demonstrated alternative to welded-plate fabrication and machining from solid, and the port layout can be revised in CAD between builds without molds or dedicated tooling - the build itself still costs supports, fixtures, inspection and sealing-surface machining, so the comparison is build-specific.
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In the paper's high-vacuum tests the measured leakage rate was essentially attributable to the Viton flange gaskets, with printed-surface roughness not yet effective; the authors expect surface properties to become decisive below 10^-7 mbar and state that how big that influence is must come from further tests.
Source quote & editorial note
the leakage rate is essentially attributable to the Viton flange gaskets and the material properties, for example the roughness of the surface, are not yet effective, they will have a decisive influence when the pressure falls below 10-7 mbar. How big this influence ultimately is, must result in appropriate tests, which require a much greater effort.
Editorial note, tabletop extrapolation: On an elastomer-sealed machine, gasket permeation can dominate the gas load, as it did in this test - but the crossover is system-specific, so build the gas-load budget (seals, wall outgassing, leaks, trapped volumes, pump speed) before deciding which term to chase; no universal pressure divides gasket-dominated from wall-dominated systems.
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Metal 3D printing's benefit for vacuum work concentrates in single production and prototypes, where geometry freedom and function integration (the paper's example: a built-in surface heating system) carry the case; the same paper found printing standard components hardly worthwhile.
Source quote & editorial note
Especially for single production and prototypes, 3D printing technology can be of considerable benefit. This is particularly due to the freedom in geometry and the possibility of function integration, such as the realization of a surface heating system.
Editorial note, tabletop extrapolation: A one-off machine is exactly the single-production case; a sound screening default is to consider printing where a part is unique and geometrically complex and to price catalog, machined, welded and printed options case by case.