Design Guide
1374 design rules for small and tabletop cyclotrons, extracted from the
amateur-relevant accelerator literature — from Livingston & Blewett to
undergraduate machine theses. Each rule carries its formula where the source
gives one, a verbatim quote, and a page-level citation. Applicability notes are
calibrated to a concrete reference point: where a note says “the reference
machine”, it means a representative, publicly documented amateur build of
the tabletop class — roughly 0.6 T on 8-inch poles, ~150 keV protons —
used as a worked example so the numbers are concrete, not abstract. Where a note
says “a next machine”, it means a prospective higher-field,
tighter-gap successor to such a build. Every rule has a stable identifier
(dg-001…dg-1374), shown beside its domain tags,
so a rule can be cited by id and linked directly — e.g.
/design-guide/#dg-217. The same rules are also published as
per-subsystem pages (one static page per domain tag, in the directory above the
schematic), which load faster and are what site search returns. The schematic below maps the major
subsystems of a generic classical cyclotron onto the rule domains used
throughout this guide.
Verify before use. These rules were machine-extracted from the literature, in part from freshly OCR'd scans. Quotes and numbers were checked against page images where the OCR looked suspect, but transcription errors can survive. In the status vocabulary of this site’s editorial methodology, every rule here is a source extract — faithful to its cited source, not an independently validated engineering requirement. Any rule that drives a real design decision — and every safety-critical number — should be re-read at the cited page of the source before you commit metal, money, or high voltage to it. These rules are an educational reference, not an operating procedure: pair them with the safety fundamentals and your jurisdiction’s registration requirements.
-
Momentum-analyze the beam to separate H+ from H2+ using a bending field and defining slit: 10 cm bend radius, 4 cm wide poles with 1 cm gap at up to 18 kG, and a 0.5 x 1 cm slit selects one species with a small energy spread.
r = 10 cm, gap 1 cm, B up to 18 kG; slit 0.5 cm x 1 cmSource, quote & tabletop applicability
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
Tabletop: In a cyclotron the machine itself is the analyzer, but any external beamline species check on the next machine can copy these modest slit and pole proportions.
-
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 & tabletop applicability
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
Tabletop: For 8-in poles at 5.9 kG with ~1.5-in gap, usable R is roughly 3.25 in, predicting ~115 keV; a wider pole or smaller gap directly buys energy as B^2R^2.
-
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; stability requires 0 < n < 1; f_axial = sqrt(n)*f0, f_radial = sqrt(1-n)*f0Source, quote & tabletop applicability
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
Tabletop: Map n(r) on the 8-in poles; any region where field rises with radius (n<0) defocuses axially and kills the beam.
-
Shape the field to fall approximately linearly 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.
total radial field decrease: 3-4% (small cyclotrons), ~2% (15-20 MeV), ~1% (very large)Source, quote & tabletop applicability
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
Tabletop: The reference machine is the 'small, few-turn' case: aim for a smooth 3-4% droop center-to-edge rather than a flat field.
-
Design the n(r) profile to rise roughly linearly from 0 at center to ~0.02 where fringing begins, reaching ~0.4 at the exit-slit radius and 1.0 at the maximum-energy radius; place the septum just inside the max-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 & tabletop applicability
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
Tabletop: Scale directly: on 8-in poles keep n tiny out to ~3 in radius and take the beam off where n has climbed to ~0.4.
-
Machine pole faces parallel to about 1 part in 50,000 of the pole diameter; a rigid stack of machined blocks needs few bolts, with dowel pins for alignment.
parallelism tolerance ~ D_pole / 50,000Source, quote & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 193
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: At 5.9 kG straight cylindrical poles are fine; only if a next machine pushes past ~12-15 kG does pole taper start paying for itself.
-
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 & tabletop applicability
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
Tabletop: On 8-in poles the historical ratio suggests a ~1-in gap; every extra 1/4 in of gap costs both field (amp-turns) and usable radius.
-
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 & tabletop applicability
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
Tabletop: A modern current-regulated supply meets this easily, but verify ripple and thermal drift: 0.1% of 5.9 kG is 6 G, comparable to the whole shim budget.
-
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, largest ~ pole diameter, stacked concentricallySource, quote & tabletop applicability
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
Tabletop: Scaled to 8-in poles: a stack of 0.020-in disks of roughly 1.2, 2.8, 3.6, 4.4 in diameter is a proven starting recipe for the 2-4% droop.
-
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 & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 196
Tabletop: A small edge ring (order 0.15 x 0.05 in scaled, or trimmed empirically) can extend the reference machine's usable radius, but re-check the field plot at every operating current.
-
Hold azimuthal field variation below 0.1 to 0.2 percent on every circle of constant radius, most critically near the exit radius; 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 & tabletop applicability
Most operators agree that a variation of less than 0.1 to 0.2 per cent is desirable ... After careful correction by use of sector-shaped and wedge-shaped shims, the errors were reduced to less than 0.1 per cent.
Livingston & Blewett, Particle Accelerators (1962) — p. 196-197
Tabletop: 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.
-
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, and recenter it by trimming excitation of the upper coil relative to the lower.
two identical coils in series opposition straddling midplane; balance point = magnetic median planeSource, quote & tabletop applicability
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
Tabletop: The beam follows the magnetic plane, not the machined one; with separate top/bottom coil circuits (or a resistor across one layer) the builder can steer it back to mid-gap.
-
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 & tabletop applicability
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
Tabletop: The single strongest process lesson for a next machine: map first, shim from data - a weekend of Hall-probe mapping replaces months of trial-and-error beam chasing.
-
Local field defects have local fixes: a 0.5 percent weak spot (e.g., casting blowhole) is corrected with a small spot shim; a fundamental (once-around) azimuthal sinusoid means non-parallel poles or an off-center measurement pivot.
Source, quote & tabletop applicability
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
Tabletop: Read the harmonic content of azimuthal maps like a diagnosis chart: 1st harmonic = tilt/centering, higher harmonics = discrete iron defects needing taped-on trial shims, then permanent installation.
-
Below ~10 kilogauss the gap field is linear in excitation, B = mu0*Ni/g; above that apply an efficiency factor K (about 0.73 at 18 kG) because iron reluctance and leakage grow.
B = K*mu0*Ni/g; K ~ 1 below 10 kG, ~0.73 at 18 kG; 10 kG in a 10 cm gap needs 7.95e4 ampere-turnsSource, quote & tabletop applicability
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
Tabletop: At the reference machine's 5.9 kG the linear formula is trustworthy: ~1.4e4 ampere-turns for a 3 cm gap; headroom for a hotter field on the next machine is cheap until ~10 kG, expensive after.
-
Expect the usable field to end about half a gap-length inside the pole edge (0.45g with edge shims, 0.6g without), where 'usable' means field within ~2 percent of central value.
R_useful ~= R_pole - (0.45 to 0.6)*g; boundary moves inward at high B due to pole-corner saturationSource, quote & tabletop applicability
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
Tabletop: With a 1.2-in gap on 8-in poles the builder loses ~0.6 in of radius to fringing; shrinking the gap or adding ring shims recovers usable radius.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The reference machine's observed resonance peak vs magnet current is a magnetization-curve measurement of their own magnet - log it at every retune.
-
A 'dished' (saucer-shaped) median plane indicates asymmetric iron, asymmetric coil placement, or a shorted turn; flatten it by paralleling a resistor across one coil layer to trim its current.
Source, quote & tabletop applicability
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 ... At MIT such a 'dished' median plane was corrected by connecting an external resistor in parallel with one of the coil layers.
Livingston & Blewett, Particle Accelerators (1962) — p. 288
Tabletop: Rebar in the floor or a nearby steel bench can dish an H-frame tabletop field; check for it and trim electrically rather than re-machining.
-
Field strength scales inversely with gap: shrinking the pole gap from 3.8 cm to 1.3 cm was expected to raise the same magnet from ~0.49 T to ~0.75 T; energy gain is quadratic in B so small gap reductions pay twice.
B ~ 1/g (fixed MMF); T_final ~ B^2Source, quote & tabletop applicability
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
Tabletop: 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.
-
Expect the usable uniform-field region of a flat-pole magnet to extend to only about 80% of the pole radius (measured: 0.493 T uniform to 1% out to 6.19 cm on 7.6 cm radius poles); size the dee to sit inside it.
r_uniform(1%) ~ 0.8 * r_poleSource, quote & tabletop applicability
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
Tabletop: Matches the reference machine's 8 in poles: plan for a usable beam radius of ~3.2 in unless shims extend the flat region.
-
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 with 8 cm radius poles yields E = q^2*B^2*r^2/(2m) ~ 1.96 MeV protons.
KE = q^2*B^2*r^2/(2m); 2.7 T, r=0.075 m -> 1.96 MeVSource, quote & tabletop applicability
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
Tabletop: 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.
-
Taper the pole from a wider stem to a narrower face and leave a thick shoulder at the face, then add peripherally placed steel shims for uniformity: Iowa State tapered 12-inch pole stems down to 10-inch pole faces with a 0.7-inch-thick shoulder at the face.
12 in stem -> 10 in face (1.2:1 taper), 0.7 in shoulder at pole face, plus peripheral steel shimsSource, quote & tabletop applicability
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 ... 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
Tabletop: A concrete, machinable geometry for concentrating flux into an 8-10 inch pole face at ~1.7 T; the shoulder plus edge shims are what flatten B(r) near the outer orbit.
-
Plan roughly 20 kW of DC coil power (water-cooled hollow copper tubing on a 2-ton mild-steel core, 33-inch-diameter coils) to hold 17 kG across a 10-inch pole gap.
20 kW dc from motor-generator sets into water-cooled hollow-copper coils, 33 in coil diameter, 2 ton mild steel core, 2.5 tons totalSource, quote & tabletop applicability
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
Tabletop: Sets the scale of the jump from the reference machine's 0.59 T solid-copper-tubing magnet to a 1.7 T machine: hollow conductor and real water cooling become mandatory, and power goes to tens of kW.
-
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 & tabletop applicability
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
Tabletop: This is the closest historical analogue to a next machine's target: same pole diameter as the reference machine, ~3x their field and ~10x their dee voltage buy ~10x the energy.
-
Regulate magnet current, not field, with a precision shunt feeding a difference amplifier against a reference: this held 17,000 gauss to +/-4 gauss (2.4e-4), which is the stability the cyclotron resonance condition demands.
+/-4 G on 17,000 G = 2.4e-4 stabilitySource, quote & tabletop applicability
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
Tabletop: Sets a concrete stability target for a home magnet supply: a few parts in 10^4, achievable with a shunt, op-amp and pass bank.
-
Use an NMR (proton/lithium) magnetometer for absolute field, readable to 1 gauss, and reserve the Hall probe for mapping - a Hall gaussmeter alone is not accurate enough to set the resonance condition.
NMR field meter resolution ~1 gauss on 17 kGSource, quote & tabletop applicability
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
Tabletop: A cheap DIY NMR gaussmeter (coil, oscillator, water sample) is a well-known amateur build and would let the builder set f = qB/2*pi*m exactly.
-
Hold pole-gap parallelism to better than 0.005 in at any radius; gap-height error is field error.
gap variation < 0.005 in over full poleSource, quote & tabletop applicability
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
Tabletop: Scaled to the reference machine's 8 in poles and ~2 in gap, a few-thousandths flatness/parallelism spec is achievable on a decent mill and is the tolerance to ask a machinist for.
-
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 at 84-97% of pole radius) - plus external stacked pyramid discs (1/16 in steps) for the bulk profile.
Rose rings 1/4 in x 2 in at r/R ~ 0.85-0.97; external shim pyramid of 1/16 in discs of decreasing radiusSource, quote & tabletop applicability
Magnetic shimming consists of internal Rose rings and external stepped shims... The rings are 1/4 inch thick and 2 inches wide.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 10-11
Tabletop: 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.
-
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% - carbon is the impurity that most degrades permeability.
C ~ 0.12% (low-carbon steel, 1010-1020 class or better)Source, quote & tabletop applicability
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
Tabletop: A concrete steel spec to hand a supplier for a next machine's yoke stock: 1010/1018-class low-carbon steel is fine; avoid high-carbon or unknown scrap for pole tips.
-
Size the yoke return-path (arm) cross-section 25% larger than the pole so the arms run at only ~75% of pole flux density (1.2 T vs 1.6 T) and never saturate first.
A_arm = 1.25 * A_pole -> B_arm = 0.8 * B_poleSource, quote & tabletop applicability
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
Tabletop: A ready sizing ratio for a next machine's H-frame: make every return-path section at least 25% larger in area than the pole face.
-
Machine a slight convex taper of about 0.02 inch from pole center to edge to create the radially decreasing field needed for weak (betatron) focusing.
pole taper ~0.02 in (0.5 mm) center-to-edgeSource, quote & tabletop applicability
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
Tabletop: A concrete starting number for 8-12 inch poles; the same 0.02 in figure was used on 12 inch poles at 1.6 T, so it scales directly to a next machine.
-
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 & tabletop applicability
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
Tabletop: Trivial machining step for a next machine's pole tips that buys margin against edge saturation at higher fields.
-
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 & tabletop applicability
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
Tabletop: Gives the builder a sanity band for their own field maps: a few percent droop is by design, much more costs resonance synchronism.
-
Size the coil from NI = B*g/mu0 using the gap alone; 1.6 T across a 2.13 in gap required 720 total turns at 110 A (~79 kA-turns).
NI = B*g/mu0; example: 1.6 T x 0.054 m / mu0 ~ 6.9e4 A-turns (they used 720 x 110 A)Source, quote & tabletop applicability
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
Tabletop: Same sizing equation the reference machine's 538-turn magnet obeys; lets them trade gap, turns, and current for any next machine's target field on one line.
-
Design the peak gap field no higher than about 1.6 T, since common iron/steel magnetically saturates near 1.7 T and further excitation is wasted.
B_design <= 1.6 T; B_sat(1060 steel) ~ 1.7 TSource, quote & tabletop applicability
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
Tabletop: Directly applicable: at 0.59 T the builder is far from saturation, but a next machine pushing past ~1.5 T must budget yoke cross-sections against the 1.7 T ceiling.
-
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 & tabletop applicability
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
Tabletop: If a next machine uses NdFeB anywhere (source magnets, PM cyclotron study), this back-of-envelope method sizes gap flux without FEA - but trust it for totals, not point fields.
-
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 & tabletop applicability
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
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 15-16
Tabletop: Mostly a curiosity at cyclotron-gap geometry (where the gap dominates and cladding gains little), but valuable for compact PM ion-source or steering assemblies.
-
A Halbach 'magic cylinder' delivers a transverse bore field Bw = Br*ln(R2/R1); 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 and no stray field.
Bw = Br*ln(R2/R1); practical max ~2*BrSource, quote & tabletop applicability
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
Tabletop: 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.
-
Open (non-enclosed) permanent magnet field sources are practical only when the required gap field is less than about half the material remanence; above that, flux confinement (cladding or closed yoke) is mandatory.
B_gap,open <~ Br/2Source, quote & tabletop applicability
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
Tabletop: Quick feasibility screen: with Br ~ 1.3 T NdFeB, an open PM assembly tops out near ~0.6 T in a usable gap - marginally at the reference machine's current field, insufficient beyond.
-
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 & tabletop applicability
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
Tabletop: Same lesson as Tanabe from the PM side: all quick hand methods assume unsaturated iron, another reason to keep a next machine's yoke flux under ~1.5 T.
-
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 & tabletop applicability
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
Tabletop: Practical warning: alnico horseshoe magnets salvaged for a PM gap lose field every time the circuit is opened for chamber access; NdFeB tolerates gap changes reversibly.
-
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 (Bg*R)^2 = (Bm*mu*Hm)*Vm/(Lg*pi), and the PM works hardest at Bm = Hm = Br/2.
Bg = (Bm*mu*Hm)*Vm/Vg; (Bg R)^2 = (Bm mu Hm) Vm/(Lg pi) ~ particle energy; max (Bm x Hm) at Bm = Hm = Br/2Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The hill/valley ratio (~4.6:1) and 45-degree sector angle are directly scalable to an 8-12 inch AVF pole set; iron saturation, not coil power, is the ceiling.
-
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 & tabletop applicability
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
Tabletop: Gives the gap ratio for a first AVF pole-tip design; a deep valley is also where an amateur puts the Dee/RF and pumping.
-
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 & tabletop applicability
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
Tabletop: Design in adjustability (a gap or shim you can still reduce after measuring), because your FEMM answer will be a few percent optimistic too.
-
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 iterations from flat gap to isochronous <B>(r) over r = 0-36 cmSource, quote & tabletop applicability
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
Tabletop: Budget several map-machine-remap cycles for a next machine's pole profile; it is normal, not a sign of a bad design.
-
For permanent-magnet designs, allow for a field temperature coefficient of about -0.07%/degC and residual field of ~560 gauss in the 'off' state; that residual is low enough that the magnet can still be disassembled by hand.
dB/B = -0.07%/degC; residual field 560 G max at nominal-zero settingSource, quote & tabletop applicability
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
Tabletop: A PM cyclotron in an unheated garage will drift off resonance with the seasons: 10 degC swing = 0.7% field change, far more than the few-parts-in-10^4 the resonance wants.
-
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 & tabletop applicability
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 ... 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
Tabletop: A ten-fold reduction in orbit wander for the cost of drilling a second, unused hole - directly applicable to any asymmetric feature in the reference machine's pole or chamber center.
-
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 & tabletop applicability
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
Tabletop: The correction term is exactly what bends the reference machine's excitation curve at high current; measuring B vs I against this formula reveals where the yoke saturates.
-
Choose yoke topology by trade-off: C-core gives easy access but needs pole shims and is less rigid; H-core is symmetric and rigid but still needs shims; window-frame gives the best field quality with no shims but worst access.
Source, quote & tabletop applicability
'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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Edge shims are how a next machine can widen its flat-field fraction beyond the bare ~80% of pole radius without bigger poles.
-
Judge dipole field quality with the plot (By(x)-By(0))/By(0); precision machines hold ~1e-4 over the good-field region, and a chart of the whole gap at +/-0.01% contours is the standard deliverable of a field computation.
dB/B ~ +/-1e-4 (storage-ring grade); amateur target more like 1e-2-1e-3Source, quote & tabletop applicability
typically +/- 1:104 within the 'good field region' of -12mm <= x <= +12 mm.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 41, 43
Tabletop: Sets the metric (not the number - a cyclotron needs far less) by which the builder should present their own field maps: normalized deviation over the beam region.
-
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)Source, quote & tabletop applicability
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
Tabletop: The mathematically optimal version of the Cyclotron Kids' 45-degree chamfer; worth machining on a next machine's pole edges if the builder pushes past ~1.4 T.
-
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 & tabletop applicability
pressure @ 0.5T 99,472 Newton/m2... ~ 1 atmosphere
Tabletop: 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.]
-
Estimate magnet stored energy as U = B^2/(2*mu0) * (gap volume) and inductance as L = 2U/I^2; the ramping voltage needed is V ~ B*N*a*L/dt, 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 = 2U/I^2; V = B0*N*a*L/dt + IRSource, quote & tabletop applicability
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.
Tabletop: Quick check on a next machine's supply matching: stored energy in a 10 inch, 1 T, 5 cm gap magnet is ~100s of joules, and turns count trades current for voltage against whatever surplus supply the builder finds.
-
Reduce unwanted fringe/leakage field primarily by making the yoke and return legs as thick as possible: the leaked field scales with (B_iron/mu) of the return path, so an unsaturated fat yoke leaks least.
B_fringe ~ (B_iron/mu) * (L_iron/L_fringe)Source, quote & tabletop applicability
This reduction is accomplished by reducing the saturation by making the yoke and back leg of the septum magnet as thick as possible.
Tabletop: Justifies generous H-frame cross-section on the next machine: extra return-path steel is the cheapest way to keep stray field away from ion gauges, turbo pumps and CRT-era instruments on the bench.
-
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; an approximately parabolic chamfer depth, found empirically, cancels it.
fringe length ~ h at pole end, varying ~quadratically across widthSource, quote & tabletop applicability
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.
Tabletop: 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.
-
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; and be aware POISSON's mesher is weak for detailed geometry.
Source, quote & tabletop applicability
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.
Tanabe, Iron Dominated Electromagnets, Lecture 4: POISSON — A Two-Dimensional Magnetostatic Solver (2005) — p. 10, 19
Tabletop: Saves hours on shim-profile studies where dozens of geometry variants are compared; also justifies using FEMM instead for fiddly shim shapes.
-
Use the free LANL POISSON/PANDIRA/AUTOMESH/WFSPLOT chain for 2-D magnet cross-sections: AUTOMESH builds the mesh from a text file, POISSON relaxes the vector potential (PANDIRA diagonalizes instead), and WFSPLOT draws geometry and equipotentials.
workflow: .am text file -> AUTOMESH -> Tape35 -> POISSON or PANDIRA -> WFSPLOT / OUTPOISource, quote & tabletop applicability
It is a public access code (it's free), maintained under contract with DOE by Los Alamos National Accelerator Laboratory (LANL) personnel.
Tabletop: Free tool that runs on a PC and is the same code the Houghton thesis used - the standard amateur path to pole-profile design.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: Halves the mesh and run time for the symmetric H-frame cross-section the builder would model.
-
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, so a hobbyist modelling ordinary mild-steel plate can use the default material without measuring a BH curve.
mat=1 air; mat=2 iron (generic BH ~ 1010 steel); mode=0 selects finite permeability from a tableSource, quote & tabletop applicability
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.
Tabletop: Removes the main excuse for not simulating: home-built yokes are usually A36/1018 mild steel and the default curve is close enough for first-pass design.
-
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 & tabletop applicability
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.
Tabletop: The two mistakes that make a first POISSON run fail; also shows amp-turns (not turns and amps separately) are what the model needs.
-
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 & tabletop applicability
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
Tabletop: Lets the builder size a next machine's amp-turns to ~2% accuracy with hand arithmetic before any FEA.
-
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 & tabletop applicability
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.
Tabletop: Single-point grounding of the yoke also matters on a solid-core machine carrying RF and HV nearby - one deliberate ground, no accidental loops.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Accelerator magnet alignment norms: hold transverse and vertical position to about +/-250 um, longitudinal to +/-500 um, and roll/pitch/yaw to +/-0.2 mrad - and build the fiducials and adjusters in from the start, because retrofit is prohibitively expensive.
+/-250 um transverse/vertical; +/-500 um longitudinal; +/-0.2 mrad rotationsSource, quote & tabletop applicability
Magnet alignment specifications... typically call for < +250 um precision transversely and vertically and < +500 um longitudinally... The cost of retrofit is high.
Tabletop: 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.
-
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 & tabletop applicability
A true kinematic support system must have at least and at most six linearly independent supports.
Tabletop: A next machine's stand with three adjustable feet plus lateral stops gives repeatable leveling of the median plane without fighting a warped frame.
-
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 & tabletop applicability
Solid iron yokes are often used in simple, flat pole contour magnets.
Tabletop: Settles the question for a next machine: a one-off DC cyclotron magnet should be solid steel; laminations buy nothing at quantity one.
-
Iron B-H properties vary with carbon content from heat to heat, with position in the pour, and with rolling direction - order non-oriented steel, and cut all flux-path pieces for one magnet from the same heat/plate when possible.
Source, quote & tabletop applicability
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).
Tabletop: Practical purchasing rule: buy a next machine's pole and yoke stock as one lot from one heat, and expect top/bottom asymmetry if pieces come from different sources.
-
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 & tabletop applicability
IV > 150 V-Amperes or I > 30 Amps or V > 130 Volts or when the magnet stored energy is > 5 joules.
Tabletop: The reference machine's magnet exceeds several of these thresholds; a simple sheet-metal or polycarbonate coil cover including the hot cooling fittings brings the machine to lab-standard electrical safety.
-
Set the isochronous shim correction from the measured orbital-frequency error using dB(r)/B(r) = gamma(r)^2 * df_p(r)/f_p(r) - shim the field by the square of gamma times the fractional frequency error at each radius.
dB(r)/B(r) = gamma(r)^2 * df_p(r)/f_p(r)Source, quote & tabletop applicability
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
Tabletop: At 160 keV-1 MeV gamma ~ 1.0002-1.001, so isochronism errors are dominated by mechanical field errors, not relativity - this formula converts the reference machine's measured phase-slip vs radius directly into required shim thickness profile.
-
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 & tabletop applicability
The maximum kinetic energy T determines magnetic rigidity: B*rho = sqrt(T^2+2T*E0)/(300*Z)
Zaremba, Magnets for Cyclotrons (2005) — p. 19
Tabletop: 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).
-
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 & tabletop applicability
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
Tabletop: Frames the central tradeoff for a next machine: shrinking the reference machine's gap raises B for the same 538 turns, but everything (dee aperture, ion source, probe) must still fit and pump through it.
-
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 & tabletop applicability
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
Tabletop: The most common amateur failure mode is a magnet that works but leaves no port for the probe or pump; run this five-item checklist on every layout iteration for a next machine.
-
Do first-pass cyclotron magnet numbers analytically: 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, 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 & tabletop applicability
coil cooling estimation: dT(C) = 60*P(kW)/(4.19*N(l/min))
Zaremba, Magnets for Cyclotrons (2005) — p. 30-32
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: If a next machine goes AVF to escape the weak-focusing energy ceiling, these are proven starting numbers: 3 or 4 sectors, half-open valleys, and a modest nu_z ~ 0.2 target.
-
Follow the iterative magnet design loop: rough model, hand calculations, 2-D field code, then 3-D field code - and expect a good 3-D model to agree with measurement to better than 3%.
3-D calculation vs measurement < 3%Source, quote & tabletop applicability
calculation results and measurements differ less than 3 percent
Zaremba, Magnets for Cyclotrons (2005) — p. 4, 35
Tabletop: The reference machine's Poisson/FEMM workflow is the professional one; a >3% mismatch between model and Hall-probe map means the model geometry or BH data is wrong, not the method.
-
Target field homogeneity of dB/B <= 0.01% over the good field region of a dipole (0.1% for a quadrupole gradient) - 'reasonable but nevertheless challenging'.
dipole: (By(x,y)-By(0,0))/By(0,0) <= 0.01%Source, quote & tabletop applicability
Achieving the following homogeneity values is reasonable but nevertheless challenging. Dipole: dB/B0 <= 0.01%
Tabletop: A useful upper bar; a weak-focusing cyclotron deliberately wants a controlled radial gradient, but azimuthal variation should be held near this level to avoid a first harmonic.
-
Build the aperture budget as: good field region + vacuum chamber wall (0.3-2 mm) + installation/alignment margin (0-5 mm), with 5-10 mm extra allowed for orbit distortion in the good field region itself.
aperture = GFR + chamber wall (0.3-2 mm) + margin (0-5 mm); GFR includes 5-10 mm closed-orbit allowanceSource, quote & tabletop applicability
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).
Tabletop: Explains why the pole gap must exceed the chamber's internal height by a centimetre or so; useful when trading gap (and hence amp-turns) against chamber wall thickness.
-
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.
NI_per_pole = B*h/(2*eta*mu0); eta ~ 0.99; mu0 = 4*pi*1e-7Source, quote & tabletop applicability
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.
Tabletop: First-cut sizing for a next machine: at a 2 cm gap and 1.0 T you need ~8000 A-turns per pole, which sets conductor/current density before any FEMM run.
-
Size the iron cross-section so the flux density in the yoke stays below 1.5 T and the yoke reluctance is under about 1% of the gap reluctance (lambda/mu_iron < 0.01 h/mu0); follow this and circuit efficiency exceeds 99%.
B_iron < 1.5 T; lambda/mu_iron < 0.01 * h/mu0 -> eta > 99%Source, quote & tabletop applicability
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%.
Tabletop: The single most useful yoke-sizing rule for an H-frame homebuilt magnet: pick return-leg area = flux/1.5 T and the magnet behaves predictably.
-
Approximate the magnetic (effective) length as l_mag = l_iron + 2*h*k with k between 0.3 and 0.6; k shrinks when pole width is smaller than the gap, when poles saturate, or when coil heads sit close to the beam.
l_mag = l_iron + 2 h k, k = 0.3-0.6Source, quote & tabletop applicability
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.
Tabletop: Quantifies the fringe-field bulge at the pole edge - the region where a tabletop cyclotron's outermost orbits actually live.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
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); L = 2U/I^2; V_tot = RI + L dI/dtSource, quote & tabletop applicability
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)
Tabletop: Tells you the inductance and therefore how fast a bench supply can ramp the magnet and how big the flyback/crowbar protection must be.
-
Choose magnet topology by field quality: window-frame gives homogeneous field even without shims, H-magnets are symmetric and lighter than C-magnets but need transverse shims, and a C-magnet inherently produces a ~0.1% gradient across the pole plus 'forbidden' even harmonics.
C-magnet: ~0.1% gradient across pole vs central field, harmonics n = 2,4,6Source, quote & tabletop applicability
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.
Tabletop: 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.
-
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 cannot be pulsed 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 & tabletop applicability
Sheet thickness 0.3 <= t <= 1.5 mm ... Coercivity Hc < 65 A/m ... Coercivity spread dHc < +/- 10 A/m
Tabletop: 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.
-
Always cycle the magnet up to maximum current before settling at the operating field, whatever field you need, so hysteresis and remanence are reproducible; zero the field with demagnetization cycles rather than by trusting zero current.
Source, quote & tabletop applicability
In normal operation, the magnet is always cycled to its maximum value, irrespective of the required field, to ensure that hysteresis effects are reproducible.
Tabletop: Free operational fix for run-to-run field shifts in a home cyclotron - important because resonance is set by B and the beam vanishes on a few-gauss error.
-
Estimate the mean turn length as l_avg = pole perimeter + 8 x (clearance between pole and coil) + 4 x coil width, and sanity-check it against 2.5*l_iron < l_avg < 3*l_iron for racetrack coils.
l_avg = pole perimeter + 8*clearance + 4*coil width; 2.5 l_iron < l_avg < 3 l_ironSource, quote & tabletop applicability
l_avg = pole perimeter + 8 x clearance between pole and coil + 4 x coil width
Tabletop: Gives copper length, hence resistance and power, straight off a sketch - exactly what a garage builder needs before ordering tubing.
-
Pick current density from the cooling method: <=1 A/mm^2 for bulky air-cooled coils buried in the yoke, <2 A/mm^2 for small thin air-cooled coils, and ~10 A/mm^2 as the conservative standard for direct water-cooled hollow conductor (80 A/mm^2 is possible but wrecks reliability).
air: j <= 1-2 A/mm^2; water: j ~ 2-10 A/mm^2; j > 10 A/mm^2 implies multiple parallel circuits and erosion riskSource, quote & tabletop applicability
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
Tabletop: The reference machine's 538-turn solid copper tubing coils sit in the air-cooled regime; this rule says they must stay under ~1-2 A/mm^2 unless they switch to hollow conductor with water flow.
-
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 & tabletop applicability
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.
Tabletop: Gives hard numbers for a home chilled-water loop: exceed 5 m/s and you erode the tubing; exceed 60 C and the insulation ages fast.
-
Use the closed-form water-cooling recipe: 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.
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)^0.571Source, quote & tabletop applicability
Q_water = 2.388 x 10^-4 P/dT ... d = 5.59 x 10^-3 (P/(dT Kw))^0.368 (l/dp)^0.21
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: One-line check of the reference machine's 538 turns: at 0.59 T and their gap this formula predicts the required current within a couple percent if the H-frame iron is unsaturated; a measured efficiency well below ~95% signals a saturated or gappy flux path.
-
Choose magnet steel with carbon <= 0.10% (1010 steel); its BH curve becomes highly nonlinear above B ~ 1.5 T and is fully saturated (mu -> 1) by B ~ 2.0 T, so keep working iron flux density below ~1.5 T for linear, reproducible excitation.
1010 steel: nonlinear for B >= 1.5 T, fully saturated at B >= 2.0 TSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 - all three prevent local saturation that makes field shape change with excitation.
Source, quote & tabletop applicability
At high fields, the top of the pole can saturate. The right hand figure illustrates a tapered pole which is wider at the top... a radius at the pole corner, reducing this magnetic flux stress concentration.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 251-252
Tabletop: Cheap insurance for the next machine's pole design: a root taper and corner radius cost one lathe operation and keep the field map valid from low current to full excitation.
-
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 & tabletop applicability
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
Tabletop: Tells the builder where their usable field really stops on an 8 inch pole: with a ~2 inch gap the field is already dying ~1 inch inside the pole edge, which sets the practical maximum orbit radius and extraction geometry.
-
When end-chamfering poles to fix the integrated field, machine the computed depth distribution at a 45 degree angle - the angle itself is unimportant, but 45 degrees splits the corner into two equal half-angles and minimizes local saturation.
chamfer depth Delta-z(x) from measured Leff(x); cut angle 45 degSource, quote & tabletop applicability
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.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 253-254
Tabletop: If the next machine's pole edge is chamfered or radiused to soften the field falloff for extraction, use ~45 degrees and bolt-on machinable end pieces so the shape can be iterated (Tanabe converged in two iterations on SPEAR3).
-
Improve dipole field flatness by adding smooth bumps (shims) near the pole edges rather than widening the pole; the bumps squeeze flux through a locally narrower gap and extend the uniform-field fraction of the aperture while reducing corner saturation.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Do not use plain radial-sector pole tips on a small machine: measured on the Rutgers 12-inch, radial sectors give the steepest average-field falloff with radius - so steep it is unusable - while spiral sectors compromise 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 & tabletop applicability
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
Tabletop: Direct guidance for a next machine's pole-tip upgrade at the 8-12 inch scale; also warns that narrow spiral vanes saturate at large radius (measured field fell below simulation).
-
Screen candidate pole-tip designs with just two numbers derived 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) - and reserve full phase-space tracking for the final one or two contenders.
nu_z^2 ~= n + F^2 (N^2/(N^2-1)); n = field index, F = flutter, N = AVF periodicitySource, quote & tabletop applicability
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
Tabletop: A cheap, quantitative design filter that works from measured maps of a home-built magnet, no orbit code required.
-
Build the mapping stage for ~800 steps/inch (1.8 deg/step motor on a 0.25 in-pitch double-lead screw), run the steppers at 25% of rated current with ramped velocity, and take readings only while moving in the forward direction to kill backlash.
800 steps/inch = 200 steps/rev / 0.25 in pitch; motor current = 25% ratedSource, quote & tabletop applicability
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
Tabletop: A 1/800 inch (0.03 mm) grid is more than enough for an 8-12 inch pole and is buildable from surplus stepper/leadscrew parts.
-
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 & tabletop applicability
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
Tabletop: Directly applicable: any DIY gaussmeter-plus-stepper mapper on an 8-inch magnet needs this calibration or the map carries 1% systematic error.
-
Fiducialize the field map with five small excited iron needles placed on a known circle around the pole: four to calibrate x and y scale, and a fifth off-symmetry to resolve the axis-inversion ambiguity that plotting software introduces; locate each bump by fitting a 2-D Gaussian.
5 needle bumps, <100 gauss each, measured with main magnet de-energized; bump-pair spacing recovered as 2.500 in vs 2.500 in mechanicalSource, quote & tabletop applicability
Four needles were used to scale both dimensions; the fifth needle was used to break the symmetry, removing orientation ambiguities.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 3-4
Tabletop: Trivially cheap (iron nails plus a few turns of magnet wire) and it ties the field map to the mechanical chamber center, which is what you actually need for placing the ion source and target.
-
Before trusting a two-scan (magnet-off then magnet-on) mapping procedure, prove stage 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 within the 0.0000-inch resolution of a digital dial indicator.
1600 travel manipulations / 2.4e6 motor steps -> return error < 0.0001 inSource, quote & tabletop applicability
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
Tabletop: Cheap insurance: an afternoon of cycling the homemade stage validates every field map you take afterwards.
-
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 the center shifts by less than the data noise.
minimize sigma(Bz) around circle vs center position; Rutgers centers from different radii agreed to 1e-4Source, quote & tabletop applicability
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
Tabletop: 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.
-
For an AVF (sectored) field, pick a reference circle of about half the maximum ion radius, FFT Bz around it, and move the circle center to maximize the Nth harmonic (N = number of hill/valley pairs) while minimizing harmonics 2, 3 and 5.
reference circle radius = 0.5 x r_max (2.5 in for a 5 in max ion radius); maximize 4th harmonic for a 4-fold AVFSource, quote & tabletop applicability
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
Tabletop: 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.
-
Ferromagnetic yokes stop paying off above saturation (~2 T): effective permeability collapses toward 1 and the field pattern reverts to that of the bare coil - iron-dominated designs should stay comfortably below 2 T.
mu_r -> 1 for B >> ~2 TSource, quote & tabletop applicability
ferromagnetic materials lose their advantages above their saturation field (typically 2 T).
Humphries, Principles of Charged Particle Acceleration (1986) — p. 104, 108
Tabletop: Defines the absolute ceiling of the iron-magnet approach for a next machine (~1.6-1.8 T practical); beyond that only superconductors or air-core help.
-
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 & tabletop applicability
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
Tabletop: Numerically the same worked example the builder needs: their 538 turns at ~30 A across ~5 cm predicts ~0.4 T ideal - the shortfall vs measured maps the iron's contribution.
-
Fringe and deflection fields extend beyond a gap or electrode pair a distance comparable to the gap/electrode spacing itself (Laplace-equation scale length) - this sets fringe allowance at pole edges and is why extraction requires a septum to terminate the deflector field.
fringe extent ~ gap width gSource, quote & tabletop applicability
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
Tabletop: Rule of thumb for a next machine's layout: reserve roughly one gap-height of radius at the pole edge as unusable fringe, and shield any deflector with a grounded septum.
-
An inclined sector-magnet edge focuses vertically with focal length f = r_g/tan(beta) (r_g = gyroradius, beta = edge angle): rotating an exit edge is a free vertical lens for extracted beamlines.
f_vertical = r_g/tan(beta)Source, quote & tabletop applicability
fx = (gamma mo vz/qBo)/tan beta = rgo/tan beta.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 141
Tabletop: If a next machine ever extracts a beam, angling the magnet exit edge focuses the diverging beam without any extra magnet.
-
Weak-focusing orbit stability requires field index 0 < n < 1 everywhere in the beam region: n > 0 for vertical focusing, n < 1 to keep radial focusing.
0 < n(r) < 1; nu_r = sqrt(1-n), nu_z = sqrt(n)Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The master sizing formula: the reference machine's 0.59 T at ~0.09 m gives ~135 keV; 1 MeV needs (R*B) ~ 0.144 T-m, e.g. 1.2 T at 12 cm.
-
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 & tabletop applicability
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
Tabletop: Confirms the reference machine's flat-pole H-frame inherently provides weak focusing from its natural radial falloff - the design task is controlling how fast n rises, not creating it.
-
Cyclotron final energy scales as T ~ K*Q^2/A with K = (e*B*rho)^2/(2*m0), so for fixed energy the iron mass shrinks roughly as the cube of the field increase (rextraction falls from 2.28 m at 1 T to 0.76 m at 3 T - a 1/27 volume ratio).
K_B = (e*B*rho)^2/(2*m0); volume ~ (1/B)^3 at fixed energySource, quote & tabletop applicability
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
Tabletop: The B^2 energy leverage argues for pushing the next machine's field toward the iron limit (~1.5-1.8 T) before enlarging poles: doubling B quadruples energy at fixed radius while iron mass stays fixed.
-
Choose the ISM frequency 13.56 MHz (B = 0.889 T for protons) if you want to drive the dee with commercial RF generators and standard 50-ohm hardware through a matching transformer.
f = qB/(2*pi*m): 13.56 MHz protons -> B = 0.889 T; 50-ohm source -> matching network -> high-Z deeSource, quote & tabletop applicability
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
Tabletop: 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 and legal.
-
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.
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 & tabletop applicability
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
Tabletop: Exactly the reference machine's problem class and size: machine a gentle crown or stepped 'lump' into the 8-inch poles (or shim equivalently) targeting ~2-3% center-to-edge fall-off for axial focusing.
-
Respect mechanical constraints when contouring poles: a theoretically better (steeper) profile can be unbuildable because pole thickness at the mounting screws goes to nothing, so blend a flat screw-land rim with a central contoured boss.
example lump model (R=6 in, 3% fall-off): flat rim ~1 in wide, boss height ~0.3 in, boss crown rho ~19.6 inSource, quote & tabletop applicability
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
Tabletop: Directly applicable fabrication pattern for a next machine's contoured pole caps that still bolt on.
-
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 & tabletop applicability
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
Tabletop: Directly frames the next machine's decision: staying at 8 inches keeps it a demonstration machine; nuclear-reaction goals argue for 12-inch-class poles and higher field.
-
Compute magnet excitation from NI = 2.02 x B(gauss) x gap(inches), using the leakage-multiplied total flux for the iron.
NI (ampere-turns) = 2.02 x gauss x inches of gapSource, quote & tabletop applicability
Ampere-Turns = 2.02 x gauss x inches gap
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Tabletop: Directly applicable; e.g. 5900 G x 2 in gap needs ~24,000 A-turns before iron reluctance and leakage corrections.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Run the magnet iron near saturation for most economical performance; expect soft iron to begin saturating near 16 kG, with some irons usable to 21 kG.
B_sat(soft iron) ~ 16 kG; upper limit ~21 kGSource, quote & tabletop applicability
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
Tabletop: Directly applicable; the reference machine's 0.59 T (5.9 kG) gap field leaves large iron margin, so a next machine could roughly double the field before core saturation dominates.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Directly applicable to a next machine's H-frame; coil space usually forces compliance automatically, but check it when shortening the frame.
-
Force saturation to occur in the pole cores only by giving the return yoke at least 25% more total cross-sectional area than the cores.
A_yoke >= 1.25 x A_coreSource, quote & tabletop applicability
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
Tabletop: Directly applicable: for 8-inch (50 in^2) cores, provide >= 63 in^2 of total yoke steel around the flux return path.
-
Machine yoke-to-yoke and yoke-to-core contact surfaces flush to eliminate parasitic air gaps in the magnetic circuit.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable; a few thousandths of an inch of unintended air gap is a noticeable fraction of a small machine's ampere-turn budget.
-
Make vacuum-chamber top and bottom thin steel plates not much larger than the pole diameter (they become pole extensions), and make the side wall non-magnetic (brass) so field is not bypassed.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable chamber architecture for a small machine; every millimeter of chamber wall inside the gap costs ampere-turns.
-
The homogeneous magnetic field is the single most expensive subsystem, and B ~ mu0*NI/g means the gap drives everything: keep the pole gap as small as the vacuum chamber allows, even at the cost of a harder chamber design.
B = mu0*NI/gSource, quote & tabletop applicability
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
Tabletop: The central trade for a next machine: every millimeter of gap saved is field (and energy ~B^2) for free.
-
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: 1.0-1.7 T maps to 15.2-25.9 MHz, with matching capacitance 166 pF down to 57 pF).
f(MHz) = 15.23 * B(T) for protonsSource, quote & tabletop applicability
B (Tesla) 1 ... 1.6 ... f (MHz) 15.23 ... 24.36
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 12
Tabletop: The reference machine's 0.59 T machine resonates at ~9.0 MHz; any next machine's field choice instantly fixes the oscillator/tank tuning range via this 15.23 MHz/T constant.
-
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 & tabletop applicability
Increased cross section reduces flux through yoke to 1.2T
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 8
Tabletop: Simple area-ratio rule the builder can apply when welding a next machine's frame from surplus plate: yoke area ~ 1.3-1.5x pole area keeps 1010-grade steel comfortably linear.
-
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 & tabletop applicability
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
Tabletop: Confirms the standard amateur approach for the reference machine's scale: put the field index into the pole profile (taper/gap growth with radius) rather than relying on accidental fringing.
-
A 300 keV-class proton cyclotron was completed for under $1000 with base pressure 0.01 mTorr, 1.6 kVpp on the dees at ~400 W peak RF, and a C-frame yoke of welded 5x5 inch soft-steel bar with meehanite pole pieces face-milled to a profile giving the appropriate field index.
300 keV: ~1e-5 torr, 1.6 kVpp dee, 400 W pk, machined field-index pole profileSource, quote & tabletop applicability
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
Tabletop: An existence proof at exactly the reference machine's energy: modest dee voltage (1-2 kVpp), 1e-5 torr, and a machined pole profile suffice below ~300 keV; heroic RF and UHV are not prerequisites.
-
For first beam, fix the RF frequency and slowly sweep the magnetic field through the resonance condition while watching the collector - this is how the Rutgers 9-inch prototype found its first beam.
sweep B at fixed f until f = qB/(2*pi*m)Source, quote & tabletop applicability
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
Tabletop: The standard commissioning move for a next machine: B-field is the easy knob to sweep since the RF stays matched at fixed frequency.
-
Keep the field index n below 0.2 everywhere inside the maximum ion radius: n = 0.2 marks the coupled (2*nu_z = nu_r) resonance and, if it lands inside the orbit region, the beam is lost.
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 & tabletop applicability
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
Tabletop: This is the single design criterion for weak-focusing pole shaping on a 100 keV-1 MeV tabletop machine; it is computable from a measured B(r) curve.
-
Keep cyclotron shims thin - Lawrence 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 is lost there.
shim thickness <= 0.25 in (6.35 mm); Houghton modelled 0.3175 / 0.635 / 1.27 cm shims and all were too thickSource, quote & tabletop applicability
the magnetic field changes too quickly near the edge of the shim. This is a result of making the shim too thick.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 25, 44, 46
Tabletop: Warns the builder off the obvious first shimming attempt; the useful shims are thinner than are convenient to fabricate and hold in place.
-
Shape the magnet for a Bz that decreases LINEARLY with radius: a linear falloff makes Br grow linearly with distance from the median plane, giving simple-harmonic axial focusing, so judge every pole/shim/lid modification by the linearity of B(r).
dBz/dr = -C constant -> Br = C z -> SHM about median planeSource, quote & tabletop applicability
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
Tabletop: Gives a single, plottable acceptance test for a shimming attempt on the reference machine's 8-inch poles - no orbit code needed to reject a bad shim.
-
Watch for adding-type trim coil configurations that make B rise with radius out to ~5 cm: that produces a NEGATIVE field index and axial defocusing - worse than doing nothing.
B increasing to r ~ 5 cm -> n < 0 (down to -0.1 in the modelled cases)Source, quote & tabletop applicability
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
Tabletop: A concrete trap when adding any iron or coil near the center of an 8-inch pole; check the sign of dB/dr everywhere, not just at the edge.
-
Do not expect trim coils to rescue weak focusing on a small cyclotron: bucking coils moved n = 0.2 outward by only ~0.2 cm while costing ~20% of peak field (1.27 T to 1.07 T), and since T ~ B^2 that is a losing trade.
dr(n=0.2) = +0.2 cm for dB = -20% (1.27 T -> 1.07 T); T proportional to B^2 r^2Source, quote & tabletop applicability
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
Tabletop: Saves a next machine's builder from spending months on trim coils inside a small gap; also note trim coils steal gap height.
-
Replace non-magnetic vacuum-chamber lids with magnetic stainless-steel lids extending about 2.2 cm beyond the pole/Dee radius: acting as wide pole faces they pull field lines outward, linearize B(r), push n = 0.2 from r = 5.9 cm out to r = 8.3 cm (past the 7.8 cm Dee), and by cutting the effective pole gap from 3.9 cm to 2.54 cm raise Bmax from 1.27 T to 1.77 T.
lid radius = pole radius + 2.2 cm; gap 3.9 cm -> 2.54 cm; B 1.27 T -> 1.77 T; f 27.0 MHz; Tmax 0.41 -> 0.91 MeVSource, quote & tabletop applicability
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.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 54-55
Tabletop: The highest-leverage cheap upgrade in this batch: swapping aluminium chamber lids for steel roughly doubles theoretical proton energy on a machine essentially identical to the reference machine's.
-
Use the free Poisson Superfish (2-D magnet cross-section) plus SIMION 8.1 (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 & tabletop applicability
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
Tabletop: Zero-cost simulation path for a hobbyist; the appendix geometry file is a working starting template for an 8-15 cm pole magnet.
-
Expect beam current to fall steeply with collector radius in an unshimmed weak-focusing machine; add ferromagnetic shims between chamber and pole faces to strengthen magnetic focusing and recover current at large radius.
Source, quote & tabletop applicability
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.
Tabletop: Predicts the current-vs-radius profile the builder should measure, and the standard shim fix if a next machine loses beam before full radius.
-
Iron-pole cyclotrons hit a hard field ceiling when the poles saturate at about 2 T; beyond that, energy grows only with radius, so plan around B <= ~1.8-2 T for any iron magnet.
pole saturation ~2 TSource, quote & tabletop applicability
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
Tabletop: 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), but above ~1.8 T iron stops helping and only pole diameter buys more.
-
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 & tabletop applicability
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
Tabletop: The core magnet-shimming target for the next machine: map B(r) with a Hall probe, compute n(r) by finite differences, and add edge shims until n(r) is a clean 0-to-1 ramp over the dee radius.
-
Budget cooling water across subsystems explicitly: the Houghton 15 cm magnet needed 6.1 L/min at 70 A but the chiller could spare only 3.0 L/min after the diffusion pump's 0.8 L/min, capping operation at 50 A / 1.1 T - the chiller, not the 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 & tabletop applicability
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
Tabletop: 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.
-
Measure n(r) by finite differences of Hall-probe readings on a rotating non-magnetic jig (aluminum disc in the median plane, 1 cm radial steps); approximating dBz/dr by dBz over 1 cm is adequate to reveal where focusing is lost.
n ~ -(r/Bz)*(dBz/dr), dr = 1 cm stepsSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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)
Tabletop: A purchasable-magnet benchmark almost exactly at the reference machine's scale; the 0.8 gpm figure sizes a chiller for a ~kW-class coil.
-
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 & tabletop applicability
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.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Tabletop: 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.
-
Make pole tips removable/swappable inserts (up to 1 in thick, bolted to fixed poles) so field shaping, shimming experiments, and AVF upgrades never require touching yoke or coils.
Source, quote & tabletop applicability
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
Tabletop: Probably the single best architecture decision the builder can copy: a next machine with bolt-on tips can iterate field profiles cheaply.
-
Power the upper and lower coils from independent supplies so a deliberate top/bottom ampere-turn imbalance can steer the magnetic median plane vertically onto the geometric midplane of the dee.
Source, quote & tabletop applicability
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
Tabletop: Cheap beam-height trim for a next machine: two supplies (or a shunt rheostat on one coil) instead of re-machining anything.
-
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 and beam crossing it inside the machine blows up axially.
n(r) = -(r/Bz)(dBz/dr); require n < 0.2 for all r < r_finalSource, quote & tabletop applicability
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
Tabletop: 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.
-
Proof by counterexample: pole tips with n = 0.2 occurring at r = 3.5 in inside a 5 in dee radius produced observable axial beam blow-up - a deliberately 'bad' taper is only ~40% steeper than a good one.
n=0.2 at 70% of dee radius -> axial lossSource, quote & tabletop applicability
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.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 5
Tabletop: Shows how little margin there is between good and bad tapers on an 8-12 inch machine; motivates measuring n(r), not guessing it.
-
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 & tabletop applicability
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
Tabletop: If a next machine ever gets sector pole tips (to allow a rising average field), these two lines are the whole first-order design calculation.
-
To find closed orbits experimentally, toss a current-carrying wire loop (e.g. 30 AWG, ~2.5 A) into the magnet gap: it snaps to and traces stable equilibrium orbits, revealing off-center orbits you would never find analytically.
30 AWG loop, 71 mm circumference, 2.5 ASource, quote & tabletop applicability
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
Tabletop: A zero-cost field-quality diagnostic the builder can run on the existing magnet this weekend.
-
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^2(1+2tan^2 xi) and the matching radial expression, where flutter F^2 = (<B^2>-<B>^2)/<B>^2.
nu_z^2 = n + (N^2/(N^2-1)) F^2 (1 + 2 tan^2 xi); F^2 = (<B^2> - <B>^2)/<B>^2; n = -(r/B) dB/dr = 1 - gamma^2Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
N large: high maximum energy, F small and quasi circular orbits -> spiral compulsory
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 26, 28
Tabletop: Explains when the extra machining pain of spiral tips pays off; at 8-12 inch pole size with N=4 a modest spiral is worth more than more sectors.
-
Use N > 2 sectors in any AVF design: with N < 2 the flutter term makes nu_r^2 negative (the pi stop-band), and each N sets 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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Explains the negative field index a flat-pole tabletop magnet already has - and why a bigger gap gives more weak focusing but less field.
-
Reach for the iron before the copper when shaping the field: iron shaping is very effective, simple, cheap and reliable but highly non-linear and fixed once cut, while trim coils are flexible but very weak in a warm magnet and steal gap height - model either one before implementing it.
Source, quote & tabletop applicability
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
Tabletop: Settles the shim-vs-trim-coil question for a small warm magnet the same way the Houghton thesis did empirically: iron wins.
-
Work through the iron field-shaping catalogue in order: 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 movable iron flaps, or change local saturation with trim rods.
Source, quote & tabletop applicability
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
Tabletop: A ranked menu of things the builder can machine on 8-inch pole tips, each demonstrated on a real cyclotron; movable flaps in particular give post-build adjustability.
-
Choose yoke stock by construction method: laminations are limited to about 300 mm thickness (200 mm usual) but give good, slightly anisotropic magnetic and mechanical properties; castings allow large low-deflection parts with poor mechanical properties and porosity risk; forging is best and most expensive.
laminated stack thickness: 300 mm max, 200 mm usualSource, quote & tabletop applicability
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
Tabletop: 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.
-
Trade pole gap deliberately: a small gap needs fewer ampere-turns and keeps orbits away from the pole edge but leaves no room for probes, injection and pumping and is very sensitive to errors (vertical losses); a large gap eases vacuum and diagnostics at the cost of field.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
Follow the four-step magnet design order - squeeze the requirements, get starting numbers by hand calculation, then 2-D global model, 3-D global model, and 2-D cuts for local details - preferring 2-D calculations at every opportunity and iterating.
step0 requirements -> step1 hand calculation -> step2 2D global -> step3 3D global -> step4 2D radial cutsSource, quote & tabletop applicability
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
Tabletop: A workflow a solo builder can actually execute, and it puts pencil-and-paper (Zickler-style) sizing ahead of any software.
-
In a hill/valley magnet the average field at large radius is <B> = k*B_hill + (1-k)*B_valley with stacking factor k = hill angle/90 deg; RF efficiency prefers k = 0.5 but making the machine smaller pushes k up - C235 chose k = 0.67 (60-degree hills).
<B> = k B_hill + (1-k) B_valley; k = hill angle/90 deg; C235: k=0.67, 0.67*3 + 0.33*(3-2.1) = 2.31 T; B0 = 2.31/gamma(1.25) = 1.8 TSource, quote & tabletop applicability
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
Tabletop: Shows the exact arithmetic used to go from a required <B> to hill/valley fields and sector angle - reusable at any scale.
-
Design to a target axial tune around nu_z = 0.2, which then fixes the spiral angle once n, N and F are known; keeping flutter and spiral modest lets you tolerate 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 & tabletop applicability
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
Tabletop: Gives a numeric focusing target to design toward instead of 'as much focusing as possible' - and 0.2 is achievable with weak focusing at the reference machine's energies.
-
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 & tabletop applicability
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
Tabletop: The core sizing identity for a home magnet: shaving the pole gap buys field for free, whereas making the poles bigger does not.
-
Remember permeability is a strong function of B: for good magnet steel mu_r runs ~4000-5000 at low induction but collapses toward 1 above ~2 T, and 0.9%-carbon steel has a maximum mu_r of only ~1000 versus ~5000 for 99.8% iron - so use low-carbon steel 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 & tabletop applicability
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
Tabletop: Concrete reason to buy A36/1018 low-carbon plate rather than whatever scrap steel is on hand for an H-frame yoke.
-
Model a 3-D sectored magnet in 2-D axisymmetry by using pseudo-materials whose BH curve is scaled by the stacking factor: B_pseudo = mu0*H + k*(B - mu0*H), where k is the fraction of the circle occupied by real material.
B_pseudo = mu0 H + k (B - mu0 H), k = stacking factor (fraction of azimuth filled by iron)Source, quote & tabletop applicability
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
Tabletop: Lets a hobbyist study an AVF pole set in free 2-D codes (POISSON/FEMM) before committing to a 3-D solver.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Practical simulation hygiene: use FEMM/POISSON to compare shim options (differences), and use the Hall probe for the absolute field.
-
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) over the acceleration region and ~2% total to full radius, with azimuthal variation shimmed below 0.2%.
dB/B ~ -1%/13 in over main region; total ~ -2% at r_max; azimuthal ripple < 0.2%Source, quote & tabletop applicability
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
Tabletop: The fractional numbers transfer, not the inches: aim for a smooth ~1-3% total field fall-off center-to-edge on the 8-inch pole and shim azimuthal asymmetry to the few-per-mille level.
-
Machine field-correcting shims from thick steel plate on a boring mill and iterate against field maps; treat shims as the precision trim on a deliberately oversized magnet.
Source, quote & tabletop applicability
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.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 35
Tabletop: Directly applicable method: leave gap allowance for removable machined shim rings/plates so a next machine's field shaping is a measurement-and-remachining loop, not a magnet rebuild.
-
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.
control coils: 65 turns/pole, 0-75 A, reversible polaritySource, quote & tabletop applicability
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.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 35
Tabletop: Directly applicable and cheap for a next machine: a few dozen turns on one pole with a bipolar bench supply gives a knob for vertical beam centering instead of mechanical re-shimming.
-
Site the RF power stage where the stray magnetic field is below ~60 oersteds (map the fringe field first), and line its cabinet with copper to cut losses and interference.
B_stray at oscillator < ~60 GSource, quote & tabletop applicability
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
Tabletop: Directly applicable: map the reference machine's H-frame fringe field with a hall probe and keep the LDMOS amplifier, its magnetics, and instrumentation outside the ~60 G contour.
-
Choose accessibility-driven machine orientation early: the 86-inch put the median plane vertical in a U-shaped (window-frame) magnet purely so a crane could lift the whole dee/liner assembly straight out.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: Direct transfer of tolerancing practice: face-grind a next machine's pole and yoke mating surfaces and check with a dial indicator; magnetic attraction, not atmosphere, is the structural design load.
-
Use plain low-carbon steel for cyclotron iron (ORIC forgings: ~0.11% C, low Si/Ni), from consistent stock, and a conventional closed yoke with pole-base to yoke cross-section ratio near 1:1.
steel ~0.11% C; A_pole_base : A_yoke ~ 1:1 (closed yoke)Source, quote & tabletop applicability
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
Tabletop: Directly applicable: 1018/1010-class steel is the right iron for a next machine, and yoke area comparable to (Wouters says 25% above) pole area is the design corridor.
-
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 & tabletop applicability
Approximately 1/8-scale model magnets were energized ... A complete grid of points 1/4 in. apart is thus obtained over the entire model.
Tabletop: Inverted for the builder: their whole magnet is model-sized, so a dense XY hall-probe map on a ~5 mm grid with attention to probe positioning and current regulation (the two dominant error terms) is the equivalent discipline.
-
Budget field-mapping errors explicitly: probe position error dominates where gradients are steep, and current regulation must be held to ~0.3% or better during a map.
delta-B/B per point: position 0.4%, regulation 0.3%, readout 0.2%; goal 0.1%Source, quote & tabletop applicability
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.
Tabletop: Directly applicable to a next machine's shimming: regulate magnet current (not just set it) while mapping, and index the probe mechanically, or the map noise will exceed the shim effects being measured.
-
When choosing dee voltage, remember it trades against gap size: more volts means fewer turns and better transmission but a larger required breakdown clearance and hence magnet gap; ORIC settled on 100 kV as near-optimal.
V_dee up -> turns down, but gap (breakdown clearance) up -> compromiseSource, quote & tabletop applicability
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.
Tabletop: The coupled optimization transfers: for a next machine, pick dee voltage and magnet gap together, since every kV of dee needs clearance that costs ampere-turns.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
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).
U = rho*(Ni)^2*l*N / (coil volume); q(gpm) = 6.82*U(kW)/dT(F)Source, quote & tabletop applicability
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
Tabletop: If a next machine's coils run hot, the fix is more copper, not more cooling: doubling conductor volume halves dissipation at the same ampere-turns.
-
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 & tabletop applicability
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
Tabletop: Potting the reference machine's coils stops the slow insulation abrasion that coil hum causes; their low coil voltage means the resin-glass numbers alone give ample margin.
-
Cooling water for magnet and RF systems: demineralized, conductivity kept at or below 10 micromho with pH ~7; the dee cooling water must be temperature-stable to 1 F or the RF tune walks.
sigma <= 10 umho/cm, pH ~7, dee water dT stability <= 1 FSource, quote & tabletop applicability
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
Tabletop: Two directly portable specs: DI-water loop quality for any hollow-conductor coil, and tight dee-water temperature control if a next machine water-cools the dee.
-
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 & tabletop applicability
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
Tabletop: For a next machine dissipating ~1-5 kW, buy the chiller/radiator rated for ~3x that; margin is what makes long runs boring.
-
Water-cool (or oil-cool) the RF matching secondary coil: even minute thermal expansion of the copper detunes its inductance and drops the dee voltage.
Source, quote & tabletop applicability
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
Tabletop: Explains RF drift during long runs at the reference machine's power levels; cooling the tank coil stabilizes tune.
-
A water-cooled 1/4 in x 1/4 in hollow square copper conductor safely carries about 120 A; operate at ~110 A to keep a ~10% safety margin (roughly 3 A/mm^2 on the copper).
I_max ~ 120 A for 1/4 in sq hollow conductor, run at 110 ASource, quote & tabletop applicability
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
Tabletop: Direct conductor rating for the exact class of hollow-conductor coil a next machine would use in place of the reference machine's refrigeration tubing.
-
Wind coils as epoxy-potted 'double pancakes' (two-layer sub-coils with both leads exiting the same side) rather than one continuous spiral: easier to wind stiff conductor, more uniform field, and parallel water paths.
Source, quote & tabletop applicability
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
Tabletop: The reference machine's 538 turns of copper tubing could be rebuilt as ~10 potted double-pancakes per pole with a cooling manifold, easing fabrication and repair.
-
Keep coil temperature below about 142 F (61 C) in normal operation and 173 F (78 C) absolute maximum for the insulation/epoxy system.
T_normal <= 142 F, T_max <= 173 FSource, quote & tabletop applicability
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
Tabletop: Sets the thermal design point for any potted coil in a next machine; consistent with Tanabe's <30 C rise rule for long potted-coil life.
-
Pick number of turns N to match the power supply, not the physics: NI is fixed, but large-N/low-I gives cheap thin cables and dangerous high voltage, while small-N/high-I gives safe low voltage, better copper packing, and bulky expensive connections.
NI fixed; N chosen from supply V/I window (Diamond dipole example: 40 turns, 1500 A, 500 V circuit)Source, quote & tabletop applicability
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
Tabletop: The reference machine's 538 turns were set by their supply; for a next machine, pick the surplus supply first, then wind N = NI_required/I_supply.
-
Air-cooled conductors and cables are limited to a current density of about 1.5-2 A/mm^2; above that you must water-cool.
j_air <= 1.5-2 A/mm^2Source, quote & tabletop applicability
Power distribution cables... are generally limited to a current density of <1.5 to 2 Amps/mm2.
Tabletop: The go/no-go line for whether a next machine's coil design can skip water cooling: at or below ~1.5 A/mm^2 in the copper, air cooling can suffice.
-
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 & tabletop applicability
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.
Tabletop: For a home machine where power cost matters and coils are hand-wound, the ~4 A/mm^2 end of the range is the better choice; the reference machine's tubing coil runs even lower.
-
Compute coil water pressure drop from P = 0.433*f*(L/d)*(v^2/2g); use f = 64/Re for laminar flow (Re<2000) and the smooth-tube turbulent solution for Re>4000 (water nu = 1.216e-5 ft^2/s at 20 C); design in the turbulent regime for good heat transfer.
P[psi] = 0.433*f*(L/d)*(v^2/2g); Re = v*d/nu; f = 64/Re (Re<2000)Source, quote & tabletop applicability
f = 64/Re for laminar flow Re < 2000. For turbulent flow (Re>4000), the friction factor is gotten by solving a transcendental equation.
Tabletop: The complete hydraulic sizing recipe for any hollow-conductor or tubing-wound coil at the reference machine's scale.
-
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]; target <10 C, max 30 CSource, quote & tabletop applicability
Desirable temperature rise... < 10 deg. C. Maximum allowable temperature rise (assuming 20 deg. C. input water) < 30 deg. C for long potted coil life.
Tabletop: One-line flow-rate calculator: a 1 kW coil on a next machine needs ~0.4 gpm for a 10 C rise.
-
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 & tabletop applicability
For water velocities > 15 fps, flow vibration will be present resulting in long term erosion of water cooling passage.
Tabletop: Hard upper bound when the builder sizes pump and passage diameter for a next machine's hollow-conductor coil.
-
Pressure drop scales as 1/Nw^3 with the number of parallel water circuits: doubling the circuits cuts required pressure by a factor of 8 - subdivide the coil rather than buy a bigger pump.
P ~ 1/Nw^3Source, quote & tabletop applicability
Pressure drop can be decreased by a factor of eight if the number of water circuits are doubled.
Tabletop: Argues for manifolded pancake sub-coils on a next machine instead of one long series water path through 538 turns.
-
Pressure drop scales roughly as 1/d^5 with cooling-hole diameter; a slightly larger hole slashes pump requirements, and an undersized (out-of-tolerance) hole blows the hydraulic budget.
P ~ 1/d^5Source, quote & tabletop applicability
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.
Tabletop: When choosing hollow conductor for a next machine, err to the larger bore; also a reason to flow-test each pancake before potting.
-
Wind each water circuit from one continuous length of conductor (no splices buried in potting), wind in a chip-free clean area, and ball-test conductor before winding by blowing a ball <= 80% of the hole diameter through the passage with high-pressure air.
ball diameter <= 0.8 * cooling-hole diameterSource, quote & tabletop applicability
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.
Tabletop: 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.
-
Impulse-test coils for intermittent turn-to-turn shorts before installing on the core (start ~10 V/turn, raise toward 200 V/turn or 2 kV max); a healthy coil's ringdown waveform only scales in amplitude, while frequency/damping changes or 'hash' indicate a short. The test does not work once the coil is on iron.
impulse: 10 V/turn up to 200 V/turn or 2 kV; hipot: 2x operating voltage + 1 kV, leakage <= 2 mA/kVSource, quote & tabletop applicability
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.
Tabletop: A signal generator, capacitor and scope let the builder certify the next machine's coils before they are trapped under the yoke; also hipot potted coils at 2x operating voltage + 1 kV with < 2 mA/kV leakage.
-
Measure actual coil water flow at the real supply pressure rather than trusting handbook calculations - many tight-radius turns add flow impedance the formulas miss - and record ambient temperature since viscosity changes flow substantially.
Source, quote & tabletop applicability
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.
Tabletop: The reference machine's 538-turn tubing coil is exactly the many-tight-turns case; a bucket-and-stopwatch flow test at operating pressure is the real spec, not the straight-pipe pressure-drop formula.
-
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 & tabletop applicability
Water hoses should be at least one meter long and use nonconducting material to prevent current leakage from the magnet.
Tabletop: The reference machine's water-cooled copper-tubing coil sits at supply potential; a meter of plastic hose per lead and interlock-on-return are exactly the cheap practices that prevent shocks and detect a blocked circuit at home scale.
-
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 & tabletop applicability
The normal set-point of Klixons is about 89 C... One thermal interlock is installed on each water circuit.
Tabletop: A $5 thermal snap-switch soldered to the coil exit tube, in series with the magnet supply enable, is the single best protection against cooking the next machine's winding on a lost-water event.
-
Insulate coils to scale: inter-turn insulation 0.3-1.0 mm, ground insulation 0.5-3.0 mm depending on voltage; air-cooled wire varnish 0.02-0.1 mm or half-lapped Kapton 0.1-0.2 mm, giving filling factors 0.63 (round wire) to 0.8 (rectangular).
inter-turn 0.3-1.0 mm; ground 0.5-3.0 mm; varnish 0.02-0.1 mm; Kapton 0.1-0.2 mm; fill 0.63-0.8Source, quote & tabletop applicability
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.
Tabletop: Sets realistic packing-factor expectations for a hand-wound 538-turn coil and how much window the insulation eats.
-
Wind hollow conductor with a bending radius at least 4x the conductor width; at 3x width, keystoning grows the conductor dimension by 3.6% per bend and accumulates over many turns until the coil no longer fits the yoke window.
R = 3A -> dA/A = 3.6%; use R >= 4A to ignore keystoningSource, quote & tabletop applicability
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.
Tabletop: Directly applicable to bending copper tubing for a 538-turn homemade coil: tight bends also pinch the cooling bore and risk insulation damage.
-
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); c:b between 1:1 and 1:2; fc = 0.6-0.8Source, quote & tabletop applicability
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.
Tabletop: Turns the amp-turn number into an actual coil window size before you buy tubing or start winding.
-
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 & tabletop applicability
This implies that for a given flow, the pressure drop is reduced by a factor of eight by doubling the number of cooling circuits.
Tabletop: Explains why splitting a big coil into 2 or 4 hydraulic circuits lets a modest garage chiller pump do the job.
-
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 & tabletop applicability
Water resistivity higher than 0.1x10^6 Ohm m; pH-value between 6 and 6.5; dissolved oxygen below 0.1 ppm
Tabletop: If a next machine uses water-cooled coils at high voltage, tap water will leak current and corrode; a small DI cartridge loop is the fix.
-
Limit convectively (air) cooled conductors and busses to j <= 1.5 A/mm^2; anything above that needs water cooling.
j_air <= 1.5 A/mm^2Source, quote & tabletop applicability
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
Tabletop: The reference machine's copper-tubing winding at 538 turns: if any leg of the circuit (bus, jumper, lead) runs above ~1.5 A/mm^2 without water flow it will run hot; size leads accordingly.
-
Use the canonical current density j = 10 A/mm^2 for water-cooled magnet coils, a coil packing fraction of ~0.5 for small conductors, and average turn length ~3x the magnet core length for first-pass coil sizing.
j = 10 A/mm^2 (water-cooled); f ~ 0.5; l_ave ~ 3*L_magSource, quote & tabletop applicability
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.
Tabletop: Lets the builder size a next machine's coil cross-section on one sheet of paper: gross coil area ~ NI/(j*f) = NI/5 in mm^2 for water-cooled copper.
-
Design coil water circuits for fully turbulent flow (Re >= 4000) 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 (<= 15 C if field stability matters).
Re >= 4000; v <= 4 m/s; dT <= 30 C (15 C for stability)Source, quote & tabletop applicability
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
Tabletop: 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.
-
Estimate the coil power-weight tradeoff with kW x tons = 0.118 x (mega-ampere-turns)^2 x (mean turn length in inches) for copper.
kW x tons(Cu) = 0.118 x (MA-turns)^2 x (in. mean turn length)Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Directly applicable guidance for a next machine's coil geometry.
-
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 & tabletop applicability
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
Tabletop: Directly applicable thermal sizing rule for a next machine's magnet coils.
-
Favor large conductor cross-section and high current over many turns at high voltage; this simplifies both insulation and winding.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable when choosing wire gauge and supply for a next machine's coils.
-
Interleaving thin water-cooled copper cooling plates between pancake windings plus a circulation fan raises the allowable steady coil current density to about 1300 A/in^2.
J ~ 1300 A/in^2 (2.0 A/mm^2) with interleaved water-cooled plates + fanSource, quote & tabletop applicability
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
Tabletop: Directly applicable cheap upgrade: 1/16-inch copper donut plates with soldered edge tubing between pancakes nearly doubles allowable steady excitation.
-
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 & tabletop applicability
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
Tabletop: Directly applicable cautionary datum: quote coil ratings as (current, time-to-overheat) pairs, not just maximum field.
-
Never open the magnet coil circuit at high current without surge protection (thyrite resistor or electrolytic dump tank) across the coil.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable; a next machine with tens of henries of coil inductance needs a freewheel diode/varistor dump path or it will arc its switchgear.
-
Size the Dee tank circuit from the Dee capacitance: ~76 pF of Dee against a 0.87 uH secondary gives resonance up to 19.5 MHz (411 keV protons at 1.28 T), with the coils made of 1/4 inch copper tubing wound coaxially (6 cm primary outside a 4 cm secondary) and the primary tapped to set coupling.
C_dee ~ 76 pF; L ~ 0.87 uH -> f = 19.5 MHz; 1/4 in copper tubing; 6 cm dia primary over 4 cm dia secondary; 3-turn primary tappedSource, quote & tabletop applicability
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
Tabletop: Concrete LC numbers for a next machine's tank at the same scale; the swappable-primary approach lets you retune coupling without rebuilding the tank.
-
Watch coil insulation temperature: expected insulation life roughly halves per ~8 C, so alarm at a fixed winding temperature (ORNL alarmed at 70-80 C, 130 C absolute max) and remember coils take 1-3 hours to reach thermal equilibrium.
life ~ halves per ~8-10 C; alarm 70-80 C; t_equilibrium ~ 1-3 hSource, quote & tabletop applicability
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.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 33
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Directly applicable to the homemade dee-tank coil, which sees circulating RF current far above the dee's DC feed current.
-
Never nickel-plate an RF conductor: 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.
ferromagnetic plating: delta shrinks with permeability; Ni (mu~500) delta = 0.00025 in at 1 MHz vs Cu 0.0025 inSource, quote & tabletop applicability
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
Tabletop: Reject nickel-plated hardware (and nickel underlays beneath chrome or silver) anywhere RF current flows in the resonator, coil, or ground-return path.
-
Specify electrical-grade copper for RF parts: common phosphorus-deoxidized copper tube (0.015-0.08% P) has only 60-90% IACS conductivity versus 101.6% for electrical grade.
P-deox Cu tube: 60-90% IACS; electrical-grade Cu: 101.6% IACSSource, quote & tabletop applicability
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
Tabletop: Buy the tank-coil tubing as electrolytic/electrical-grade (C10100/C11000) copper, not generic plumbing tube, for up to ~20% lower RF resistance.
-
Practical single-layer air-core coils top out near true Q of 800; chasing Q much above 1000 forces abnormal dimensions, wire sizes, or turn counts.
practical Q_true <= ~800; Q > ~1000 impracticalSource, quote & tabletop applicability
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
Tabletop: Budget the resonant step-up assuming coil Q of a few hundred (loaded lower still), not textbook thousands, when sizing the amplifier for 5-13 kV dees.
-
Expect a Q meter to read below true coil Q, because 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 & tabletop applicability
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
Tabletop: When characterizing the dee resonator with a VNA or Q meter, treat the reading as a lower bound and keep leads/fixture capacitance minimal.
-
Q increases with coil diameter and with frequency, 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 & tabletop applicability
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
Tabletop: At 9 MHz a 3-4 inch diameter tank coil can reach Q well over 1000, directly multiplying dee voltage per watt of drive.
-
Wind coils with conductor diameter between 0.45 and 0.70 times the center-to-center turn spacing; commercial stock coils often violate this and lose Q.
0.45*S <= wire_dia <= 0.70*S (S = center-to-center turn spacing)Source, quote & tabletop applicability
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
Tabletop: For a 9 MHz matching/tank inductor, space the turns so the wire fills 45-70% of the pitch; close-winding bare tubing throws away Q to proximity effect.
-
Maximum Q occurs at a coil length-to-diameter ratio of 0.35-0.45, falling rapidly below that and slowly above; use L/d of at least 0.5 as a practical design margin.
Q_max at L/d = 0.35-0.45; design L/d >= 0.5; low L/d = high Q, high L/d = low QSource, quote & tabletop applicability
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
Tabletop: Make the resonator coil short and fat (roughly half as long as its diameter), not the long skinny solenoid that fits most easily in a corner.
-
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 & tabletop applicability
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
Tabletop: A 2-3 turn link or coupling loop at 9 MHz is outside the formulas; measure it rather than calculate it.
-
Estimate dee capacitance by summing three parallel-plate sections (top, bottom, edge) of the dee-to-chamber geometry; on the Rutgers 12-inch this gave 77.5 pF calculated vs 78.1 pF measured on an L-C meter.
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 & tabletop applicability
Measurement of the capacitance with an L-C meter yields a value of 78.1pF. Nice agreement seen!
Tabletop: 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.
-
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 & tabletop applicability
the trend of DEE voltage to follow the square root law of the input RF power is accurate over all measured power ranges
Tabletop: This is the sizing equation for the reference machine's LDMOS upgrade: doubling dee voltage costs 4x power, so going from 1.3 kV to 5-13 kV needs a 15-100x power increase unless L/C or Rs improves.
-
Budget the tank's effective series resistance at roughly 10-16x the coil-only handbook estimate: the Rutgers coil alone computed 50 mOhm (1.3 mOhm/inch for 1/4-inch Cu tube, 38 inches), but the whole system measured 800 mOhm because of the stainless chamber return, stainless Conflat dee-stem support, and feedthroughs.
Rs_system ~ 10-16 x Rs_coil; Rutgers: 0.05 ohm coil estimate vs 0.8 ohm measured systemSource, quote & tabletop applicability
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.
Tabletop: When predicting a next machine's dee voltage, don't use the coil resistance alone; the stainless chamber and stem return path dominates losses, so use copper return paths where possible and expect ~1 ohm scale Rs.
-
Direct HV probes fail above ~200 W forward power (the P6015 departed from the sqrt-P trend, acting like a resistive breakdown); calibrate a capacitive chamber pickup against the direct probe at low power and extrapolate linearly for high-power dee voltage measurement.
Rutgers: Dee Vp-p = 3710 x pickup Vp-p (R^2 = 0.994), valid to at least 1300 WSource, quote & tabletop applicability
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
Tabletop: Exactly the measurement chain the builder needs for the LDMOS upgrade: calibrate their pickup at 5-50 W against a scope probe, then trust the pickup alone at 100-500 W.
-
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 & tabletop applicability
the P6015 probe introduced 3.0pF of capacitance; the tank circuit was indeed reduced in frequency corresponding to 3 pF
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: A bench L-C meter trick the builder can use to characterize their coupling loop; M of tens of nH is the expected scale for a matched half-turn loop.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Expect an unloaded Q of roughly 900-1000 for a copper-refrigeration-tube tank coil at ~15 MHz (Q0 = wL/Rs = 920-1036 on the Rutgers machine); a measured loaded Q of ~460 at match confirms critical coupling.
Q0 = omega*L/Rs = (9.42e7)(1.1e-6)/0.107 ~ 968Source, quote & tabletop applicability
From Fig.12 we determine Qmeasured at a distance of 11mm to be 460. This implies a Qo of 920.
Tabletop: A benchmark for the reference machine's ~9 MHz tank: if their measured Q0 is far below ~900, there is excess loss (bad joints, steel in the return path) worth hunting down.
-
Any coupling geometry that presents (50+j0) ohms at resonance yields the same peak dee voltage for a given forward power - different loop-coil distances and tap settings are equivalent once matched, so optimize for mechanical convenience.
Source, quote & tabletop applicability
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.
Tabletop: The builder need not agonize over loop position vs tap point: any combination that nulls reflected power delivers identical dee voltage, so pick the mechanically stable one.
-
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 & tabletop applicability
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.
Tabletop: For a next machine, shrinking dee-to-liner capacitance (larger dee-to-lid spacing) and using a bigger low-loss coil buys dee voltage for free before spending on amplifier watts.
-
On a 12-inch-class machine, ~1000 W forward power produces ~15 kV p-p dee voltage (Rs=0.8 ohm, L=1.1 uH, C=78 pF); the chamber tolerated 2000 W but the tank, housing and stem run very warm.
1000 W -> ~15 kVp-p; 2000 W withstood with significant heatingSource, quote & tabletop applicability
It is not necessary to operate at 2000 watts, as shown above 1000 watts produces a peak-to-peak DEE voltage of approximately 15kV.
Tabletop: Scales the reference machine's plan: with a similar tank, a 500 W LDMOS amp should land near 10 kVp-p - comfortably in their 5-13 kV target - and thermal management of stem and coil becomes the real issue.
-
Protect the beam-current electrometer from RF pickup with a large series inductance (RF choke) in the collector lead instead of a thick shield around the collector tip.
Source, quote & tabletop applicability
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
Tabletop: Lets the builder use an unshielded collector at nA levels: a ~100 uH-mH choke at the feedthrough kills 9 MHz pickup without blocking DC beam current.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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/He++ f = 0.76*BSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Make the source mount adjustable by a few mm in both directions and tune position for beam, not for geometric center.
-
Electric gap focusing helps only in the first few turns and only for ions crossing while the RF field is DECREASING; ions bunch toward peak-voltage phase automatically, and the total usable phase migration for an extracted beam is one half-cycle (0 to -pi/2 and back).
phase focusing quadrant: field decreasing during transit; total phase excursion ~pi radians; internal targets tolerate up to ~3*pi/2Source, quote & tabletop applicability
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
Tabletop: 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.
-
Raising dee voltage is the universal cure for marginal resonance (fewer turns, more phase-slip budget) but trades against breakdown and RF power; 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 & tabletop applicability
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
Tabletop: At 1.3 kV and 160 keV the reference machine's ions make ~60+ turns; doubling dee voltage halves turns and dramatically relaxes both field-uniformity and vacuum (scattering) requirements.
-
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; larger clearance is the only durable fix beyond polishing.
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 & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 175
Tabletop: At 1.3 kV the builder has enormous margin; for a next machine at several kV, ~50 kV/in of clearance in vacuum with rounded edges is a comfortable design gradient.
-
Water-cool dees aggressively: cooling tubes soldered inside on 2-3 in spacing prevent local heating and warping under RF power; taper the dee height toward the periphery to follow the shrinking beam envelope and cut lid capacitance and RF power.
cooling-tube pitch 2-3 in; ~10 kW dissipated per dee+line at MIT scaleSource, quote & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 175
Tabletop: At tens of watts the builder needs no water, but the warping lesson stands: dee thermal drift detunes the resonator, so keep dee structures stiff and thermally anchored.
-
Match the exposed ionization-column length to the dee aperture (5/8 in for a 1.6-in aperture, 1-3/8 in for 4-in dees); too long a column loads the RF circuit with off-focus ions and drags down dee voltage.
optimum column length ~ 0.35-0.4 x internal dee apertureSource, quote & tabletop applicability
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
Tabletop: Hood or collimate the reference machine's source so only ~1/3 of the dee aperture height of plasma column is exposed; more column means RF load, not more beam.
-
Feed the dees through quarter-wave resonant lines (dee on inner-conductor end), drive push-pull, and suppress the push-push mode; keep the oscillator physically simple with the shortest possible leads - that is the only general anti-parasitic rule.
f_pushpull = 1/(2*pi*sqrt(L(C+2C'))); push-push mode has higher Q and no dee-to-dee voltageSource, quote & tabletop applicability
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
Tabletop: If the next machine goes two-dee push-pull, watch for the push-push mode (no accelerating voltage, oscillator happily locked); a single-dee-plus-dummy design sidesteps it.
-
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 & tabletop applicability
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
Tabletop: The reference machine's ~1.3 kV dee sits right in classic multipactor territory; surface conditioning, low pressure, and the ability to snap the drive up fast are the standard escapes.
-
Fit a remotely adjustable trimmer capacitor (movable grounded plate facing a dee edge, ~1 percent frequency range, with excellent RF contact to the wall) to balance the two dee-circuit frequencies and dee voltages under power.
tuning range ~1% in frequencySource, quote & tabletop applicability
Such a variable capacitance can be provided by a movable plate on the side wall of the chamber facing one edge of the D ... a range of motion sufficient to tune over about 1 per cent in frequency.
Livingston & Blewett, Particle Accelerators (1962) — p. 188
Tabletop: 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.
-
Expect spark conditioning of a freshly opened chamber: assemble clean (no fingerprints, dust, steel wool, or coarse abrasives), round and polish all high-field contours, then let sparking rain until it subsides - no amount of polish eliminates conditioning.
Source, quote & tabletop applicability
dust should be controlled and all grease removed (even fingerprints), and under no circumstances should steel wool or coarse abrasives be used in cleaning.
Livingston & Blewett, Particle Accelerators (1962) — p. 189
Tabletop: After every chamber opening, budget an hour of gradually raised dee voltage for conditioning before expecting stable beam.
-
Prefer a self-excited oscillator closely coupled to the high-Q dee circuit (frequency follows dee warping and loading automatically); the grounded-anode push-pull variant with crossed neutralizing capacitors is the simplest and most parasitic-free of the classic circuits.
Illinois 42-in: two '880' tubes, ~60 kW total input; grounded-anode, cross-neutralized, low-Q grid coilSource, quote & tabletop applicability
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
Tabletop: The same logic favors the reference machine's self-excited or PLL-followed drive: let the dee resonator define frequency so mechanical drift retunes the drive instead of killing the beam.
-
Seal flanges with a gasket in a machined groove, gasket ~50 percent thicker than groove depth; 1/4-in gaskets suffice for even the largest seals; use neoprene (low vapor pressure, grease-tolerant) and 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 & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 199-201
Tabletop: Directly usable rules for the reference machine's lid and port seals; the copper-foil RF bridge over elastomer joints prevents mysterious Q loss and local heating.
-
Set the RF frequency slightly below the central-field cyclotron frequency but above the edge-field frequency, so accumulated phase error first grows negative then recovers - this minimizes the dee voltage needed to reach full radius.
f_edge < f_rf < f_centerSource, quote & tabletop applicability
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
Tabletop: A concrete tuning rule for the builder: don't tune RF to the central field value; split the difference toward the outer-radius field.
-
If RF is tuned exactly to the central frequency of a radially decreasing field, ions slip to 90 degrees of phase in only about a dozen turns and stop gaining energy - which is why exact-center tuning demands very high dee voltage.
~12 turns to 90 deg phase slip with f_rf = f_centerSource, quote & tabletop applicability
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
Tabletop: Quantifies how little phase budget a mistuned tabletop machine has; explains failed runs where beam dies at small radius.
-
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 & tabletop applicability
it has one dee-shaped copper electrode, and the grounded vacuum chamber functions as the other electrode
Tabletop: The reference machine already does this; it remains the right choice for a next machine unless push-pull two-dee RF is needed for higher energy gain per turn.
-
Size the dees to about 0.9 of the pole radius with a small dee-to-dee gap: Iowa State's thin sheet-copper dees were 22.5 cm diameter and 2.4 cm high, separated by a 1.5 cm gap, water-cooled through the supporting stems.
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 & tabletop applicability
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
Tabletop: A directly copyable dee geometry for an 8-10 inch pole; note the dees must be water cooled once RF power reaches ~kW.
-
Budget extraction realistically: even a mature machine extracted only ~30% of the circulating beam, and overall RF-to-beam power efficiency was 10-15%.
extraction ~30% of internal beam; beam power / RF DC input ~ 10-15%Source, quote & tabletop applicability
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
Tabletop: Sets expectations if a next machine attempts a deflector: losing two-thirds of the beam at the septum is normal, not failure.
-
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 & tabletop applicability
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
Tabletop: Direct rule for the reference machine's source-to-puller spacing and any dee-to-ground clearance: a few-kV dee needs sub-mm minimum, but leave margin because sputtered metal films spoil the 'clean surface' assumption fast.
-
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 & tabletop applicability
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
Tabletop: When insulating the reference machine's extraction or dee leads with PTFE sheet or heat-shrink, use the bulk (70 kV/mm-class) figure with a 5-10x safety factor, not the datasheet film value.
-
For automated matching prefer an L-network over T or Pi: it has only one L-C combination per load (simplest search algorithm), and two complementary L configurations selected by an RF switch cover the whole Smith chart.
2 L-network topologies (shunt-C input vs shunt-C output) + RF switch = full impedance coverageSource, quote & tabletop applicability
Compared to T or Pi networks, the L network uses only one combination of inductance and capacitance. This simplifies the microcontroller tuning algorithm.
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 11
Tabletop: If the builder automates their dee match at 9 MHz, a stepper-driven L-network is the simplest topology whose tuning can't get lost in redundant solutions.
-
Sample line power through a ~30 dB directional coupler so a +17 dBm-max AD8307 log detector can read up to 200 W; 30 dB coupling keeps main-line loss negligible.
P_coupled = P_line - 30 dB; 200 W (53 dBm) -> 23 dBm approx detector maxSource, quote & tabletop applicability
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
Tabletop: Exactly sized for the reference machine's 100-500 W upgrade: a homebrew 30 dB coupler plus AD8307 boards gives continuous forward/reflected monitoring across their whole power range.
-
Build the HF coupler the Kaune way: ferrite toroids (FT-82-67) wound with AWG 26 wire slipped over 2-inch sections of RG-8, so the coax shield passing through the toroid blocks capacitive coupling and only magnetic coupling samples the line; achieves 28-35 dB directivity across 3.5-30 MHz.
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 & tabletop applicability
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
Tabletop: A ~$5 coupler build that brackets the reference machine's 9 MHz band; the shield-through-toroid trick is the detail that makes homebrew directivity respectable.
-
Coupler directivity sets the floor of SWR measurement: with 28 dB directivity a perfectly matched load still reads SWR 1.08, with 35 dB it reads 1.03; commercial HF couplers span 15-44 dB.
SWR_floor = 1.08 at 28 dB directivity; 1.03 at 35 dBSource, quote & tabletop applicability
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
Tabletop: Tells the builder not to chase SWR below ~1.1 on a homebrew bridge - that residual is the instrument, not the match.
-
Calibrate homebrew power sensors in two ranges: against a VNA/signal generator at low power and against a Bird 43 thruline wattmeter from 30 to 100 W, building an ADC-to-dBm lookup table (AD8307 slope 25 mV/dB).
AD8307: 0.025 V/dB slope, ~2.0 V intercept; two-range calibration 0-30 W and 30-100 WSource, quote & tabletop applicability
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
Tabletop: The builder already lives in this instrument ecosystem; a Bird 43 (or borrowed one) transfers absolute power calibration to permanently installed cheap sensors.
-
A workable auto-tune algorithm: alternately step the capacitor then the inductor toward the SWR minimum, repeating up to 3 times, stopping at SWR < 1.5:1 (4% reflected power) - the standard 'acceptable match' threshold for solid-state amplifiers.
SWR 1.5:1 <=> 4% reflected; iterate C then L, <= 3 passes; matched initial SWRs up to 26:1Source, quote & tabletop applicability
actuates stepper motors to alternately adjust a variable capacitor and a variable inductor to reduce VSWR to less than 1.5:1
Blodgett, 3.5 to 30 MHz Automatic Antenna Impedance Matching System (2012) — p. 6-8, 40
Tabletop: SWR 1.5:1 is the protection threshold for the reference machine's LDMOS amp too; coordinate-descent on C then L converges fine for the single-resonance dee load.
-
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 & tabletop applicability
fo = qBo/2pi mi = (1.52x10^7) Bo(tesla)/A
Humphries, Principles of Charged Particle Acceleration (1986) — p. 524
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: At sub-MeV this limit is distant (10 kV dee -> ~3 MeV proton ceiling), but the same physics governs field-flatness tolerance: fewer turns forgives more field error.
-
Low-energy protons orbit at 15.23 MHz per tesla (f = qB/2*pi*m); scale RF frequency linearly with field for any classical proton cyclotron.
f(MHz) = 15.23 * B(T) for protonsSource, quote & tabletop applicability
Low energy proton in 1 T field: 15.23 MHz
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 29
Tabletop: 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.
-
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*(T1/T); e.g. 250 MeV at 17 keV/turn -> N~15,000, dr/dN ~ 20 umSource, quote & tabletop applicability
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
Tabletop: For the builder: 1 MeV at 2 kV/gap (2 gaps) is ~250 turns with final-orbit spacing ~0.2 mm at r=12 cm - explaining why higher dee voltage directly eases both extraction and vacuum requirements.
-
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 & tabletop applicability
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
Tabletop: Reassurance and ceiling in one number: at 1 MeV gamma-1 = 0.001, ~0.4 deg/turn - a next machine is nowhere near the relativistic limit, and the classical (non-AVF) architecture is fine to several MeV.
-
A single real dee working against its image in a grounded plate is a proven small-machine RF architecture: 50-ohm amp, wattmeter, matching transformer, and a hand-adjustable inductor to pull the LC resonance onto the cyclotron frequency.
f = 1/(2*pi*sqrt(LC)), C fixed by dee geometry, L adjusted (deformable coil) to tuneSource, quote & tabletop applicability
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
Tabletop: This is the reference machine's exact topology, validated on a comparable machine; the deformable-inductor trim is a simple tuning mechanism for a next machine.
-
Expect an unloaded resonator Q of order 1000+ from a well-made small dee circuit (this machine measured Q = 1600 unloaded), and remember high Q means a narrow resonance requiring precise, stable tuning.
Q = f0/delta-f = 2*pi*E_stored/E_lost per cycle; measured Q_unloaded = 1600Source, quote & tabletop applicability
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
Tabletop: Direct benchmark for the reference machine's resonator: if measured Q is far below ~1000, hunt for lossy joints; and thermal drift of a Q~1600 circuit needs active or frequent retuning at 9 MHz.
-
Know which breakdown regime you're in: below ~1e-5 torr the physics is vacuum breakdown (field emission/particulates), above ~1e-4 torr it is gas breakdown (Paschen); the decade between is a gray zone.
vacuum regime < 1e-5 torr; gas regime > 1e-4 torrSource, quote & tabletop applicability
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
Tabletop: Cyclotrons run 1e-5 to 1e-4 torr with gas feed - squarely in the gray zone - so the reference machine's spark limit will move with operating pressure, and tests at base pressure overstate what they can hold with gas flowing.
-
Condition ('bake out') the tank with RF applied in short bursts at reduced power, never leaving RF on through a glow discharge, gradually raising power until vacuum stays below 1e-4 mm with ~2 kV steady RF.
condition until P < 1e-4 torr with RF steady at ~2 kVSource, quote & tabletop applicability
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
Tabletop: Directly applicable startup ritual at the reference machine's 1.3 kV dee level; persistent glow during conditioning signals organic contamination (grease, oil, rubber) in the tank.
-
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 & tabletop applicability
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
Tabletop: Exactly the reference machine's architecture; the dummy-dee edge is a proven low-cost next-machine upgrade for a cleaner accelerating gap.
-
For the RF drive, a grounded-grid Hartley self-excited oscillator confines RF currents to intended paths better than most circuits; include the dee-to-ground capacitance as the major tank-circuit capacitance and trim frequency with a small parallel capacitor.
C_tank ~ C_dee-ground + C_trim; step-up by tapping plate down the coilSource, quote & tabletop applicability
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
Tabletop: 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.
-
Provide short, broad RF ground paths: mount the tube through a large hole in a copper ground sheet at grid-terminal level and extend that sheet to the tank wall; keep the tube close to the tank but out of the magnetic field.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable to the reference machine's amplifier: wide copper sheet/strap grounds and a short feed run, with magnetically sensitive parts (and LDMOS heat sinks) out of the fringe field.
-
Choke and bypass every circuit that connects to a tank element so RF cannot reach meters and supply lines, and make magnet, source, and RF controls instantly adjustable and kill-switchable.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable; the reference machine's beam-current, bias, and gauge lines all need feedthrough RC/choke filtering at 9 MHz.
-
Treat all cyclotron supply voltages as lethal: fit interlock switches on power-supply covers, keep grounding hooks by the machine, and enclose the oscillator in a grounded copper screen box.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable home-lab safety baseline for a next machine.
-
Thin chamber lids over a wide flat span bow inward under vacuum, changing dee capacitance (detuning the RF) and reducing flashover voltage - tack-weld internal support posts under the lids.
example: 3/16 in lids over ~2 ft span required postsSource, quote & tabletop applicability
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
Tabletop: Directly relevant to any thin-lid chamber on a next machine squeezed into a small magnet gap: plan support posts (clear of the beam spiral) from the start.
-
A single dee plus grounded dummy dee doubles the required dee voltage compared to two dees, but halves the RF feedthrough/plumbing complexity - the right trade at amateur scale.
1 dee: V_required x2, feedthroughs /2Source, quote & tabletop applicability
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
Tabletop: Confirms the single-dee choice for a next machine unless dee voltage becomes the binding constraint.
-
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; 56 pF/ft x 20 ft at 30 kV = 0.4 J; 5 ft = 0.1 JSource, quote & tabletop applicability
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
Tabletop: For any HV feed on a next machine (deflector, source bias): keep cable runs minimal - stored cable energy, not the supply, does the arc damage.
-
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 & tabletop applicability
We've encased the resistor in a grounded shield, and the coax shields go through 68 Ohm, 2 watt resistors
Tabletop: A ready-made HV-distribution recipe for the reference machine's deflector or PIG source bias; note even this shielding didn't stop arcs until the cable-energy fix - resistors limit damage, they don't prevent flashover.
-
A complete tabletop cyclotron RF chain can be assembled from commercial units - function generator (HP 33120A) -> RF power amp (ENI 155LCRH) -> ham autotuner (LDG AT-200PC) -> Bird 43A wattmeter -> dee - with the tuned circuit at fr = 1/(2*pi*sqrt(L2*C)) ignoring mutual inductance.
fr = 1/(2*pi*sqrt(L2*C))Source, quote & tabletop applicability
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
Tabletop: This is essentially the reference machine's current architecture, validated: a ham antenna tuner really can match a dee, at the cost of low Q and ~1-2 kV ceilings.
-
Through an autotuner chain, tens of watts yields kV-class dee voltage: Houghton ran 1700 Vpp from 26 W and 800 Vpp from 10 W at ~3.5 MHz - roughly consistent with sqrt(P) scaling.
26 W -> 1700 Vpp; 10 W -> 800 Vpp (ratio 2.1 vs sqrt(2.6)=1.6)Source, quote & tabletop applicability
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
Tabletop: Benchmarks the reference machine's setup (1.3 kV from 5-50 W is right on this curve) and warns that the autotuner path plateaus in the low-kV range.
-
Low dee voltage caps the usable field/energy through orbit count: at 800 Vpp, no beam peaks appeared for fields above ~0.5 T because reaching full radius required ~44 orbits - too many turns for the beam to survive gas scattering and defocusing.
N_orbits = T_final/(e*Vpp); 35 keV / 800 eV ~ 44 orbits was the practical survival limitSource, quote & tabletop applicability
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
Tabletop: 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.
-
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*L/R_AC = U/P; Q_loaded = Q0/2 at optimumSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
Record Input Power 2kW: 8.4 kVpeak
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 19
Tabletop: Anchors the power budget: even a well-built 12-inch tank needs kW-class RF for ~10 kV dee voltage, so the reference machine's 500 W LDMOS should target ~4-8 kV peak.
-
Validate the dee-voltage calibration with beam: calculation said first ions squeak past the source structure at 165 W, and in practice beam current dropped abruptly to zero at 170 W as RF power was ramped down from 300 W.
predicted threshold 165 W vs measured beam cutoff 170 W at 14.864 MHzSource, quote & tabletop applicability
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
Tabletop: A free end-to-end check for the builder: the RF power at which beam vanishes measures the true dee voltage through pure geometry, independent of every probe.
-
Thermal drift of the dee, chamber and tank coil during operation shifts the resonant frequency enough to require persistent retuning; automate it by phase-comparing the drive RF with the dee pickup and driving a motorized trim capacitor in parallel with the dee from the DC error signal.
phase(drive) - phase(pickup) -> DC error -> motor-driven parallel trim capacitorSource, quote & tabletop applicability
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
Tabletop: At 100-500 W the next machine will drift off resonance within minutes of turn-on; this phase-lock autotuner (or the equivalent PLL driving their signal source) is the fix.
-
Infer dee voltage from beam physics: the radius of the first half revolution satisfies E(r) = qB^2 r^2/2m = (1/2) e Vp-p, giving a probe-independent 'beam inferred dee voltage' that Rutgers plotted alongside pickup and rectifier data.
E(r) = q*B^2*r^2/(2m) = 0.5*e*Vp-p in first half revolutionSource, quote & tabletop applicability
Beam Inferred DEE Voltage
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 33
Tabletop: The builder can cross-check their 1.3 kV estimate by measuring where the first half-turn lands - the beam itself is the most honest voltmeter.
-
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 -- permanently raises the threshold, so condition new electrodes gradually and expect to redo it after every air exposure.
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 & tabletop applicability
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
Tabletop: Bring the reference machine's dee and extraction voltages up over tens of minutes on first pump-down, watching for micro-discharge pulses; a gap that arcs at 15 kV cold will often hold 20+ kV after patient conditioning.
-
At an insulator-cathode junction, terminate the insulator at ~31.5 degrees to the cathode so the surface charges negatively or not at all; screening the cathode end (or adding a semiconducting layer) raises flashover voltage ~2.5x, and roughening the insulator surface near the cathode adds another ~40%.
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 & tabletop applicability
They found that at a critical angle of 31.5 deg, the surface charge was zero... by screening the section of the insulation surface near the cathode... the breakdown voltage was raised by a factor of approximately 2.5.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 113-114
Tabletop: Free flashover margin for the next machine's source stalk and dee-stem insulators: cone the insulator ends at ~30 degrees toward the negative electrode and recess the triple junction behind a metal skirt.
-
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 -- roughly 2-4.5 kV/mm of creepage length, 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 & tabletop applicability
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
Tabletop: Budget ~2 kV per mm of insulator surface path in vacuum (before sputter contamination); a 20-kV extraction stalk wants >=10 mm of clean creepage plus corrugations.
-
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 & tabletop applicability
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
Tabletop: The classic failure of home-built HV feedthroughs: a loose PTFE sleeve over a rod arcs in the annular air film; pot it, oil-fill it, or evacuate the annulus so Paschen cannot be satisfied.
-
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; also round the edge of any outer/shield conductor to a radius no smaller than the inner conductor's radius.
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 & tabletop applicability
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.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 117, 122-124
Tabletop: Sizes the reference machine's HV stalk directly: for a grounded 25-mm-bore chamber port, a ~9-mm center conductor minimizes field stress; and never leave a sharp-edged washer or nut on the HV end.
-
Sputtered cathode metal plates every line-of-sight insulator and eventually shorts it: shadow-shield the HV stalk from direct ion flow (coaxial shield tubes, conical shadowing insulator facing the cathode) and corrugate insulator surfaces to lengthen the surface-leakage path.
design rules: 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 & tabletop applicability
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.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 87, 105, 109
Tabletop: In the reference machine's small chamber everything sees the source; a simple washer-stack or skirt shielding the feedthrough ceramic from the chimney slit will multiply time-between-cleanings.
-
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 & tabletop applicability
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
Tabletop: Explains why the reference machine's next big win may be Dee voltage, not magnet shaping: at ~160 keV with a low Dee voltage the turn count is what kills the beam.
-
When scanning the magnet at fixed RF frequency, expect resonance current peaks not just at the fundamental field B but at B/3, B/5, etc. (odd subharmonics), for every ion species present.
peaks at B, B/3, B/5, ... for each q/m speciesSource, quote & tabletop applicability
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.
Tabletop: Essential for interpreting the reference machine's magnet scans: a peak at one-third field is a subharmonic, not a mystery species, and H2+ vs H+ vs They peaks can be disentangled this way.
-
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 & tabletop applicability
It can be seen that in general, an increase in dee voltage results in a higher beam current.
Tabletop: For a fill-gas machine like the reference machine's, dee volts are the strongest single knob on beam current; prioritize RF voltage over almost everything else.
-
Find resonance by a three-stage frequency sweep - 0.5 MHz steps over the whole band, then 0.1 MHz, then 0.01 MHz around the peak - while plotting dee-voltage gain (Vdee/Vrf); the Houghton peak showed a gain of ~80x at f0 = 3.55 MHz.
sweep steps 0.5 -> 0.1 -> 0.01 MHz; observed voltage gain ~80x at resonanceSource, quote & tabletop applicability
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
Tabletop: A simple, scope-only resonance-finding recipe the builder can use after any mechanical change to a next machine's dee or stem.
-
An autotuner-matched dee circuit runs at low Q (Houghton measured Q = 16.1 from f0/dF = 3.55/0.22 MHz; their earlier chamber was Q = 22) - orders of magnitude below a directly coupled copper tank (Q0 ~ 900), trading voltage gain for tuning convenience.
Q = omega0/delta-omega_FWHM = 3.55/0.22 = 16.1Source, quote & tabletop applicability
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.
Tabletop: Quantifies the reference machine's architecture choice: an antenna-tuner match (like their current setup) gives kV-class dee voltage; multi-kV needs a high-Q tank coil instead.
-
Expect manual and analyzer-based resonance measurements to disagree slightly (3.55 vs 3.63 MHz at Houghton) because a HV probe near the dee adds capacitance and shifts the resonant frequency.
probe proximity shifted f0 by ~0.08 MHz (~2%)Source, quote & tabletop applicability
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.
Tabletop: When the builder cross-checks NanoVNA SWR sweeps against probe measurements, a few-percent frequency disagreement is expected instrumentation loading, not a fault.
-
Calibrate the pickup probe by scanning frequency with the chamber open and a direct HV probe on the dee: Houghton found real dee voltage ~11,300x the pickup voltage at 3.55 MHz, and the factor must be re-measured every time operating frequency changes.
V_dee = 11300 x V_pickup at 3.55 MHz (linear fit)Source, quote & tabletop applicability
the real voltage was roughly 11,300 times the pickup voltage ... the probe had to be recalibrated every time the frequency was adjusted.
Tabletop: The pickup scale factor is frequency-dependent - the builder must recalibrate their pickup whenever they retune, not assume one constant.
-
A tabletop machine can make measurable beam at very low RF power once matched: at SWR 1:1 and only 15.4 W forward, Houghton accelerated protons to 9.2 keV (r = 5.95 cm) with ~1.5 pA on the Faraday cup.
15.43 W forward, SWR 1:1, 3.55 MHz -> 9.2 keV protons at 5.95 cmSource, quote & tabletop applicability
a SWR of 1:1 and forward power of 15.43 W were measured
Tabletop: Reassurance for commissioning a next machine: hunt for first beam at tens of watts with a clean match before scaling power - beam detection, not power, is the bottleneck.
-
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 & tabletop applicability
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
Tabletop: At the reference machine's sub-MeV energies relativistic slip is negligible (~0.1%), so dee voltage matters mainly through path length and gas scattering - but this rule sets the fixed-frequency ceiling for any future MeV-class ambition.
-
Use an AEI hairpin electron-microscope filament floating at about -90 V and heated with 2 A as the ion source, and short RF pickup on each filament lead to ground through a 0.001 uF capacitor.
filament bias -90 V, heater 2 A, 0.001 uF RF bypass on each leadSource, quote & tabletop applicability
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.
Tabletop: An off-the-shelf, cheap, replaceable filament choice plus the RF-bypass detail that keeps the filament supply alive next to a live Dee.
-
Expect only 10-40 W of RF drive to reach up to ~3000 V peak on the Dee against a grounded dummy Dee in a decent tank circuit.
10-40 W forward RF -> up to ~3 kV Dee amplitude; typical running 2100 VppSource, quote & tabletop applicability
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
Tabletop: Tells the builder that Dee voltage is a tank-Q problem, not a brute-force power problem: a modest amplifier plus a good resonator beats a big amplifier into a lossy one.
-
Operate at as low an RF frequency as other constraints allow, because engineering art and components are far more available at low frequency (ORNL chose <15 Mc/s).
prefer f < ~15 MHz where B and size permitSource, quote & tabletop applicability
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
Tabletop: The reference machine's 9 MHz sits in this sweet spot; for a next machine, avoid pushing frequency (i.e., field) past where cheap RF parts and simple technique still work.
-
Budget dee excitation power from P ~ 2*pi*f*C*V^2/(2Q): the 86-inch needed 96 kW of RF for 400 kV dee-to-dee with C=176 pF, f=13.5 MHz, loaded Q=3700 (unloaded 12,300).
P_dee = pi*f*C*V_dee-gnd^2/Q; C_dee=176 pF, Q_loaded=3700, Q_unloaded=12300Source, quote & tabletop applicability
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
Tabletop: Formula transfers directly: at 9 MHz, ~50 pF and Q~1000, 5 kV on the dee costs only tens of watts, telling the builder exactly how much amplifier a higher-voltage dee on a next machine needs.
-
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 & tabletop applicability
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
Tabletop: 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.
-
When beam current is pushed up, sparking is what ends the climb; treat sustained spark-free operation, not peak meter readings, as the machine's real rating.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable test discipline for a next machine's dee-voltage conditioning: rate the machine at the level it holds quietly for minutes, not the level it touches.
-
Expect overall (wall-plug RF to beam) gross efficiency in the few-percent range and rising with dee voltage and beam power; the 86-inch measured 2.6-9.3% gross and 30-44% counting all accelerated ions.
gross eff = beam kW / oscillator DC kW ~ 3-9%; improves with V_deeSource, quote & tabletop applicability
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
Tabletop: Order-of-magnitude expectation transfers: most RF power goes to resonator and ion-loading losses, so judge a next machine's RF sizing on resonator dissipation, not beam power.
-
Make every high-current RF joint a clamped, silver-plated, water-cooled surface: silver-plate the dee stems over the tuning range and clamp the shorting plane with split silver-plated rings.
Source, quote & tabletop applicability
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
Tabletop: Scaled down: any sliding or bolted joint in the reference machine's dee-stem/coil path should be a broad, clean, plated, firmly clamped contact - RF joints, not wires, set small-resonator Q.
-
Bring cooling water into RF-hot structures through insulating hose or RF-choke coils of the tubing itself; ceramic water-lead insulators failed at 200 kV and were replaced by copper-tubing chokes.
water leads: ~7 ft of 2 in rubber hose (DC bias) / copper-tube RF choke coilsSource, quote & tabletop applicability
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. 59
Tabletop: 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.
-
Build the plate/oscillator DC supply from many identical paralleled units with individual fused disconnects so one failed unit can be dropped without stopping the machine.
Source, quote & tabletop applicability
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
Tabletop: Transferable architecture: paralleled small supply modules (or PA pallets) with individual protection give a home machine graceful degradation.
-
Bias the dees a few hundred volts to several kV negative to suppress ion loading and multipactor so the self-excited oscillator starts cleanly and can be brought up at full power.
dee DC bias 0.3-5 kV negative, interlocked to RFSource, quote & tabletop applicability
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
Tabletop: Directly applicable if a next machine's RF start-up stutters or the dee glows at low voltage: insulate the dee for DC and add a few-hundred-volt negative bias through an RF choke.
-
Allow roughly 1.5 inches of vacuum clearance from dee to grounded liner per 100 kV peak RF (about 26 kV/cm), and treat that gap as precious space stolen from the magnet.
d_clearance ~ 1.5 in per 100 kV peak (~26 kV/cm RF in cyclotron vacuum)Source, quote & tabletop applicability
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.
Tabletop: Scales directly: the reference machine's 1.3 kV needs well under a millimeter electrically, so their clearances are set by beam aperture and tolerance, but a 20-50 kV dee on a next machine should keep several millimeters to grounded surfaces.
-
Energy gain per dee crossing is 2*V_dee*sin(theta/2) for dee angular width theta, so half-dees and cut-away lips directly tax energy gain (a 15-degree wedge off a dee lip cost 30% for third-harmonic particles).
dE_per_crossing = q * 2*V_0*sin(N*theta/2) (N = harmonic order)Source, quote & tabletop applicability
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
Tabletop: Directly applicable when the builder trims a next machine's dee for probe or source clearance: keep the dee close to 180 degrees or account for the sin(theta/2) energy-gain penalty.
-
High dee voltage at practical drive power is only achievable with a high-Q resonant circuit; treat the dees and stems as a quarter-wave line foreshortened by dee capacitance, tunable via C, stem length, or stem impedance.
dee system = lambda/4 line foreshortened by C_dee; tune via C, l, Z0Source, quote & tabletop applicability
The high dee voltage required in cyclotrons can be achieved for practical driving power only by using a high-Q resonant circuit.
Tabletop: 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.
-
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 & tabletop applicability
it is possible to bias the dees to prevent multipactoring, and a more complex booster oscillator circuit is required
Tabletop: Directly applicable: multipactor lives exactly in the few-hundred-volt, MHz regime of a starting tabletop dee; plan the DC-bias insulation into a next machine's dee stem from day one.
-
Mount RF power boards to a machined copper heat spreader with screws only - no solder - and use heat-sink compound only between the copper spreader and the aluminium heat sink.
Source, quote & tabletop applicability
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
Tabletop: Standard practice for any kW-class dee driver a home builder assembles from LDMOS boards.
-
Stabilize a high-gain LDMOS stage at the low-frequency end with degenerative drain-to-gate feedback of about 15 nH - literally 1.5 cm of #20 wire per side, not a wound coil - in series with the feedback resistor.
L = 15 nH = 1.5 cm of #20 AWG wire, drain-to-gate, in series with feedback resistorSource, quote & tabletop applicability
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
Tabletop: Useful if the builder builds a broadband solid-state dee driver: the devices have huge low-frequency gain and will oscillate without this.
-
Measure the actual harmonic spectrum with a spectrum analyzer through ~40 dB of attenuation before choosing any output filter: in a push-pull LDMOS deck the second harmonic is naturally suppressed but the third came out only 8-10 dB down, which 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 & tabletop applicability
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
Tabletop: A cyclotron dee tank is narrowband, but the same rule holds: measure what the PA actually emits before designing filtering or worrying about RF interference from a garage machine.
-
For solid-state PAs, prefer diplexers that dump harmonic energy into a resistor over reflective low-pass filters, because reflecting harmonic power back into the FET drains risks driving the device into oscillation.
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 & tabletop applicability
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
Tabletop: Relevant if the builder drives the dee with a broadband solid-state PA instead of a tube: protect the FETs from the highly reactive dee load.
-
Expect to move every filter cutoff upward after the first build: cutoffs and crossovers designed too close to the operating frequency produced excessive passband insertion loss and high VSWR, and 'virtually every part value changed' during tuning.
design settings used: Chebyshev, T-type, 0.005 dB passband ripple, >43 dB stopband <30 MHz, 60 dB aboveSource, quote & tabletop applicability
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
Tabletop: Schedule tuning time (this cost the author three months); the same applies to a homemade dee tank and matching network.
-
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 & tabletop applicability
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.
Buckler, Solid-State, 2-Decade, 1.25 kW Linear Amplifier — Development Notebook (2015) — p. 31-32
Tabletop: Cheap fault-tolerance rules for any homebuilt high-voltage/high-current RF deck; voltage-derating the caps matters more with the reactive load a dee presents.
-
Budget roughly 10% loss between the amplifier deck and the load: a deck measuring 1.4 kW output delivered about 1.3 kW at saturation after T/R relays, harmonic filters and directional couplers.
1.4 kW at deck -> ~1.3 kW after T/R switches + filters + couplersSource, quote & tabletop applicability
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
Tabletop: Size the RF chain for the dee power you actually need plus ~10-15%; the same relay/coupler/filter tax applies to a cyclotron dee drive.
-
Do not assume silver plating lowers RF loss: commercial bright silver deposits run 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 & tabletop applicability
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
Tabletop: Skip decorative silver plating on the dee and coil; a jobbing-shop bright-silver finish would raise, not lower, resonator loss at 9 MHz.
-
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 & tabletop applicability
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
Tabletop: For dees, stems, and tank coils at 9 MHz: bare electrical-grade copper plus thin lacquer beats commercial silver or nickel plate.
-
A lower-conductivity plating hurts most at about 1.5 skin depths thickness (resistance maximum), while very thin layers of either very high or very low conductivity over copper have negligible effect on RF resistance.
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 & tabletop applicability
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
Tabletop: A sub-micron corrosion-protection flash on copper is harmless at 9 MHz; a mid-thickness medium-conductivity coating is the worst case to avoid.
-
A thin gold flash (10 microinches) over silver is porous; at least 200 microinches of gold are needed to stop sulfide films creeping from exposed silver over the gold.
t_Au >= 200 uin (~5 um) for pore-free protection of silverSource, quote & tabletop applicability
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
Tabletop: For RF contact fingers and connectors on the resonator, distrust thin gold flash; specify thick gold or use bare copper with lacquer instead.
-
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 & tabletop applicability
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
Tabletop: Any silver-plated RF joints in the shop atmosphere (or near vacuum-pump exhaust) need protection or periodic cleaning, or kV-level circulating currents will heat them.
-
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 & tabletop applicability
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
Tabletop: Polishing dee edges and stems serves double duty at 5-13 kV: lower RF resistance and higher voltage-breakdown threshold.
-
Give the amplifier controller hardware safety monitoring of temperature, load failure, and reflected power (SWR), with ALC feedback that limits drive and prevents hot-switching of relays.
Source, quote & tabletop applicability
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
Tabletop: A directional coupler plus fast drive-cut on high reflected power is the single best defense when the cyclotron dee arcs or drifts off resonance mid-run.
-
Use regulated, temperature-compensated gate bias and feed VDD to each drain separately so high DC currents stay out of the RF output transformers.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable to a homebrew 9 MHz LDMOS deck: thermal-tracking bias prevents runaway, and DC-free transformers avoid core saturation at high drain current.
-
Add degenerative (negative) feedback to a broadband MOSFET power amplifier for stability; the QST author retrofitted it only after a 'smoke in the cockpit' failure in service.
Source, quote & tabletop applicability
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
Tabletop: A dee resonator is a narrowband, sometimes-detuned load; build feedback in from day one rather than after the first blown transistor.
-
Never bolt an LDMOS device straight to an aluminum heat sink: flow-solder it to a thick copper heat spreader first, then mount the spreader to the heat sink with thermal paste.
Source, quote & tabletop applicability
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
Tabletop: At 100-500 W a copper spreader under the LDMOS pallet is cheap insurance against the die-temperature excursions that killed the reference machine's earlier MOSFET amps.
-
Expect the third harmonic of a push-pull Class AB amplifier to be only 8-10 dB down (the second harmonic is suppressed by symmetry), so output low-pass filtering is mandatory, not optional.
3rd harmonic ~ -8 to -10 dBc before filtering; ARRL-measured suppression after filtering: 48-66 dBSource, quote & tabletop applicability
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
Tabletop: At 9 MHz the 27 MHz third harmonic can excite spurious dee-resonator modes and detune the match; filter it between amp and matching network.
-
Prefer a diplexer (absorptive) harmonic filter over a plain reflective low-pass filter on a solid-state HF amplifier, because harmonic energy reflected back into the FET drains can drive oscillations.
Source, quote & tabletop applicability
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
Tabletop: The dee is a high-Q load that reflects everything off-resonance; an absorptive diplexer gives the LDMOS a resistive termination at harmonics and protects against the mismatch failures the builder has already had.
-
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 & tabletop applicability
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
Tabletop: When copying an LDMOS pallet layout, reproduce the output-transformer connection geometry exactly; millimeter changes shift the match at hundreds of watts.
-
A dummy dee (grounded bar) of 3/8-inch thickness gives satisfactorily low distortion of the accelerating field lines relative to a full second dee (verified in Poisson Superfish at 10 kV).
dummy dee thickness 3/8 in = 9.5 mmSource, quote & tabletop applicability
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
Tabletop: Supports the single-dee/dummy-dee topology at the reference machine's scale; a ~10 mm grounded bar is field-equivalent enough to a second dee and frees chamber space.
-
The beam envelope is widest at one-third to one-half of final radius and narrows toward extraction as sqrt-n damping compresses axial oscillations (MIT: 0.8 in initial amplitude damped to ~0.1 in at the exit slit).
amplitude damping z/z0 ~ n^(-1/4) growth regions combined; MIT overall damping factor ~0.12 center-to-exitSource, quote & tabletop applicability
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
Tabletop: Give the first third of radius generous vertical aperture (that is where ions are lost); the outer region can be tight, which also helps RF economy.
-
Use graphite for arc bodies, cones, and dee feelers near the source - it runs hot with minimal sputtering and evaporation; use feeler extensions on the dee faces opposite the source to raise the extraction field and improve first-turn focusing.
Source, quote & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 166-178
Tabletop: Graphite source parts keep metal sputter off insulators and chamber walls; a feeler (puller) on the dee edge is the single cheapest first-turn-capture upgrade.
-
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 & tabletop applicability
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
Tabletop: Explains why source-to-dee geometry (chimney position, puller gap, aperture height) dominates beam capture on small machines: the magnet cannot help until several turns out.
-
Particulate contamination on the cathode, not the electrode material, determines vacuum breakdown: at 95 MV/m (14.5 kV across 150 um), 40 of 52 particle-contaminated sites broke down versus only 1 of 16 clean sites.
150 um gap, 14.5 kV -> ~95 MV/m; contaminated 40/52 fail vs clean 1/16Source, quote & tabletop applicability
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
Tabletop: The single biggest lever on the reference machine's dee-voltage ceiling: gloves, solvent cleaning, and dust-free assembly of dee and stem buy more holdoff than any material upgrade.
-
Practical vacuum-gap breakdown fields span 5-200 MV/m, and smaller gaps withstand higher fields; clean millimeter-scale electrodes routinely hold >100 MV/m, so a well-prepared mm-scale gap at tens of kV is far from intrinsic limits.
breakdown range 5-200 MV/m; clean electrodes >100 MV/m at 150 um gapsSource, quote & tabletop applicability
breakdown occurs between 5 and 200 MV/m ... In general, smaller gaps can withstand higher fields.
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 78, 95
Tabletop: At 13 kV across the reference machine's ~6 mm gap the mean field is only ~2 MV/m - if it sparks there, the cause is edges, insulators, particles or gas pressure, never the vacuum gap itself.
-
Spark conditioning works: in the early-processing regime each breakdown is overwhelmingly likely to raise the site's breakdown field (successive/previous ratio > 1 up to ~100 MV/m), so deliberate controlled arcing is a legitimate in-situ cleaning technique.
E_breakdown(n+1)/E_breakdown(n) > 1 in early processing; gains shrink toward a saturation fieldSource, quote & tabletop applicability
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
Tabletop: After assembling the next machine, the builder should ramp dee voltage slowly and let a limited number of current-limited sparks condition the surfaces before declaring a voltage ceiling.
-
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 & tabletop applicability
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
Tabletop: Directly applicable at 1.3 kV and above: give the stem a continuous insulating sleeve with generous creepage past the grounded feedthrough.
-
Round every high-voltage edge and check it against Emax = 0.9V/(r*ln((r+a)/r)); aluminum breaks down near 290 kV/inch, and Rutgers chose a 0.1875-in minimum edge radius to keep the peak field at 170 kV/inch (~60% of the limit).
Emax = 0.9V/(r*ln((r+a)/r)); Al limit 290 kV/in; r_min = 0.1875 in -> Emax = 170 kV/inSource, quote & tabletop applicability
Aluminum=290 kV/inch ... We settled on a minimum radius of R=.1875 inches ... Emax=170 kV/inch
Tabletop: The edge-radius rule the builder needs when pushing dee voltage to 5-13 kV: radius all dee and stem edges so the enhanced edge field stays under ~half the material's breakdown value.
-
Support the dee against the dummy dee with machinable-ceramic spacer strips (Houghton used four, ~2.5 x 0.77 x 0.18 cm) setting a 0.635 cm acceleration gap; the earlier glass insulators were destroyed by a discharge.
gap = 0.635 cm; 4 ceramic strips 2.53 x 0.77 x 0.18 cmSource, quote & tabletop applicability
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.
Tabletop: Machinable ceramic (Macor-class) spacers are the spark-tolerant choice for holding the reference machine's dee-to-dummy-dee gap, replacing glass or plastic.
-
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 & tabletop applicability
This design strategy made it impossible to fix a single component of the apparatus, such as the insulation, without replacing the entire piece.
Tabletop: A next machine should assume sparks WILL damage insulators eventually; screw-together modularity turns a total rebuild into a one-part swap.
-
Vent every blind screw hole in the dee (Houghton drilled a No. 55 side hole into each) so trapped air/water doesn't slowly outgas into the vacuum.
No. 55 drill (~1.3 mm) side vent per screw holeSource, quote & tabletop applicability
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.
Tabletop: Directly applicable to any screwed-together dee on a next machine: unvented blind holes are virtual leaks that cap the achievable base pressure.
-
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 & tabletop applicability
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
Tabletop: Matches the reference machine's ~1.3 kV operating point today; at their planned 5-13 kV the same geometry needs proportionally more ceramic creepage distance.
-
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 & tabletop applicability
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.
Tabletop: Direct fabrication template; the single-Dee-plus-dummy topology halves the RF feedthrough problem versus two live Dees.
-
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 & tabletop applicability
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
Tabletop: Directly applicable: at 1.3 kV the reference machine's protons make many turns; the single biggest transmission lever for a next machine is more dee volts, not more source current.
-
Cool dees by furnace-brazing flattened copper tubing to thin (1/8 inch) copper dee plates rather than machining internal channels; it performs as well and is far cheaper, with flow concentrated along the accelerating edge where heating peaks.
Source, quote & tabletop applicability
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
Tabletop: At 1.3 kV the builder needs no water; if a next machine's dee runs kilowatt-class RF, soldered-on flattened tubing along the dee lip is the proven cheap construction.
-
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 & tabletop applicability
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
Tabletop: Perforation transfers directly (pressure inside an unvented dee can be much worse than gauge pressure); graphite armor matters only if a next machine reaches activation-capable energies.
-
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 & tabletop applicability
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
Tabletop: Moot for pump choice today, but the underlying rule stands: condensable metal vapors on HV electrodes trigger field emission; keep electrode surfaces free of conductive films.
-
A canal-ray (obstructed glow) proton source produces maximum proton output at a discharge voltage of about 20 kV; only a small fraction of discharge current becomes protons, so run 10-100 mA of discharge to get ~1 mA of beam (about 5%).
optimum discharge ~20 kV; I_beam/I_discharge ~ 1 mA / 20 mA = 5%Source, quote & tabletop applicability
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
Tabletop: Sets the historical proton-conversion baseline: expect percent-level proton yield from a gas discharge and budget discharge power accordingly.
-
Keep the anode-cathode annular gap small (~4 mm) so no discharge can build up in the gap; the discharge then concentrates naturally on the cathode canal hole, and cathode/tube parts may run red-hot and radiate their heat.
anode-cathode radial clearance ~4 mm (below discharge maintenance distance at operating pressure)Source, quote & tabletop applicability
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.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 260-261
Tabletop: The 'gap smaller than the dark space' principle is how the builder can force their source discharge to localize at the extraction aperture rather than wander.
-
A fresh hydrogen discharge beam is largely molecular H2+ ions; only after extended running does it become nearly all protons, so condition the source before assuming beam species, and verify with magnetic analysis.
H2+ of energy E behaves like two protons of E/2 each: disintegration threshold doubles, curve rises twice as steeplySource, quote & tabletop applicability
At first this beam consists very largely of molecular ions, but after running for some time it changes over and becomes nearly all protons
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 261-262, 269
Tabletop: Critical for p-B11: an unconditioned source delivers H2+ that behaves as half-energy protons, silently killing the expected alpha yield at fixed magnetic rigidity.
-
Degas an accelerating column by running a hydrogen discharge at 20-60 kV at the highest possible current density for about half an hour; after pumping out, the tube holds 200 kV stably, and thereafter ~30 min of morning running restores steady state.
conditioning discharge 20-60 kV, ~30 min -> holds 200 kVSource, quote & tabletop applicability
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
Tabletop: A concrete glow-discharge conditioning schedule the builder can scale for dee and extraction electrodes that must hold voltage without sparking.
-
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), suspect meager ion production rather than RF voltage or focusing.
Source, quote & tabletop applicability
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
Tabletop: A triage rule for the reference machine's low-current debugging: measure current at small radius first; if it's already low there, more RF power won't fix it - the source will.
-
Run the ion source as a low-voltage hot-cathode arc: 2-3 A discharge at 100-150 V, cavity pressure ~1e-2 mm Hg maintained through the exit hole, gas flow ~2 cm3/min (STP); expect ~0.5 mA resonant beam from such a source.
arc 3 A @ 100 V; electron beam ~2 A; gas 2 cm3/min atm; cavity ~1e-2 mm Hg; resonant beam ~0.5 mASource, quote & tabletop applicability
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
Tabletop: These operating points scale down gracefully; the key architecture point - a differentially pumped cavity at ~1e-2 torr feeding a chamber at 1e-5 - applies at any size.
-
Heat the source cathode with DC or ~100 kHz AC, never mains-frequency AC, to avoid vibration damage from the magnetic field; keep oxygen out of the gas (it erodes the cathode) and expect 100-200 hr filament life.
cathode: heavy W or Ta rod; heating dc or ~100 kc; life 100-200 hrSource, quote & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 177-178
Tabletop: A 60 Hz-heated filament in a 0.59 T field literally shakes itself apart; DC heating and clean hydrogen are cheap reliability.
-
Design for operating pressure ~2e-5 mm Hg with source gas flowing (base <1e-6); the ion-source gas load, not outgassing, sets the working pressure, so put pumping speed close to the dees.
MIT: 2400 l/s on 2000 l volume; base <1e-6 mm Hg, operating ~2e-5 mm Hg with D2 flowSource, quote & tabletop applicability
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
Tabletop: The builder should expect an order-of-magnitude pressure rise when hydrogen flows; low-2e-5 territory while running is normal and workable, not a leak.
-
Heat the spiral filament ion source with high-frequency AC rather than DC or mains AC, to avoid the self-generated J x B forces tearing the spiral apart in the main magnetic field.
Source, quote & tabletop applicability
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
Tabletop: Concrete fix for a failure mode the builder will hit at 0.6-1.7 T with a hairpin/spiral filament: filament life is a chronic tabletop problem.
-
Penning-source housekeeping numbers: gas consumption 0.2-0.6 sccm, source pressure 1-10 Pa, ignition needs 3-5 kV even if the running arc is 0.3-1.3 kV, extraction 5-25 kV, anode (chimney) apertures 1x25 to 1.5x45 mm with cathode spacing 6-25 cm in big machines.
gas 0.2-0.6 sccm; p_source = 1-10 Pa; V_ignition = 3-5 kV; V_arc = 0.3-5 kV; V_extraction = 5-35 kVSource, quote & tabletop applicability
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
Tabletop: The reference machine's MFC should be sized and calibrated around the 0.1-1 sccm range, and the arc supply must tolerate a several-kV open-circuit ignition transient before folding back to run voltage.
-
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 & tabletop applicability
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
Tabletop: Do not clamp Ta filament legs directly in stainless fixtures near the hot zone; use Mo or graphite intermediate parts in the next machine's chimney.
-
Pick hot-zone insulators by temperature and outgassing: quartz and Macor to ~1000 C, boron nitride excellent to 1200 C but absorbs water and outgasses badly (bake gently first), alumina to 1400 C is the workhorse; BN releases nitrogen above 1500 C.
quartz 1000 C; Macor ~1000 C; BN 1200 C (1500 C max, decomposes); alumina 1400 C; zirconia 1600 C but conducts above 1000 CSource, quote & tabletop applicability
Boron nitride is an excellent material for most applications for temperatures up to 1200 C... 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
Tabletop: 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 & tabletop applicability
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
Tabletop: 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.
-
Design extraction optics around an aspect ratio (aperture radius : gap) of S ~ 0.5, which gives a per-aperture current limit I[mA] = 0.703*sqrt(q*/u)*U[kV]^1.5 and minimum divergence; the plasma density must then be matched to the field or the beam over/under-focuses.
S = r/d ~ 0.5; I[mA] = 0.703*sqrt(q*/u)*phi[kV]^(3/2); divergence w0 = 0.5*(r/d)*(1 - 1.67*Pi_normalized) for round aperturesSource, quote & tabletop applicability
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
Tabletop: For the puller gap in a next machine: make the source-slit half-width about half the slit-to-puller distance, then tune arc density (not geometry) until the beam is parallel.
-
Size thermionic cathodes with the Richardson formula and treat temperature as the only real knob: a 10% temperature change swings emission roughly 10-fold, so regulate filament heating current 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 & tabletop applicability
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
Tabletop: The reference machine's hydrogen filament source lives or dies on filament temperature stability; a constant-current supply with fine adjustment is worth more than raw power.
-
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); filament V ~ sqrt(d)*l, I ~ d^1.5, independent of lengthSource, quote & tabletop applicability
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
Tabletop: 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.
-
Run refractory filaments at the lowest temperature that gives enough emission -- evaporation lifetime is savage: a 1-mm W wire lasts ~8,300 h at 2500 K but ~46 h at 2900 K; a 1-mm Ta wire ~7,000 h at 2400 K but ~350 h at 2600 K; lifetime scales linearly with wire diameter, and Ta (the easiest refractory to form) embrittles in hydrogen.
W: 2500 K -> 0.30 A/cm^2, 8.3e3 h (1 mm); 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 & tabletop applicability
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
Tabletop: For a next machine, a fatter filament run cooler at ~0.1-1 A/cm^2 buys weeks of run time instead of days; treat used Ta hairpins as brittle after hydrogen exposure.
-
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 & tabletop applicability
Gas efficiency: >50% for hydrogen and higher for other gases.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 57, 69, 110
Tabletop: At 0.2 sccm feed and 50% efficiency only ~0.1 sccm of H2 leaks into the chamber; doubling source gas efficiency is worth as much as doubling pump speed for keeping the beam path at low pressure.
-
Expect only 10-100 h filament life in a working arc source; the proven quiet-arc template (Freeman) is 40-70 V at 1-3 A with a massive 2-mm Ta/W cathode rod heated by ~130 A, and since erosion concentrates at the positive filament end, periodically reversing DC heater polarity extends life (AC evens wear but adds energy spread).
filament life 10-100 h; Freeman window: V_arc = 40-70 V, I_arc = 1-3 A, 2-mm-dia rod cathode, I_heat ~ 130 A, B ~ 0.01 T; reverse heater polarity at ~half-lifeSource, quote & tabletop applicability
The arc current is 1 to 3 A and the arc voltage just 40 to 70 V... The lifetime of the source is given by the lifetime of the filament, which is between 10 and 100 h... Changing the polarity of the filament... improves cathode lifetime.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 73
Tabletop: For a next machine: a thick rod cathode instead of thin wire is the cheapest lifetime upgrade, plus a DPDT reversing switch on the heater and an arc-hours log.
-
Standard extraction/exit slit for slit-type arc sources is about 2 mm wide by 40 mm long; going longer (up to 90-100 mm) degrades current-density uniformity along the slit because of the voltage drop along the cathode.
slit ~ 2 x 40 mm typical; 100 x 5 mm max realizedSource, quote & tabletop applicability
The extraction slit is usually about 2 mm wide and about 40 mm long. Larger slits are possible, such as 90 mm, but... the current density is not uniform along the long slit.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 74, 76
Tabletop: For a cyclotron chimney only the few-mm of slit facing the dee gap matters; a ~1-2 mm wide slit is the proven starting width before puller optimization.
-
PIG/Penning discharges split into two useful regimes: cold-cathode (arc >1 kV at 0.5-5 A) and hot-cathode (arc <1 kV at 1-50 A); the magnetic field barely matters above a minimum of ~0.1 T, and arc voltage rises as gas flow is cut until the arc 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 & tabletop applicability
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
Tabletop: The reference machine's cyclotron field (>0.1 T at the center) already satisfies the PIG minimum, so a next machine's internal PIG source can trade the fragile filament for a self-heated cathode running a sub-kV, multi-ampere arc.
-
Extracted current from a PIG source is proportional to arc current, at roughly 10-100 (mA/cm^2) of extracted current density per ampere of arc for extraction through the anode slit -- so beam scaling is done with the arc supply, not the extraction voltage.
j_extracted ~ (10-100 mA/cm^2) per A of arc current; ion current density at cathodes is 5-10x that at anodeSource, quote & tabletop applicability
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
Tabletop: With a ~1 mm^2 chimney slit, even a 1-A arc gives ~0.1-1 mA available at the slit, orders of magnitude above the reference machine's nA beams; source output will not be the bottleneck.
-
Cold-cathode PIG arcs are limited to about 1 kW per cathode before uncontrolled thermionic emission sets in; a cathode is worn out when its sputter-erosion crater depth reaches about the anode bore radius, after which the discharge goes 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 & tabletop applicability
The arc power for cold cathode operation is limited to about 1 kW per cathode... The cold and hot cathodes are worn out when the erosion crater's depth reaches around the anode bore radius.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 84-85
Tabletop: Gives a concrete inspection criterion: measure the cathode pit depth against the chimney bore 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 cathode can be burned down completely without instability -- the standard cyclotron internal-source upgrade path.
e-bombardment heating: 0-2 kV / 0-2.5 A onto cathode rear; filament itself 50-150 A at 2-8 VSource, quote & tabletop applicability
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
Tabletop: A next machine's source can keep a small filament hidden behind a Ta block cathode, out of the hydrogen plasma, converting filament sputtering into slow self-sputtering of a thick block.
-
Expect the open-filament arc to run 0.5-2 A at 100-500 V at ~1e-4 mm Hg; strike it at 0.5-1 A and 100-200 V, and set filament emission 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 & tabletop applicability
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
Tabletop: Directly applicable operating envelope for a simple hot-filament source at the reference machine's scale.
-
Admit hydrogen so tank pressure rises by about 1e-4 mm above base while watching arc current; control flow with a long-taper needle valve, a thread-leak, or a heated palladium leak.
delta-P(H2) ~ +1e-4 torr over base pressureSource, quote & tabletop applicability
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
Tabletop: Directly applicable gas-flow set-point; the reference machine's parker metering valve fills the needle-valve role.
-
Use an ion source filament of ~0.025-inch tungsten (about 25 A at a few volts) instead of fragile automobile-lamp filaments, and float the filament supply across a storage battery to filter ripple that vibrates the filament.
0.025 in W filament ~ 25 A dc at a few voltsSource, quote & tabletop applicability
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
Tabletop: Directly applicable filament sizing; the modern equivalent of the battery filter is a well-filtered DC (not raw rectified) filament supply to stop magnetically driven filament vibration.
-
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 & tabletop applicability
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
Tabletop: A proven upgrade from a bare filament for a next machine: better-defined source position, less RF loading of the plasma.
-
Beam current improved an order of magnitude (10 -> 70 pA) by running higher frequency, lower H2 partial pressure (2.2e-6 vs 1.5e-5 torr), lower base pressure, and a much smaller filament bias (-6 V vs -100 V) - gas scattering and source conditions dominate over RF power.
6.04 MHz, H2 2.2e-6 torr, -6 V filament -> 70 pA vs 3.55 MHz, 1.5e-5 torr, -100 V -> 10 pASource, quote & tabletop applicability
Higher frequency, lower H2 and base pressure, lower filament voltage
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 17-18
Tabletop: For the reference machine's current-hunting: before adding RF watts, cut chamber pressure and re-optimize filament bias - Houghton's 7x gain cost zero watts.
-
Make the inner grid diameter about one-fifth of the chamber diameter and keep geometric transparency above 92%; three loops of 0.114 mm tungsten wire on a 4.2 cm sphere give 99.2% transparency.
d_grid ~ D_chamber/5; transparency = 1 - (pi*d_grid*N_loops*d_wire)/(4*pi*r^2) >= 0.92Source, quote & tabletop applicability
fusion efficiency is enhanced by transparency of at least 92 percent (Donovan). The inner grid is 99.18 percent transparent with three loops
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 19-20
Tabletop: The transparency bookkeeping (wire cross-section vs aperture area) is the same calculation the builder needs for any grid, mesh, or slit that their beam must pass repeatedly.
-
Choose grid/electrode wire for high melting point, low sputter yield, and HIGH work function (to suppress parasitic thermionic electron current); the supply cannot tell an ion arriving from an electron leaving, so every emitted electron steals ion current from the same supply budget.
I_supply = i_ion + i_electron at fixed P_ext = V*I; maximize ion fraction by high-work-function, cool gridSource, quote & tabletop applicability
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
Tabletop: When the builder meters 'beam current' anywhere near a hot cathode, part of it is electrons; a high-work-function collector surface and magnetic electron suppression keep the nA readings honest.
-
Thermal limit of a wire electrode: maximum steady current before sagging is I = A*eps*sigma*T^4/V (black-body balance); a 10-cm stainless grid (A~76 cm^2, eps~0.15, sag at ~1500 K) can only handle ~9.5 mA at 200 kV, so stainless caps usable power.
I_max = A*eps*sigma*T_safe^4 / V; SS: melt ~1800 K, sag ~1500 K, eps ~0.15Source, quote & tabletop applicability
Assuming that sagging occurs at ~1,500 K and equating the black body radiation rate to the input power... This gives 9.5 mA of ion current at 200 kV.
Tabletop: Same balance sizes any wire electrode, probe, or beam stop in the reference machine's chamber: compute AeσT^4 at the material's sag temperature and keep beam-power deposition below it.
-
W-25%Re is the sweet-spot electrode alloy: melting ~2800 K, low sputter yield, spot-weldable and formable (unlike pure W); a stainless grid lasted under a week at power while the W-25Re grid ran 30-130 kV at 30-180 mA for >1,000 h and survived over 2 years.
W-25%Re: T_melt ~ 2800 K; validated 30-130 kV, 30-180 mA, >1000 h; pure W spot-welding needs Ni foil interlayer (Ni then limits temperature)Source, quote & tabletop applicability
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.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 145-146
Tabletop: W-Re thermocouple wire is commercially available in small quantities and is the best upgrade for any sputtered electrode in the reference machine's source: W durability with Ta-like workability.
-
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 & tabletop applicability
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.
Tabletop: When the builder scales chamber geometry or pressure for the p-B11 test cell, keep pd constant to preserve the discharge; and remember all sputtering damage happens at the cathode sheath edge.
-
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 & tabletop applicability
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.
Tabletop: Explains why the reference machine's source may need a several-kV kick to strike but then runs at a few hundred volts, and why current-limited (ballasted) supplies are mandatory to stop glow-to-arc runaway.
-
In a gridded low-pressure device the ion mean free path sets ignition: at 2 mTorr the ion mfp is ~7 cm and striking voltages reach tens of kV, at 20 mTorr the mfp is ~0.7 cm and striking is easy; typical hydrogen/deuterium operation is 2-15 mTorr with breakdown at 5-50 kV.
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 & tabletop applicability
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
Tabletop: For any glow-driven ion supply in the p-B11 experiment, pressure is the ignition control: strike at higher pressure, then throttle the MFC down to the running point.
-
A transparent wire cathode breaks down at ~3x lower pd than a solid cathode at the same voltage, because ions recirculate through the grid; below ~0.5 Torr-cm the discharge self-organizes into microchannels ('Star mode') whose effective transparency far exceeds geometric transparency -- so use large grid openings rather than fine mesh.
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 & tabletop applicability
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.
Tabletop: If the builder builds an IEC-style p-B11 test stand, a few large openings aligned with the beam axis beat a fine mesh: fewer grid hits, higher effective transparency, longer grid life.
-
To ionize low-pressure gas (1-10 microns) for a beam-mode device, add a hot filament electron emitter just outside the main electrode structure biased about +200 V with respect to ground.
filament bias ~ +200 V, located outside outer gridSource, quote & tabletop applicability
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
Tabletop: Matches the reference machine's hydrogen filament source philosophy: a modest positive bias (order 100-200 V) on/near an emitter sustains ionization at pressures where a self-sustained discharge dies.
-
Electrically shield (insulate) the support structure of a negatively biased electrode so ions bombard only the intended electrode, not its stalk and feedthrough.
Source, quote & tabletop applicability
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
Tabletop: Same rule protects the reference machine's Faraday cup stalk and source supports: unshielded biased metal collects spurious current and sputters.
-
Do not expect filament bias voltage (tested around -90 V) to move beam current; on the Houghton machine it had no significant effect.
beam current insensitive to filament bias (tests near -90 V)Source, quote & tabletop applicability
It appears that filament bias has no effect on the beam current.
Tabletop: Saves tuning time: spend effort on dee voltage and pressure, not filament bias, when hunting current.
-
With an internal fill-gas ion source there is an optimal chamber pressure band (about 1e-5 to 3e-5 Torr on the Houghton machine): current first falls then rises as pressure is lowered, and the very lowest pressures starve ionization.
operating band ~1-3e-5 Torr; highest raw current seen ~1e-4 Torr but with badly broadened resonancesSource, quote & tabletop applicability
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.
Tabletop: Gives the builder a target pressure window and the expected non-monotonic current-vs-pressure curve to map on their own machine.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Run the chamber between 1e-6 and 1e-4 Torr of hydrogen: below that there is too little gas to ionize, above it neutral collisions shorten the mean free path and the resonance peaks broaden and shift; peak current (~0.1 uA) came at ~1e-4 Torr.
operating pressure 1e-6 to 1e-4 Torr; best current 0.1 uA at ~1e-4 Torr; typical running 2e-5 TorrSource, quote & tabletop applicability
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.
Tabletop: Directly sets the gas-handling operating window for the reference machine and explains a common 'no beam' failure at too-good vacuum.
-
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 & tabletop applicability
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.
Tabletop: An amateur-grade insulated feedthrough scheme (alumina tube + Ceramabond) the builder can reuse for chimney anodes or filament leads inside the next machine.
-
A cold-cathode PIG built from an iron cathode body, ~3 kG SmCo permanent magnet, folded 0.13 mm stainless sheet anode, and iron faceplate with a 6.4 mm axial aperture delivers a continuous 1 mA H+ beam at 1 mTorr with 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 & tabletop applicability
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
Tabletop: A directly copyable permanent-magnet source recipe for the next machine's external or test-stand source at exactly hobby machining tolerances.
-
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 & tabletop applicability
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.
Tabletop: Directly applicable to the reference machine's filament/arc supply metering; logging supply volts instead of electrode volts corrupts any operating-point map.
-
In a compact source-in-chamber setup the pressure inside the ion source is only about 2x the chamber pressure, so simply backfilling the chamber can substitute for direct gas injection into the source.
P_internal ~ 2 x P_chamber (small chamber, direct injection)Source, quote & tabletop applicability
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.
Tabletop: The reference machine's MFC feed into the source chimney matters most when the main chamber is well-pumped; in a small chamber the distinction between injection and backfill largely disappears.
-
A PIG discharge ignites easily at 1 kV or less; usable beam appears from ~600 V (0.3 mA discharge, 21 uA target) and grows monotonically with voltage to the design point.
H2, 1 mTorr: 580 V -> 0.3 mA disch / 20.8 uA target; 5.4 kV -> 6.0 mA / 1.5 mASource, quote & tabletop applicability
the plasma discharge ignites easily at 1 kV or less for all cases and produces a continuous positively charged ion beam.
Tabletop: Tens-of-uA proton output at under 1 kV anode drive is ample for the reference machine's nA-scale accelerated beam; a multi-kV arc supply is not required to start.
-
Expect extracted (target) current to be roughly 20-25% of PIG discharge current; scale beam current 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 & tabletop applicability
the source has a current utilization efficiency (ratio of target to discharge current) of 25% and requires 32.4 W of power.
Tabletop: Gives the builder a sanity check: nA-to-uA beams need only uA-to-mA class discharges; if their beam/arc ratio is far below ~20% the extraction geometry is losing beam.
-
For DC post-acceleration of a PIG beam, place a negatively biased suppressor electrode ~2.5 cm downstream of the source faceplate and the target ~7.6 cm beyond it; this focused a 1 mA H+ beam at only 0.4 mTorr and 10.5 W of source power with up to -30 kV acceleration.
suppressor at 2.5 cm, target at +7.6 cm, both biased negative w.r.t. grounded cathode; 1 mA at 0.4 mTorr, 10.5 WSource, quote & tabletop applicability
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.
Tabletop: Template for a bench extraction test stand to characterize the next machine's source before it goes into the magnet.
-
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 & tabletop applicability
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
Tabletop: Benchmarks source lifetime for a next machine; hot filaments burn out far faster than a cold-cathode PIG at this scale.
-
Separate the source's gas-fed discharge region from the main vacuum with a tight-fitting boron nitride insulator; 2.5 sccm of H2 into the chimney holds the main chamber near 4e-5 Torr against a good pump (base 8e-7 Torr).
2.5 sccm H2 -> 4e-5 Torr chamber (base 8e-7 Torr); BN insulator isolates ~1e-5 Torr regionSource, quote & tabletop applicability
With a gas flow rate of 2.5 cc/min of hydrogen, the pressure in the main vacuum chamber is around 4e-5 Torr.
Tabletop: A direct benchmark for the reference machine's MFC-vs-chamber-pressure curve; large deviations from ~1.5e-5 Torr per sccm (at similar pumping speed) indicate leaks or conductance problems.
-
A cold-cathode PIG needs only a ~3 kV current-limited supply to strike and run: after striking, the arc voltage drops to whatever sustains the set current; the 1.9-3.8 mm cathode-anode gap is not a critical parameter.
strike supply 3 kV / 1 A current-limited; running arc voltage < 3 kV; gap 0.075-0.150 in non-criticalSource, quote & tabletop applicability
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.
Tabletop: Relaxes the reference machine's machining tolerances on the next machine's source gap and sizes the arc supply: a 3 kV current-limited unit suffices.
-
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 & tabletop applicability
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).
Tabletop: At the reference machine's much lower arc powers passive/conductive cooling may suffice, but the sanded-cathode arc-striking trick transfers directly.
-
For reference, hot-filament internal sources run far harder than cold-cathode PIGs: Livingston and Jones heated a U-shaped tantalum filament with ~400 A, ran 2-6 A of arc, and extracted 150 mA of protons 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 & tabletop applicability
Their cathode was a U-shaped tantalum filament, heated with about 400 amps... able to extract 150 mA using a puller voltage of 12kV and a source-puller gap of about 0.13 (3.3 mm).
Tabletop: Brackets the design space above the reference machine's filament source: proton output scales with arc current and slit area over 3+ orders of magnitude, so their nA needs are met with sub-ampere arcs.
-
Chimney slit width is the dominant knob on an internal PIG's output: doubling the 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) at the cost of ~1.7x radial 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 & tabletop applicability
The chimney with the larger slit produces a beam with a larger emittance. However, the beam is also of higher intensity.
Tabletop: Tells the builder exactly what to expect when they widen their next machine's chimney slit: current scales faster than linearly with width, emittance grows more slowly - widen until the machine acceptance is filled.
-
A DC extraction test stand characterizes an internal source before installation: a puller with 12.7 mm radius of curvature holds 50 kV across a 5.0 mm minimum source-puller gap (~10 kV/mm design margin); 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 (roughly 10 kV/mm)Source, quote & tabletop applicability
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
Tabletop: Sets the reference machine's dee-tip/puller gap voltage budget: with clean electrodes, plan on order 10 kV per mm of gap and generous edge radii.
-
Prefer a slit chimney over a hole chimney for beam quality: the slit gives a flat plasma boundary and converging beam, while a hole (1.19 mm, 60 degree chamfer) gives 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/(m2-sr) at 50 mA arcSource, quote & tabletop applicability
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
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 73-76, 91-107
Tabletop: Decides a next machine's chimney aperture style: cut a tall narrow slit, not a drilled hole, if beam brightness and predictable optics matter.
-
Raising PIG arc current raises beam current sub-linearly: for the 0.25 mm slit, 50 to 450 mA arc gave 52 to 227 uA of beam while beam/arc efficiency fell from 1.0e-3 to 0.5e-3 and emittance stayed flat; luminosity still 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 & tabletop applicability
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
Tabletop: For the builder: cranking arc power buys current with diminishing returns but does not spoil beam quality below ~230 uA - space charge is negligible at their nA-uA scale.
-
Keep hydrogen flow at or above ~2 sccm: at normal flows (2-6 sccm, arc 50-350 mA, arc voltage under 3 kV current-limited) the cold-cathode PIG beam contained no detectable H2+, but at 0.5 sccm the arc jumped to voltage-limited mode and molecular ions appeared.
flow >= 2.0 sccm -> pure proton beam; 0.5 sccm -> mode shift (3.5 kV limit, arc drops to 90 mA) + H2+Source, quote & tabletop applicability
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.
Tabletop: Directly actionable on the reference machine's MFC: starving the source of gas silently changes beam species; their flow setpoint should stay above the arc-mode transition.
-
When simulating orbits from an internal PIG, start ions on the plasma boundary with a plasma temperature of ~35,000 K (central starting energy ~4.5 eV); this reproduces measured emittance for both slit and hole chimneys.
T_plasma ~ 35,000 K; E_start ~ 4.5 eV; flat boundary (slit) / concave boundary (hole)Source, quote & tabletop applicability
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
Tabletop: Gives the builder the initial-condition recipe for any first-turn orbit simulation of their next machine's central region.
-
Use a fine-taper metering valve with a vernier handle for gas admission (Series 20: Cv 0.029, 0.055 in orifice, 3-degree stem taper, 9 +/-1 turns open) so flow settings are repeatable.
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 & tabletop applicability
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
Tabletop: The 3-degree-taper Series 20 spread over 9 turns gives the fine, repeatable hydrogen admission an ion source needs; log turns-open as the process setpoint.
-
Never use a metering valve as the shut-off: Parker states these valves are not for positive shut-off (use a separate bubble-tight valve in series), and pressure is limited to 1000 psig upstream, 500 psig downstream.
max 1000 psig operating (downstream limited to 500 psig); elastomer limits: Buna-N -10 to 250 FSource, quote & tabletop applicability
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
Tabletop: Put an isolation valve between the gas bottle and the metering valve; forcing the tapered stem closed to seal will ruin the calibrated taper and still leak into the vacuum system.
-
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 & tabletop applicability
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
Tabletop: Arc V-I and few-cc/min gas flow transfer almost unchanged to a small chimney source; graphite chimney/slit parts resist sputtering far better than copper or steel.
-
Make the source slit geometry adjustable and treat alignment of filament-to-defining-slot, arc slit, accelerating slit, and magnetic field as the critical tune: the filament must fully cover the defining slot and the slot edge sits tangent to the arc-slit plane.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
Regulate arc voltage and arc current as two independent servo loops - 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 & tabletop applicability
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
Tabletop: Directly applicable control philosophy, trivially implemented today with two small feedback supplies; a constant-current arc is what makes beam current reproducible shot to shot.
-
Machine face-seal grooves for vacuum to the Parker chart: for a 1/8 in. (0.139) cross-section ring use gland depth 0.101-0.107, squeeze 20-30%, vacuum groove width 0.158-0.164, groove radius 0.010-0.025.
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 & tabletop applicability
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
Tabletop: Directly hands the mill the numbers for every lid and port groove on the next machine's chamber; note the vacuum groove width is narrower than the liquid-service column.
-
Finish O-ring sealing faces to 16 RMS for vacuum and gas service (32 RMS is acceptable only for liquids), with groove sidewalls at 63 RMS and a 0-5 degree sidewall angle.
sealing face 16 RMS (vacuum/gas), 32 RMS (liquid); groove walls 63 RMS; sidewall taper 0-5 deg; break corners approx .005 radSource, quote & tabletop applicability
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
Tabletop: A fly-cut or turned finish on the chamber lid seat should be specified/checked to 16 RMS; a rougher face is a common reason a 1e-6 Torr system stalls in the 1e-5s.
-
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 & tabletop applicability
For External Pressure (inward pressure direction) dimension the groove by its inside diameter (Hi) and width: (H)i = Mean I.D. of O-ring
Parker Hannifin, O-Ring Handbook — Design Chart 4-3: O-Ring Face Seal Glands — p. 1
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: For a ~30-50 liter tabletop chamber the SI100 (~100+ l/s class) comfortably beats the 1 l/s-per-liter rule - margin that matters because source gas load dominates.
-
Use a double-gasket seal with a pump-out connection between gaskets on large or troublesome flanges so tightness can be tested quickly and a leak can be pumped away in service.
Source, quote & tabletop applicability
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
Tabletop: Worth adopting on a next machine's main lid: a guard-vacuum groove turns the worst leak hunt into a valve twist.
-
For static vacuum seals use face or dovetail grooves with heavy squeeze; increasing squeeze from 15% to 50% reduces helium leak rate dramatically, and above ~30% squeeze vacuum grease adds little further benefit.
squeeze 15% -> 30% -> 50% gives steeply decreasing He leak rate; grease benefit large at 15%, small at 30%, undetectable at 50%Source, quote & tabletop applicability
increasing the squeeze reduced the leak rate dramatically... at 50% squeeze the beneficial effect of the grease was not detectable.
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 3-4
Tabletop: Justifies cutting a next machine's grooves at the deep end of the squeeze range (25-30%) rather than greasing the rings harder; grease is a crutch for light squeeze.
-
Estimate O-ring permeation leak rate with L = 0.7*F*D*P*Q*(1-S)^2, where F is gas permeability of the elastomer, D ring ID in inches, P differential in psi, Q a squeeze/lubrication factor (~1.35 dry at 20% squeeze), S fractional squeeze.
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 & tabletop applicability
L = .7FDPQ(1-S)2 where: L = Approximate leak rate of the seal, std. cc/sec.
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 5
Tabletop: Lets the builder compute the permeation floor of their 10-inch Viton lid seal and check whether O-ring permeation, not leaks, sets their ultimate pressure.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Vacuum weight loss at 1e-6 Torr over two weeks is under 0.2% for butyl (0.18%), fluorocarbon (0.07-0.09%) and low-loss silicone, versus 1-3.5% for nitrile - avoid nitrile near optics, insulators, or RF surfaces.
% 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 & tabletop applicability
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
Tabletop: At exactly the reference machine's operating pressure: cheap Buna-N rings will slowly deposit oily film on feedthrough insulators and dee stems; Viton's 0.1%-class loss is why it is worth the money.
-
Pick low-permeability elastomers for vacuum: butyl is best (He permeability 6.5e-8 std cc-cm/cm2-s-bar), Viton fluorocarbon is close (12.7e-8) and adds 205 C capability, while silicone is ~37x worse (238e-8) and should be avoided as a vacuum seal.
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 & tabletop applicability
Butyl 6.5 @ 77F ... Fluorocarbon 12.7 @ 77F ... Silicone 238.0 @ 77F
Parker Hannifin, O-Ring Vacuum Sealing, Catalog 5705B (1998) — p. 7
Tabletop: Confirms Viton is a sound choice at 1e-6 Torr; if helium leak checking becomes routine, remember He walks through silicone and fluorosilicone.
-
Make alpha spectroscopy measurements with source-to-detector spacing of 1.5-2 times the detector diameter and vacuum better than 100 microns Hg (10 Pa).
spacing = 1.5-2 x detector dia; P < 100 um Hg (10 Pa)Source, quote & tabletop applicability
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
Tabletop: For his ~8 mm active-diameter PIPS, that is 12-16 mm standoff; closer spacing degrades resolution through wide-angle entrance-window losses.
-
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 & tabletop applicability
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
Tabletop: Size and maintain the SI100's backing pump so the foreline stays well under ~0.2 Torr even during beam-gas loads; a tired rotary pump silently pushes the foreline over the cliff and dumps oil vapor into the chamber.
-
Budget unbaked, uncleaned stainless steel at ~1e-5 Pa-m/s (~7.5e-9 Torr-L/s-cm2) after 10 h of pumping; reduce it 10-100x (cleaning, mild 40-80 C bake) for high vacuum, and 1e4-1e5x (150 C bake) for UHV.
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The 2.7 kg/cm figure sizes the lid bolting: a 10-inch-circumference seal needs on the order of 200+ kg of clamping just for the ring, before atmospheric load helps.
-
An unbaked Viton O-ring outgasses ~1e-3 Pa-m/s initially; a 4-h 150 C vacuum bake plus 12 h pumping drops it to 4e-7 Pa-m/s (2500x), but re-exposure to air reloads it with water.
Viton: 1e-3 Pa-m/s unbaked -> 4e-7 Pa-m/s after 4 h @150C + 12 h pumping; solvent washing is ineffectiveSource, quote & tabletop applicability
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
Tabletop: Pre-baking the Viton rings in a small vacuum oven before assembly is one of the cheapest order-of-magnitude improvements available to a diffusion-pumped 1e-6 Torr system.
-
Do not grease static elastomer seals: grease traps gas pockets that release as pressure bursts; if a scratched main-door flange forces it, apply the thinnest possible film with a lint-free cloth, and always wear gloves since finger oils have high vapor pressure.
Source, quote & tabletop applicability
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
Tabletop: Counters the amateur habit of greasing everything; on a clean 16 RMS seat with proper squeeze, dry Viton seals better and cleaner.
-
For a small diffusion-pumped system, cross over from roughing to high-vacuum pumping at ~100-150 mTorr (10-15 Pa): below that an oil-sealed rough pump backstreams (up to ~70x more oil at 1.3 Pa than at high pressure), above it the diffusion pump overloads.
crossover ~10-15 Pa (100-150 mTorr) for small chambers with oil-sealed roughing; viscous flushing suppresses backstreaming above ~15 PaSource, quote & tabletop applicability
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
Tabletop: The reference machine's chamber is exactly the 'prototypical small system': valve over to the SI100 at ~100 mTorr, don't let the rotary pump grind down to 10 mTorr first.
-
Systematic leak hunting: verify the blanked-off rough pump first, then pump sections sequentially to isolate the bad one; helium-spray external checks start at the TOP of the chamber with small flow, check welds and seals first, and use alcohol (which freezes in a leak) to temporarily plug one leak while checking neighbors.
Source, quote & tabletop applicability
External leak checking with helium should begin at the top of the chamber; only a small helium flow rate is necessary... Welds and seals are the most common leak sites
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 467-470
Tabletop: Helium rises - spraying from the bottom up floods every joint at once and destroys localization on a chamber with many ports.
-
Distinguish a leak from outgassing with a rate-of-rise test: valve off the pump and plot pressure vs time - a real (molecular) leak gives a linear rise indefinitely, outgassing rolls over toward a plateau set by vapor pressures.
Q = V*dP/dt; leak: dP/dt = const; outgassing: dP/dt decreasing to plateauSource, quote & tabletop applicability
A molecular leak causes a linear increase in pressure with time. Outgassing causes the pressure to rise to a steady-state value
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 468-469
Tabletop: First diagnostic to run whenever a next machine won't reach base pressure - it needs only the existing gauge and a stopwatch, and decides whether to reach for the helium bottle or the bakeout tape.
-
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 & tabletop applicability
The permeation time is about 20 min for a typical Viton O-ring... First, do not attempt to leak check the system during baking.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 469-470
Tabletop: On an all-Viton chamber, spray briefly and wait; a slowly rising He signal minutes after spraying is gasket permeation, not a leak at the last joint sprayed.
-
On an RGA, an air leak shows O2 at m/z=32 alongside N2 at 28 (ratio ~4:1 N2:O2); a big 18 peak with falling rate-of-rise is water outgassing - this single scan separates 'open the chamber' from 'keep pumping'.
air leak signature: m/z 28 with 32 present; water outgassing: dominant 18 (17) with decreasing rise rateSource, quote & tabletop applicability
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
Tabletop: A used RGA head is arguably the single best diagnostic upgrade for a next machine - one spectrum replaces a day of guessing.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: 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.
-
One adsorbed monolayer is ~1e15 molecules/cm2, and at 1e-6 Torr a clean surface re-covers with a monolayer in ~2.2 s (at 1e-9 Torr, ~2200 s) - at high vacuum the walls, not the volume, hold essentially all the gas.
monolayer ~1e15 molecules/cm2; monolayer time ~2.2 s @1e-6 Torr, 2.2e3 s @1e-9 Torr; at 1e-6 Torr surface/volume molecule ratio ~500Source, quote & tabletop applicability
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
Tabletop: Explains why pump-down history and surface cleanliness dominate over chamber volume: the reference machine's chamber volume empties in seconds, the walls take days.
-
A rate-of-rise test doubles as a proof test: measure Q = V(P2-P1)/(t2-t1) after isolating the vessel; a straight line means a real external leak (constant flow), a decreasing slope means outgassing or a virtual leak (internal, decaying source).
Q = V*(P2-P1)/(t2-t1) Torr-L/s; real leak: constant pressure rise; virtual leak/outgassing: decreasing riseSource, quote & tabletop applicability
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
Tabletop: The decreasing-vs-constant slope distinction also flags virtual leaks from unvented hardware, which a helium sprayer can never find from outside.
-
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 & tabletop applicability
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
Tabletop: Matches the reference machine's observed 1e-6 range with Viton - it is the natural floor of an all-elastomer system; a CF port or two on a next machine (gauge, RGA) buys headroom cheaply.
-
When helium leak checking: calibrate the detector against a standard leak before and after, use a low-flow tracer probe, keep helium away from elastomers, and bag/tape suspect regions to localize; specify leaks quantitatively (e.g. MSLD sensitivity 2e-10 atm-cc/s) and never as 'vacuum tight'.
typical MSLD sensitivity spec: 2e-10 atm-cc He/s; ASTM E432, E479, E493, E498, E499, F97Source, quote & tabletop applicability
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
Tabletop: When farming out a next machine's welds or buying used hardware, write the acceptance spec as a number (e.g. no single leak >1e-9 atm-cc/s He) - 'vacuum tight' is unenforceable.
-
Use published outgassing data comparatively, not absolutely: at 1 h under vacuum, aluminum ~80, unpolished stainless ~266, electropolished stainless ~66, slightly rusty mild steel ~58,520 (all x1e-10 mbar-L/s-cm2); after 4 h all clean metals converge to 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 & tabletop applicability
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
Tabletop: The 200x penalty for rusty mild steel is the argument for keeping any exposed magnet pole faces inside the chamber plated, painted with vacuum-compatible coating, or clad in stainless.
-
Generic cleaning sequence for vacuum components: mechanical clean, solvent degrease (acetone for tape/ink), detergent wash, water rinse between every bath, DI rinse to >2 Mohm resistivity, dry with filtered N2, then protect in lint-free wrap; a bakeout is the final step, and even glow-discharge-cleaned parts still need a 200 C bake.
DI rinse spec: >=2e6 ohm resistivity (hot 65 C final rinse); SS acid pickle 50% HNO3 + 5% HFSource, quote & tabletop applicability
Mechanical Cleaning; Degreasing or Solvent Cleaning; Detergent Cleaning; Chemical Etch; Electrolytic Polishing; High Pressure Spray; Bake-out
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 497-513
Tabletop: 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.
-
A virtual leak is trapped atmospheric gas bleeding out through a blind path; its gasload decays as 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_Lv = Pa*V/(e*t) (Torr-L/s), Pa = trapped pressure, V = trapped volume (Santeler, NASA SP-105)Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: If a next machine targets below ~5e-7 Torr with elastomers, a double O-ring lid groove pumped by the existing roughing pump (guard at ~15 mTorr) removes the permeation floor for the cost of one extra groove and a hose barb.
-
Set the vacuum requirement so the mean free path is at least an order of magnitude longer than the total spiral flight distance; compute flight distance from dee voltage (e.g. ~300 m for 2 MeV at 1 kV/gap), giving ~2e-3 torr adequate for a fast machine but far better vacuum needed at low dee voltage.
MFP >= 10 * flight path; l = kT/(P*sigma); 2e-3 torr -> ~5 km MFPSource, quote & tabletop applicability
An acceptable vacuum would allow for a mean free path an order of magnitude larger than the expected flight distance.
Tabletop: The quantitative vacuum spec for a next machine: total path length ~ (final energy)/(energy per turn) x orbit circumference; halving dee voltage doubles path length and tightens the pressure requirement proportionally.
-
Vacuum-weld discipline: make seam welds continuous and only on the atmosphere side, and stagger-weld internal bracing, so trapped volumes (virtual leaks) cannot form.
Source, quote & tabletop applicability
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
Tabletop: Standard practice worth enforcing on any welded chamber or fitting on a next machine: no vacuum-side seal welds, no closed pockets.
-
Diagnose breakdown sites by their fingerprints: arcs leave starburst patterns and craters at the initiation point (starbursts cluster at particle sites), so post-mortem inspection of electrodes locates the actual weak spot.
Source, quote & tabletop applicability
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
Tabletop: When a next machine sparks, a loupe inspection for starbursts/craters tells the builder exactly where the field problem is instead of guessing from outside the chamber.
-
Electrode material choice is secondary for HV holdoff - if contaminant particles are present they, not the substrate (Nb, Cu, Au, or their oxides), set the breakdown voltage; oxide layers hundreds of angstroms thick made no measurable difference.
Source, quote & tabletop applicability
if there are contaminant particles, then they, and not the substrate material, determine the breakdown voltage.
Werner, Probing and Modeling Voltage Breakdown in Vacuum — Cornell dissertation (2004) — p. 84
Tabletop: The builder can keep aluminum dees rather than exotic electrodes: cleaning and conditioning matter, native oxide does not.
-
Mild bake-out helps holdoff: cathode sites held 95 MV/m at 100 C with no field emission, but the same sites at room temperature showed field emission from ~40 MV/m and broke down near 90 MV/m - adsorbed gas/water degrades HV performance.
at 100 C: no FE at 95 MV/m; at 22 C: FE onset ~40 MV/m, breakdown ~90 MV/mSource, quote & tabletop applicability
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
Tabletop: A gentle heat-lamp or heater-tape bake of the dee assembly before HV runs should measurably raise the reference machine's sparking threshold.
-
Attain about 1e-5 mm Hg before starting, tolerate no worse than ~1e-3 mm Hg during RF bakeout, and expect cyclotron operation at 1e-4 mm Hg or below with RF and source on.
base ~1e-5 torr; bakeout ceiling ~1e-3 torr; operation <= 1e-4 torrSource, quote & tabletop applicability
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
Tabletop: Directly applicable pressure targets; matches the regime the builder already operates in and sets the next machine's spec.
-
Solvent-wash all tank parts before final assembly to remove organic matter; organics (grease, cutting oil, rubber) are the usual cause of a tank that will not bake out.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable (use modern solvents, not CCl4); degrease every part of a next machine that sees vacuum.
-
Run a short, fat (3 in diameter) pump duct straight down from the chamber to maximize conductance - essential to hold ~1e-7 Torr base while continuously injecting hydrogen for the ion source.
3 in dia straight vertical duct; base ~1e-7 Torr with gas loadSource, quote & tabletop applicability
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
Tabletop: Pumping a gas-fed cyclotron is conductance-limited; a next machine should place the pump under the chamber with the largest, straightest duct possible.
-
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.
Source, quote & tabletop applicability
Steel supporting rods allow thin top and bottom plates to minimize thickness
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 6-7
Tabletop: Every millimeter of lid steel is a millimeter of magnet gap; internal posts (placed outside the beam plane) let the builder close the next machine's gap without a lid that dishes under vacuum.
-
Run new vacuum hardware hot deliberately to degas it: initial operation raises pressure for minutes, after which pressure plunges below the starting point once the electrode surfaces are cleaned.
Source, quote & tabletop applicability
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
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 5-6
Tabletop: Same conditioning applies to the reference machine's chimney and dee surfaces: schedule a beam-on bake-in run and expect pressure excursions before stable operation.
-
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 & tabletop applicability
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
Tabletop: The base-pressure-then-backfill discipline is exactly the reference machine's MFC workflow; a 100:1 ratio of operating to base pressure keeps beam-gas composition dominated by the feed gas.
-
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 & tabletop applicability
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
Tabletop: Matches the reference machine's scale exactly: 1e-6 torr base bled up with hydrogen for the source is the working point of every successful machine in this peer group.
-
Match the chamber to the magnet: a 2.54 cm thick aluminium ring of 9.9 cm outer / 8.5 cm inner radius with 0.65 cm lids, ten KF-16 ports epoxied in at equal angles, and a Viton O-ring groove in the lids gives a workable 2e-6 Torr tabletop chamber.
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 & tabletop applicability
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
Tabletop: A complete, copyable chamber spec for an 8-inch-pole machine, including the epoxy-in-flange trick that avoids welding.
-
Seal large flanges with a continuous square-section rubber gasket in a groove sized so the metal faces land metal-to-metal; the metal contact gives alignment and the gasket cannot be over-crushed.
groove volume >= gasket volume; metal-to-metal closureSource, quote & tabletop applicability
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
Tabletop: Directly applicable to a next machine's chamber lids and faceplates; grooved captive gaskets beat flat sheet gaskets for repeatable sealing and alignment.
-
Backfill and purge with dry air: injecting dry air at the mechanical pump outlet replaces a refrigerated inlet trap, and venting the tank only with dry air markedly shortens the next pumpdown.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable: vent the next machine's chamber with dry nitrogen or desiccated air, never room air, and water-vapor pumpdown time drops dramatically.
-
Do not switch on a hot-filament ionization gauge until pressure is below ~0.5 micron, mount it where conductance to pumps and to tank are comparable so it reads representative pressure, and give its filament some magnetic shielding.
ion gauge on only below ~5e-4 torrSource, quote & tabletop applicability
the ion gauge is not turned on until the tank pressure is less than 0.5 microns ... 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
Tabletop: Directly applicable gauge practice near a stray-field-rich H-frame magnet.
-
Add a Penning (Philips) gauge alongside the ion gauge: it is rugged, works as a pressure interlock, and doubles as a sensitive indicator of hydrogen-flow changes; mount its axis normal to the magnet field it borrows.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable: a cheap Penning head is the right always-on interlock and gas-flow monitor for a next machine, with the ion gauge kept for absolute readings.
-
Benchmark chamber tightness by rate-of-rise: the 280 ft^3 ORNL system held 0.00015 micron/sec with pumps valved off; scale that expectation to your volume.
rate-of-rise spec ~ 1.5e-7 torr/s on 280 ft^3 (leak load ~ 1.2e-3 torr-L/s)Source, quote & tabletop applicability
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
Tabletop: Scale by volume: an equally tight ~30 L chamber on a next machine would show ~4e-5 torr/s; measure rate-of-rise after every re-seal as the standard leak health metric.
-
For vacuum service pick elastomers on three axes - low gas permeability (butyl best, fluorocarbon good, silicone/fluorosilicone worst), low vacuum weight loss, 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; postcure Viton/silicone compounds to drive off volatiles before serviceSource, quote & tabletop applicability
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
Tabletop: Endorses going beyond Parker's 30% on critical static vacuum joints if the groove is widened to take the displaced volume; 'postcuring' is the vendor name for the pre-bake O'Hanlon recommends.
-
In a group of bolts, earlier-tightened bolts relax as later ones compress the joint (elastic interaction, creep of loaded surfaces), which can nearly eliminate their tension - tighten flange bolt circles in a cross pattern and in multiple passes, re-checking the first bolts.
Source, quote & tabletop applicability
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
Tabletop: On the next machine's lid, a single-pass tightening leaves the first-torqued sector under-clamped and is a classic cause of an O-ring leak that 'moves' with each reassembly.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Use dovetail grooves only where the ring must be retained (vertical faces, lids that open); they cost more to machine, need the sharp-corner radius R held closely, and Parker sizes them for less squeeze (16-27%) with metal-to-metal flange contact.
Dovetail: 66 deg walls; W=.139 -> L=.111-.113, G=.113-.117, squeeze 20%, R=.010; radius R is critical - too small damages ring, too large causes extrusionSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: A fabrication trap the builder can skip entirely: o-ring/flat-gasket both lids, weld nothing flat and thin.
-
Stretch a groove-mounted O-ring 1-5% on its ID (2% ideal); more than 5% stretch thins the cross-section, accelerates aging, and loses seal compression.
O-ring ID = groove diameter / (1 + stretch), stretch 0.01-0.05, ideal 0.02; CS reduction ~ f(% stretch)Source, quote & tabletop applicability
This stretch should be between 1%-5% with 2% as the ideal in most applications. A stretch greater than 5% is not recommended.
Apple Rubber Products, Seal Design Guide — p. 11
Tabletop: 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 & tabletop applicability
The maximum volume of the O-ring should never surpass the minimum volume of the gland... the O-ring volume does not exceed 95% of the gland void.
Apple Rubber Products, Seal Design Guide — p. 14-16
Tabletop: Check fill arithmetic including worst-case ring tolerance before machining; Viton heated by RF or magnet proximity expands ~16e-5/C and needs that free volume.
-
Static gland sealing faces tolerate 64-128 RMS but 32 RMS is preferred (16 RMS for vacuum/gas); 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 & tabletop applicability
a finish of 32 micro-inches RMS is preferred... 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
Tabletop: For a rotating or sliding shaft feedthrough (target manipulator), back off to <=30% squeeze and a 16-32 RMS shaft finish, or friction will shred the ring.
-
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 & tabletop applicability
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
Tabletop: Silicone vacuum grease on Viton is fine; silicone grease on a silicone ring (or hydrocarbon grease on Buna-N) slowly destroys it.
-
To run a standard round O-ring in a non-round (rectangular) face-seal groove, keep every inside corner radius at least 3x the O-ring cross-section diameter and match ring centerline length to groove centerline length.
inside corner radius >= 3 * O-ring CS diameter; O-ring ID = (groove CL length / 3.14) - O-ring CSSource, quote & tabletop applicability
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.
Apple Rubber Products, Seal Design Guide — p. 84
Tabletop: 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.
-
Size the deflector with septum radius increment dR ~ 0.15R (0.1R needs less voltage but a long channel; 0.2R risks breakdown), and taper the channel gap from ~1/8 in at entry to ~1/2 in 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 & tabletop applicability
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
Tabletop: Scaled to 160 keV the same geometry needs only ~500-900 V on the deflector - an easy supply; keep the entry slit no wider than the turn separation.
-
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 & tabletop applicability
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
Tabletop: For a next machine's chamber welds specify 304L filler and pipe where possible; carbide precipitation in plain 304 welds is a known source of micro-leak porosity.
-
Verify chamber lid thickness with the fixed-edge circular plate deflection formula (Roark): a 10 cm radius aluminum lid only 3.5 mm thick deflects under 1 mm at full vacuum; use higher-yield 7075-T6 (505 MPa) rather than 6061-T6 (275 MPa) for lids.
delta_center = -q*a^4/(2D)*(L14-L11), D = E*t^3/(12(1-v^2)); 7075-T6 yield 505 MPa vs 6061-T6 275 MPaSource, quote & tabletop applicability
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
Tabletop: Gives the builder the actual formula for trading a next machine's lid thickness against magnet gap - a few mm of 7075 plate suffices at 8-12 inch chamber diameter if the edge is well supported.
-
Everything inside a strong cyclotron field must be magnetically transparent - aluminum, copper, brass - since ferromagnetic parts distort the field and disrupt measurements.
Source, quote & tabletop applicability
all cyclotron components must be made of magnetically transparent materials such as aluminum, copper, or brass
Tabletop: 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.
-
Design for maintenance access from day one: ANL mounted the dee assembly on a rail carriage so the entire dee system rolls out of the chamber for service, and put diffusion pumps on wheels.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
p-B11 disintegration alphas were first detected at ~60-70 keV proton energy (thin film ~70 kV, thick target not appreciable below 60 kV), with yield rising steeply toward 200 kV, and maximum alpha range of 4.7 cm in air; thick-target Li appears 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 & tabletop applicability
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
Tabletop: Proof that p-B11 alphas are observable far below the 675 keV resonance if the builder integrates tens of uA-hours with large solid angle - and that their alphas stop in under 5 cm of air (vacuum path to PIPS required).
-
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 & tabletop applicability
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
Tabletop: At the reference machine's ~1.3 kV dee voltage turn spacing is even smaller, so a bare, grooved copper collector (no thick shield) is essential or the probe reads zero while beam exists.
-
Entry-slit width is set by the turn separation Delta-r/R = V_rf/T (energy gain per turn over total energy); make the septum and deflector radially adjustable because calculated positions are only approximate.
dr/R = (1/2)(dT/T) = V_rf/T per turn (two gap crossings); MIT: dr ~ 0.1 in at extractionSource, quote & tabletop applicability
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
Tabletop: With 2.6 kV/turn on 160 keV, the reference machine's turn spacing at extraction is ~1.6% of R (~1.3 mm at 3.2 in) - build the septum mount with mm-scale radial adjustment.
-
Expect at best ~25 percent of circulating (resonant) beam to survive extraction under optimum tuning, and plan routine operation at less; internal probe targets see several times the extracted current.
extraction efficiency <= ~25% (MIT: 150 uA extracted of ~600 uA circulating; routine 80-100 uA)Source, quote & tabletop applicability
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
Tabletop: Judge a next machine first on internal-probe current at full radius; a 4:1 ratio between internal and extracted beam is historically normal, not a failure.
-
Protect the septum from beam power: slot it on the median plane about one beam-height wide (MIT: two 0.020-in tungsten strips with edges 1/8 in apart, silver-soldered to a curved water-cooled copper bar) so most of the beam passes instead of striking metal.
septum: 0.020-in W strips, median-plane slot ~ beam height (1/8 in at MIT)Source, quote & tabletop applicability
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.
Livingston & Blewett, Particle Accelerators (1962) — p. 184
Tabletop: At the reference machine's microamp/keV beam power the thermal problem vanishes, but the slotted-septum geometry still maximizes transmitted current into the channel.
-
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 - irrelevant below ~1 MeV.
dm/m ~ T/(938 MeV); cyclotron limit ~20 MeVSource, quote & tabletop applicability
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
Tabletop: Reassurance with numbers: at the reference machine's 100 keV-1 MeV scale, relativistic detuning is ~0.01-0.1% and can be ignored in a next machine's design.
-
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 & tabletop applicability
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
Tabletop: Lets the builder compute whether their probe or a future septum can distinguish final turns: at 150 keV, R~9 cm and 5 kV/turn gives dR ~ 3 mm - workable.
-
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 & tabletop applicability
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
Tabletop: The master rate table for the reference machine's PIPS count-rate prediction across their entire 150-675 keV window; it quantifies exactly what reaching the resonance is worth.
-
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)); B=0.976 T, T=0.472 MeV, d=0.291 in -> Vd = 32.5 kVSource, quote & tabletop applicability
Vd = 32.531 kV
Tabletop: Gives the builder the extraction-voltage scale for a next machine: deflector kV requirements scale linearly with beam energy, so a ~100 keV beam needs only ~7 kV in the same geometry.
-
In fixed-frequency magnet scans expect harmonic beam peaks at fields of B/n for odd n - Houghton observed H+/3, H+/5, H+/7, H2+/9 etc. - so label every peak with species and harmonic number before claiming fundamental beam.
resonance at B/n, n odd (ion accelerated on every nth RF cycle)Source, quote & tabletop applicability
H2+/9 H+/7 H+/5 H+/3 H+ H2+
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 15-18
Tabletop: Prevents misidentifying beam in the reference machine's B-field sweeps: a peak at one-third the expected field is the same ion on the 3rd harmonic, not a new species.
-
Fusion rate climbs steeply with grid voltage at roughly constant current: 10 cpm at -16 kV rising to 130 cpm at -31 kV (~13x for a 2x voltage increase) at 13-18 mTorr and ~10 mA, so buy voltage headroom before current headroom.
BF3 moderated counter: 16 kV -> 10 cpm; 25 kV -> 60-100 cpm; 31 kV -> 130 cpmSource, quote & tabletop applicability
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
Tabletop: Same lesson as p-B11 cross-section curves: yield is exponential-ish in particle energy, so for the builder every extra 10% beam energy buys far more counts than 10% more current.
-
Neutron yield in Hull's fusors scaled roughly two orders of magnitude per ~10 kV of drive: 22 kV gave 1e3 n/s, 33 kV gave 1e5 n/s, 45 kV gives >6e5 n/s - invest in voltage, vacuum cleanliness, and gas handling before anything else.
22 kV -> 1e3 n/s; 33 kV -> 1e5 n/s; 45 kV -> 6e5 n/sSource, quote & tabletop applicability
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
Tabletop: Reinforces the energy-over-current rule for the builder: sub-Coulomb-barrier reaction rates reward every extra keV exponentially.
-
Recognize the phase-slip failure signature: once the accumulated phase difference reaches pi/2 the ion gains nothing at the gap and beyond that it loses energy and spirals back inward, so beam current drops abruptly to near zero past a particular radius.
phase difference > pi/2 -> deceleration; beam current collapses beyond that radiusSource, quote & tabletop applicability
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
Tabletop: Diagnostic rule: a sharp cutoff in the radial current profile means phase slip, not wall collisions - which points at field shape/Dee voltage rather than focusing.
-
Identify beam species by sweeping magnet current at fixed RF: resonances appear at B and at B/n for odd n (B/3, B/5), so H+, H2+ and He+ each show up several times in a magnet scan - a cheap mass spectrometer for the internal beam.
f = n f' = n (eB/(2 pi m n)), n odd; e.g. He+ B/3 resonance at 320 mT for 3.68 MHzSource, quote & tabletop applicability
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
Tabletop: Practical commissioning technique: the builder can confirm they are accelerating protons (not H2+ or contaminants) with only a magnet current sweep and an electrometer.
-
The circulating beam is not continuous: ions populate only about 40 degrees of the 360-degree RF cycle, so average current understates peak current by roughly 9x.
bunch width ~40 deg of RF cycleSource, quote & tabletop applicability
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
Tabletop: Sets expectations for pulsed diagnostics and duty-factor arithmetic on any measurement the builder makes with fast instrumentation.
-
Suppress secondary electrons from a current-measuring target by immersing it in a stray magnetic field and insulating it (here with an ebonite sleeve); the microammeter then reads the true ion current.
Source, quote & tabletop applicability
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
Tabletop: The reference machine's Faraday cup inside the cyclotron fringe field gets free secondary-electron suppression; outside the field it needs an explicit suppressor bias or magnet.
-
For alpha counting close to a target, place a thin mica window ~1 cm from the beam spot on a minimal-shadow grid to capture a large solid angle (~0.7 sr), and calibrate absorber stack and dead space against a known polonium alpha source (range 3.80 cm air at 15 C, 760 mm).
window at 1 cm, solid angle ~0.7 sr; Po alpha range reference 3.80 cmSource, quote & tabletop applicability
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
Tabletop: The close-geometry, calibrate-with-a-known-alpha-source method is exactly how the builder should commission their PIPS geometry before hunting p-B11 alphas.
-
Diagnose acceleration radially with an insertable probe on a sliding seal: beam-current vs probe radius, and the width of beam marks on the probe edge, map both resonance quality and the vertical envelope.
Source, quote & tabletop applicability
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
Tabletop: A radial probe (the reference machine's shielded Faraday cup on a linear feedthrough) is the workhorse diagnostic; falling current at some radius localizes where field shape loses the beam.
-
For absolute field calibration use proton NMR: B(gauss) = 234.82 x f(MHz); Hall probes are ~1 percent devices and temperature-sensitive, search-coil fluxmeters are relative instruments.
B(gauss) = (234.82 +/- 0.13) * f(Mc/s); Hall: InAs plate, ~20 mV per kG at 0.2 ASource, quote & tabletop applicability
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
Tabletop: 5.9 kG corresponds to 25.1 MHz proton NMR; the machine's own resonance (f, e/m) also gives the average field to ~0.5%, a free sanity check.
-
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 & tabletop applicability
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
Tabletop: A pulser check separates electronics noise (grounding, RF pickup from the 9 MHz drive) from true detector degradation without risking source contamination.
-
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 & tabletop applicability
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
Tabletop: Slightly better-engineered alternative to the 9 V cup bias; easy to add to the reference machine's beam probe.
-
Find the beam by rocking either RF frequency or magnet current through resonance with the probe pushed in near the center, then withdraw it while re-optimizing arc, filament, and RF on the beam-current reading.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable commissioning procedure; starting the search at small radius relaxes the resonance tolerance enormously.
-
Authenticate a beam by the sharpness of the current peak versus RF tuning and magnet current and by its sensitivity to hydrogen pressure; background (non-orbit) currents are broad and insensitive.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable; a 'beam' that stays constant while you detune B or RF is ion leakage to the probe, not orbiting protons.
-
Give the target probe a high resistance to ground and protect its meter with RF chokes and bypasses; expect a few microamperes on a small machine (the 6-inch gave 7 uA).
6-inch machine: ~7 uA internal beamSource, quote & tabletop applicability
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
Tabletop: Directly comparable scale; microamp-level internal beam is a realistic expectation for a next machine and the choke-protected probe is the right pickup.
-
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 & tabletop applicability
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
Tabletop: Partially applicable: the p-Li gamma resonance needs ~440 keV, above the reference machine's 160 keV; a next machine reaching 0.5 MeV could use exactly this LiF-on-probe gamma check with their gamma detector.
-
Sub-resonance p-B11 measurements were made with only 0.5-10 nA of protons on target (with ~60-70 keV beam energy resolution); nA-scale beams suffice for alpha spectroscopy given ~1e-4 sr detectors and thin targets.
0.5-10 nA on target for Ep = 0.15-0.4 MeV data; 100-200 nA at higher energiesSource, quote & tabletop applicability
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
Tabletop: The single most encouraging number in the batch: professional low-energy p-B11 data were taken at exactly the reference machine's nA beam scale.
-
Report p-B11 yields as total alphas detected per luminosity (counts/(Nt*Np*dOmega)), not as a cross section, because the number of alphas per reaction contributing to the main peak varies with energy (~2.1 at the 675 keV resonance vs ~1.5 at 2.64 MeV).
X = Counts/(Nt*Np*dOmega) [cm2/sr]; multiplicity in dominant peak: ~2.1 (0.675 MeV), ~1.5 (2.64 MeV)Source, quote & tabletop applicability
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
Tabletop: When the builder converts PIPS counts to a 'cross section' they must divide by ~2 alphas per reaction - or better, publish counts-per-luminosity as this paper does.
-
Normalize alpha yields by integrated beam current and calibrate each detector's relative solid angle with low-energy Rutherford scattering on gold plus a known Am-241 alpha source.
solid-angle calibration: Rutherford on Au + 241Am source; yield normalization: integrated charge x dOmegaSource, quote & tabletop applicability
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
Tabletop: The builder already owns the pieces: their Faraday cup/Keithley 617 integrates charge, and an Am-241 check source calibrates PIPS solid angle and energy scale.
-
A simple energy-spread formula from deflector geometry predicts measured spread well: Rutgers predicted dT = 12.7 keV and measured 13.3 keV on a ~0.5 MeV beam using the phosphor-screen spot width.
dT = (V*R^2/d) * (eps_r/(R^2 - eps_r^2)); predicted 12.73 keV vs measured 13.3 keVSource, quote & tabletop applicability
energy at far left: T=.5087 MeV ... dT=13.3 keV ... Theory: dT/2=12.73 keV
Tabletop: Shows a phosphor screen plus this one formula suffices for energy-spread measurement at student-machine scale - no magnetic spectrometer needed.
-
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 & tabletop applicability
The location of the ammeter in the circuit keeps it essentially at ground potential... Do not omit the 10 meg bleeder resistor.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 8
Tabletop: The ground-leg metering trick is how the builder can safely log arc and extraction currents on the next machine without floating instruments at kV.
-
Bias the beam collector (a 9 V battery suffices) to suppress secondary-electron emission; unbiased collectors read falsely high beam current.
+9 V collector biasSource, quote & tabletop applicability
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.
Tabletop: A one-component fix for honest current numbers on any Faraday-cup measurement the builder makes.
-
Bias the internal target/Faraday collector to about +9 V when measuring beam current, otherwise secondary electrons leaving the target corrupt the reading.
+9 V (battery) bias on target vs grounded target comparisonSource, quote & tabletop applicability
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.
Tabletop: One battery fixes a systematic error in the main diagnostic the builder has; also gives a way to separate true beam from secondaries.
-
Accept that beam current falls with target radius and that the honest headline number for a small machine is small: Houghton's best was ~0.1 uA at a B/3 resonance and only 3 pA at the highest proton energy reached, 160 keV at 796 mT and 12.1 MHz.
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 & tabletop applicability
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.
Tabletop: Calibrates expectations exactly at the reference machine's operating point (~160 keV) and names the three things that gate the next factor of 2-3: magnet current, cooling, RF frequency.
-
Take multi-kW beams on grazing-incidence water-cooled targets so the power spreads over a long footprint (86-inch: 41.7 kW on a 6 x 10 inch aluminum grazing target).
grazing incidence spreads P_beam over ~L/sin(theta)Source, quote & tabletop applicability
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
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 24
Tabletop: 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.
-
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 & tabletop applicability
By having only three faces any one face is completely shielded from the material sputtered from that which is in the beam
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 262
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Interlock the PIPS bias supply to chamber vacuum in the beam-diagnostics routine; biasing a humid detector raises leakage and can damage the junction.
-
Clean a PIPS face only by blowing dry gas 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 will not cure leakage or radiation damage.
Source, quote & tabletop applicability
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
Tabletop: The ~500-angstrom implanted window scratches easily; in a chamber with pump oil and target debris this is the only sanctioned cleaning procedure.
-
Use leakage current as the detector health metric: about 10 nA at 20 C is nominal for these diodes, and leakage doubles for roughly every 5 C rise, so temperature-correct before comparing to the certificate.
I_leak(T) ~ I_leak(20C) * 2^((T-20)/5); certificate value 10 nA at 20 CSource, quote & tabletop applicability
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
Tabletop: A detector near warm cyclotron hardware can legitimately read several times 10 nA; only a rise beyond the temperature-corrected value indicates radiation damage or contamination.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Match electronics speed to the detector: thin silicon detectors (10-300 um) deliver their charge in 100 ps to 30 ns, so microsecond-scale shaping integrates the full charge and only noise considerations, not collection time, set the shaping constant.
collection time: Si 10-300 um: 100 ps - 30 ns; thick (cm) Si/Ge: 1-10 usSource, quote & tabletop applicability
(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
Tabletop: The reference machine's PIPS collects alpha charge in nanoseconds; they can choose shaping time purely for noise optimum without worrying about ballistic deficit.
-
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 & tabletop applicability
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
Tabletop: For the builder: mount the preamp on the vacuum feedthrough, not at the far end of a coax run - every pF of cable directly worsens alpha energy resolution.
-
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 & tabletop applicability
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
Tabletop: Confirms the standard PIPS chain for the p-B11 experiment: a charge-sensitive preamp at the feedthrough, never a plain voltage amp on the diode.
-
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), and pick the shaping time that balances the leakage-current term against the capacitance term; 1 electron = 3.6 eV in Si.
Qn^2 = 12*tau*IB + 6e5*tau/RP + 3.6e4*vn^2*C^2/tau [rms e-]; w = 3.6 eV/e-h pair (Si)Source, quote & tabletop applicability
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
Tabletop: Lets the builder compute expected keV-scale resolution of their PIPS chain from datasheet numbers before buying a shaping amplifier, and re-optimize tau if leakage rises.
-
Any particle that can transfer ~20 eV to a silicon atom displaces it; a single 1 MeV neutron transfers 60-70 keV to the recoil and displaces ~1000 atoms, so neutron-producing runs damage silicon detectors far faster than X-rays or electrons (photons below 250 keV cause no displacement at all).
displacement threshold ~20 eV; 1 MeV n -> 60-70 keV recoil -> ~1000 displaced atoms; photon displacement threshold 250 keVSource, quote & tabletop applicability
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
Tabletop: The reference machine's PIPS detectors shrug off the cyclotron's X-ray background but must be shielded or retracted during any neutron-producing (e.g., deuterium) runs.
-
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; the leakage current itself is a reproducible dosimeter.
dI = alpha * Phi * A * d; alpha(1 MeV n) = 2e-17 A/cm, alpha(650 MeV p) = 3e-17 A/cmSource, quote & tabletop applicability
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
Tabletop: The builder can track their PIPS bias current on the Keithley 617 as a built-in damage log: any secular rise flags beam or neutron exposure of the detector.
-
Silicon detector reverse-bias (leakage) current is steeply temperature dependent: cooling from room temperature to 0 C cuts it to about one-sixth, so modest cooling is the cheapest fix for noise from an irradiated or leaky detector.
I(0 C) ~ I(20 C)/6; activation energy ~1.2 eV (irradiated), 1.15 eV (unirradiated)Source, quote & tabletop applicability
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
Tabletop: A Peltier or cold-finger on the PIPS mount is a cheap resolution upgrade if leakage-current shot noise ever dominates the reference machine's alpha spectra.
-
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 & tabletop applicability
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
Tabletop: 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.
-
At the 675 keV resonance the alpha angular distribution is nearly isotropic (|A1|,|A2| a few percent of A0), so PIPS detector angle is uncritical there; significant anisotropy only appears at the 2.64 MeV resonance.
at 0.65 MeV: A0=218.4, A1=-3.2, A2=6.3 mb/sr (isotropic to ~3%)Source, quote & tabletop applicability
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
Tabletop: Frees the builder to place their PIPS detectors wherever geometry and shielding are best - solid angle, not angle, is what matters at their energies.
-
Silicon detectors for p-B11 alphas: place them ~16.5 cm from the target with small solid angles (~2.5e-4 sr each) and thickness sufficient to stop alphas at all energies; expect a large elastically-scattered-proton peak just below 1 MeV alongside the a0 and a1 alpha peaks.
8 detectors at 30-160 deg, r=16.5 cm, dOmega ~2.5e-4 sr each; proton elastic peak < 1 MeVSource, quote & tabletop applicability
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
Tabletop: Warns the builder that their PIPS spectra will be dominated below ~1 MeV by scattered protons - set the alpha discrimination window above that, or use a thin proton-stopping foil.
-
A workable p-B11 target is ~56 ug/cm2 of isotopically pure 11B on a ~9 ug/cm2 carbon backing; calibrate its thickness in situ via Rutherford-normalized elastic scattering and the energy-broadening of the elastic peak (3.6% systematic achieved).
target 56 +/- 2 ug/cm2 11B on 9 ug/cm2 C; thickness via elastic alpha scattering at 165 deg, 4.86 MeVSource, quote & tabletop applicability
the target, which was composed of 56 +/- 2 ug/cm2 of isotopically pure 11B deposited on a 9 ug/cm2 carbon backing
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
Tabletop: Defines 'thin' for the reference machine's boron target (tens of ug/cm2) and gives two independent thickness checks they can perform with their own detectors.
-
Detectable D-D fusion requires at least -15 kV on the cathode even though fusion technically begins near 10 kV; plan supplies for 25-30 kV to get statistically clean neutron counts.
V_threshold(detectable) >= 15 kV; first clean counts here at -25 kVSource, quote & tabletop applicability
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
Tabletop: Calibrates expectations for any sub-threshold nuclear signal at home: being physically above a reaction threshold is not enough; detection thresholds sit well above it.
-
For thermal-neutron activation or moderated counting, a 3.89 cm (about 1.5 inch) layer of HDPE gives the peak thermal capture rate; back the target (e.g., silver) with a second HDPE slab as a reflector.
HDPE moderator thickness ~3.89 cm for peak capture; Ag-108 t1/2 2.37 min activation targetSource, quote & tabletop applicability
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
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 23-24
Tabletop: If the builder ever cross-checks their PIPS counting with activation or a moderated tube (e.g., for D-D work), this fixes the moderator thickness to build.
-
For amateur fusion work choose D-D fuel: it needs no NRC license, is cheap, and branches 50:50 to T+p and 3He+n; D-T requires licensing and tritium handling, and 3He is prohibitively expensive.
D+D -> T + p (50%); D+D -> 3He + n (50%)Source, quote & tabletop applicability
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
Tabletop: The reference machine's aneutronic p-B11 choice sidesteps even this; but if they ever runs deuterium in the cyclotron, D-D is the only license-free fusion fuel.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
Thread lubrication is one of the most effective measures to lessen the potential for galling... Heat contributes significantly to thread galling.
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 8
Tabletop: Every stainless bolt into the stainless chamber flange gets anti-seize (outside the vacuum) or silver/moly plating (inside); one galled lid bolt can strand the whole chamber.
-
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 & tabletop applicability
Pitting primarily in the outline of the electrode - not directly underneath or on top.
Tabletop: When the builder opens the chamber after sparking, the pit geography tells them whether to fix edge radii (perimeter pits) or surface contamination (random pits).
-
Coat HV electrodes with Aerodag G colloidal graphite: it is conductive, has a low secondary-electron-emission coefficient, and suppresses breakdown; also machine away nearby ground planes to widen the gap.
Source, quote & tabletop applicability
We coated the HV electrode with Aerodag G dry lubricant, which is also conductive and has low secondary electron emission coefficient.
Tabletop: A cheap surface treatment the builder can apply to deflector or dee edges if they hit breakdown limits near the top of their voltage range.
-
Any electrode that runs under heavy ion bombardment must be tantalum or tungsten and fusion/resistance welded, not silver-soldered; silver-soldered joints melt within seconds at tens of watts and the electrode stays incandescent long after power-off.
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 & tabletop applicability
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
Tabletop: Applies to the reference machine's chimney slits, puller edges, and beam stops: anything the beam or arc touches for long runs should be refractory metal with welded, not soldered, joints.
-
Provide thread engagement of about one nominal bolt diameter in steel (more in soft materials like aluminum), and always make the nut/tapped material the sacrificial member: choose a nut whose proof load meets or exceeds the bolt's tensile strength.
length of engagement ~ 1.0*d in steel; longer in soft metals; nut proof load >= bolt tensile strengthSource, quote & tabletop applicability
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
Tabletop: Tapped holes in aluminum lids or pole pieces need 1.5-2d of thread or inserts; a stripped hole in the finished chamber is far costlier than a longer bolt.
-
Estimate tightening torque with T = K*d*F, F = 75% of proof load for standard joints (90% for structural); use K ~ 0.20-0.30 dry black, 0.17-0.22 zinc, 0.12-0.16 lubricated - and expect even a perfect torque wrench to scatter preload by 25-30%.
T = K*d*F; F = 0.75*proof load (std) or 0.90 (structural); K: 0.20-0.30 non-plated, 0.17-0.22 zinc, 0.12-0.16 lubed, 0.11-0.15 cadmium; preload scatter +/-25-30%Source, quote & tabletop applicability
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 %.
Fastenal, Technical Reference Guide, Rev. 9 (2005) — p. 25-26
Tabletop: Gives defensible torque numbers for lid bolts and magnet clamp bolts; critically, if a bolt is lubricated but torqued to the dry-K table value, preload can double and snap the bolt.
-
Do not trust torque values on reused fasteners: the first nut thread carries ~35% of the load and yields to fit its bolt, so on reinstallation friction climbs - a Grade 5 pair that needed 70 ft-lb for 9000 lb clamp needed 95 ft-lb on the 2nd use and 145 ft-lb by the 4th; never reuse any fastener that may have yielded.
thread load share: 1st ~35%, 2nd ~25%, 3rd ~18%; same-clamp-load torque drift example: 70 -> 95 -> 145 ft-lb over 4 installationsSource, quote & tabletop applicability
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
Tabletop: Lid bolts cycled dozens of times per year drift far from any torque table; for repeatable magnet-gap or flange clamping, replace nuts periodically or control by turn-of-nut instead of torque.
-
Expect a multi-year build: Iowa State started in 1954 with an undergraduate group and donated industrial materials and got first beam in spring 1957, three years later.
3 years from start to first beamSource, quote & tabletop applicability
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
Tabletop: Schedule reality check for a next machine and for any educational-accelerator product plan.
-
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 total ~ $128,500 (2010 dollars)Source, quote & tabletop applicability
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
Tabletop: Calibrates the next machine's budget: every subsystem the builder does not scrounge or fabricate costs thousands new, so design decisions should follow what surplus actually offers.
-
Buy surplus using a three-line envelope - hard cost cap, minimum performance spec, and required function/condition - then shop the vendor spectrum from sketchy-cheap (Craigslist, eBay, Fair Radio) to legitimate-expensive (Toronto Surplus, Surplus Sales of Nebraska, TestEquity).
Source, quote & tabletop applicability
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
Tabletop: A disciplined method for the next machine's shopping list: define B-field, vacuum, and RF numbers first, then match each to the cheapest vendor tier whose reliability the subsystem can tolerate.
-
Meter homebuilt HV with a ~10,000:1 high-resistance divider string feeding a low-voltage panel meter, add a high-resistance ballast against surges, and immerse the transformer and rectifier diodes in oil.
divider ratio ~1:10,000; X-ray transformer + autotransformer, oil-immersed diodes and cap filterSource, quote & tabletop applicability
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
Tabletop: Directly reusable for the reference machine's dee/extraction HV monitoring; a divider-plus-panel-meter is safer and more trustworthy than reading the supply front panel.
-
A current-limited (neon-sign type, e.g., 12 kV 60 mA) transformer with two HV terminals and case center tap, rectified by microwave-oven diodes, makes a forgiving positive-ground supply; never apply full voltage immediately, and bring voltage up slowly at a few mA.
NST 12 kV / 60 mA + 2x 12 kV MOT diodes, full-wave; positive terminal groundedSource, quote & tabletop applicability
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
Tabletop: A scrounger-grade current-limited HV architecture suitable for the reference machine's source-conditioning and glow-discharge cleaning supplies.
-
Expect and monitor for X-rays once electrode voltages exceed about 18-20 kV; use a Geiger counter at the viewport and a zero-personnel-exposure goal, since fusor/accelerator X-ray output appeared at 18 kV in practice.
X-ray hazard onset ~18-20 kV on electrodesSource, quote & tabletop applicability
At voltages greater than 20 kV, the resulting x-rays can be hazardous.
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 25, 44
Tabletop: The reference machine's dee/extraction voltages are below this, but any HV conditioning or future higher-voltage upgrades cross the 18-20 kV line where viewport X-ray monitoring becomes mandatory.
-
Above roughly 6e5 n/s of D-D output, both light neutron shielding and X-ray shielding become necessary for the operator; below that, distance and time limits suffice.
shielding threshold ~6e5 n/s (D-D, 2.45 MeV neutrons)Source, quote & tabletop applicability
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
Tabletop: Gives the builder a community-vetted numeric line for when a home nuclear device graduates from 'monitored' to 'shielded' - p-B11 alpha work stays far below it.
-
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 & tabletop applicability
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
Tabletop: This is the governing stability rule for the weak-focusing reference machine; the FEMM-derived B(r) should be checked for 0 < n < 1 over every acceleration radius, with n typically a few percent.
-
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 & tabletop applicability
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
Tabletop: In the reference machine Qr = sqrt(1-n) sits just below 1 everywhere, so the key is field symmetry: keep the first-harmonic error (pole tilt, off-center coils) to gauss level or coherent orbit distortion grows every turn.
-
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 & tabletop applicability
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
Tabletop: Very concrete for the reference machine: if the edge-field falloff pushes n through 0.2 near the last turns, the beam blows up vertically into the dee aperture; keep n < ~0.2 until the extraction radius or cross it fast.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Form the average field to within a few gauss to 10-20 gauss of the ideal isochronous curve; for a 30 MeV compact machine a <=5 G deviation holds the beam RF phase within about 5 degrees.
|B_avg - B_iso| <= ~5 G -> |RF phase error| <= ~5 deg; typical achieved tolerance a few to 10-20 GSource, quote & tabletop applicability
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
Tabletop: A concrete shimming target: on a 0.59 T, 8-inch machine, holding the measured field to ~1e-3 of the design curve (a few gauss) keeps phase errors negligible next to the classical-cyclotron phase slip itself.
-
When simulating an existing magnet, expect calculated coil-field contributions to need calibration coefficients of only ~1-2% of the current value to match measurement; agreement at that level validates using measured currents directly in the model.
calibration factor on winding field contribution ~ 1-2%Source, quote & tabletop applicability
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
Tabletop: Sets the expected FEMM-vs-Hall-probe discrepancy for the reference machine's magnet: 1-2% mismatch is normal (unknown B-H curves, geometry error) and should be absorbed by a per-coil scale factor in the builder tool, not chased in the mesh.
-
Compensate the missing flutter at the machine center with a field bump of a few tens to a few hundred gauss above isochronous; the locally decreasing field plus early gap crossings on falling voltage give axial focusing on the first turns.
B_center bump = ~30-300 G above isochronous levelSource, quote & tabletop applicability
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
Tabletop: Directly usable on a next machine: shim a small central cone so B falls gently from center outward, giving vertical focusing where n ~ 0 would otherwise leave the first turns unfocused.
-
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))*(1/Qr^2); precession amplitude x_c = pi*R*(b1/B0)*n_effSource, quote & tabletop applicability
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
Tabletop: 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.
-
Size water-cooled copper main coils for an engineering current density of about 5 A/mm^2 (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 & tabletop applicability
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
Tabletop: Direct sizing rule for a next machine's coil packs: total ampere-turns / 5 A/mm^2 gives the minimum copper cross-section with water cooling; air-cooled magnet wire should be derated well below this.
-
For maximum energy gain per turn, make the dee's RF angular size (geometric angle times harmonic h) equal to 180 degrees or an odd multiple (540, 900, ...); energy gain per turn is dE = 2NqU sin(h*dphi/2).
dE_turn = 2*N*q*U*sin(h*dphi/2); optimal h*dphi = 180 deg (or x3, x5, ...)Source, quote & tabletop applicability
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
Tabletop: 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.
-
A classical cyclotron's final proton energy is capped at 10-15 MeV with one or two dees; 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 & tabletop applicability
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
Tabletop: Directly applicable: at 100 keV-1 MeV the reference machine is far from the ceiling, but deliberately detuning the oscillator slightly low buys extra phase headroom against an imperfect field profile.
-
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 & tabletop applicability
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
Tabletop: Sets the scaling for a next machine: roughly, final energy in a classical machine tracks dee voltage; the reference machine's few-kV dee at ~160 keV is consistent, and ~1 MeV needs proportionally more volts per turn or a flatter field.
-
Design accelerating gaps for a peak surface field no more than 1.3-1.4 times the Kilpatrick limit f(MHz) = 1.64*E^2*exp(-8.5/E) (E in MV/m) for reliable vacuum-gap operation.
f[MHz] = 1.64*E^2*exp(-8.5/E), E in MV/m; run at <= 1.3-1.4 x Kilpatrick ESource, quote & tabletop applicability
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
Tabletop: At the reference machine's few-MHz, few-kV/cm gap fields this gives huge margin, but it is the correct sizing formula if a next machine pushes dee voltage up to tens of kV across small central-region gaps.
-
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 ~ severalSource, quote & tabletop applicability
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.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 52-53
Tabletop: Cheap, high-leverage geometry rule for the reference machine's PIG-style source: chamfer the slit edges ~45 degrees and keep it tall-and-narrow before touching anything else.
-
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 & tabletop applicability
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
Tabletop: If a next machine ever moves to an external source and axial injection, inject at a few kV below the dee amplitude rather than pushing injection energy up for easier transport.
-
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 & tabletop applicability
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
Tabletop: Explains why only ~30% of source output ever accelerates in the reference machine; the builder tool should launch macroparticles over this window rather than a single reference phase.
-
Modern cyclotron vacuum practice achieves ~1e-7 Torr; the vacuum serves both beam survival and voltage holding (higher breakdown threshold for dees, deflectors, inflectors).
P ~ 1e-7 Torr practical target in modern machinesSource, quote & tabletop applicability
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
Tabletop: The reference machine does not need 1e-7, but the dual criterion matters: if the dee sparks before the beam is lost to gas, vacuum improvement should be judged on breakdown margin, not just stripping loss.
-
Estimate residual-gas beam loss step-by-step as dN = sigma*n*N*v*dt with gas density n[m^-3] = 3.3e22 * P[Torr]; use oxygen cross sections for a conservative upper bound when gas composition is unknown.
dN = sigma*n*N*v*dt; n[m^-3] = 3.3e22*P[Torr] (T = 300 K)Source, quote & tabletop applicability
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
Tabletop: Lets the builder tool convert the reference machine's gauge reading and total path length (hundreds of turns) into a survival fraction, quantifying how much beam a ~1e-5 Torr vacuum costs versus 1e-6.
-
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 & tabletop applicability
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
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 56
Tabletop: 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.
-
Space-charge effects in cyclotrons become significant only at beam currents around a few hundred microamperes; below that, single-particle (emittance-dominated) tracking suffices.
I_threshold ~ few 100 uA; check Debye length lambda_D >> beam radius a for emittance-dominated regimeSource, quote & tabletop applicability
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
Tabletop: The reference machine's nA-uA internal beams are 2-4 orders below the threshold: the builder tool can safely omit space-charge solvers entirely, a major simplification.
-
For shielding design, fast-neutron production on complex nuclei is roughly one neutron per 10-15 MeV of proton energy (below 50-60 MeV), permissible human flux is 30-60 n/cm^2/s, and the neutron relaxation length in ordinary concrete is 16 cm (1-2 m walls typical).
~1 neutron per 10-15 MeV proton energy on target; limit 30-60 n/cm^2/s; concrete relaxation length 16 cmSource, quote & tabletop applicability
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
Tabletop: At <=1 MeV protons the reference machine is below most (p,n) thresholds on common metals, so neutron shielding is a non-issue unless the builder targets Li, Be, or deuterated materials - then these numbers set the shielding scale.
-
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 & tabletop applicability
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
Tabletop: The reference machine (155 keV, 2.6 keV/turn, r=9.65 cm) gets only ~0.8 mm/turn; a 10 kV dee at the same radius gives ~3-6 mm.
-
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 & tabletop applicability
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
Tabletop: Small machines fare better because dr scales as dE/E; a 350 keV next machine at 10-20 keV/turn beats this 30 MeV machine's fractional separation by ~50x.
-
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*|nu_r - 1|*xSource, quote & tabletop applicability
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
Tabletop: A deliberate few-mm source off-centering plus letting the beam run into the fringe (n rising to 0.2-0.4) can triple the next machine's turn spacing for free.
-
Size the coherent oscillation to roughly equal the incoherent (emittance) amplitude - larger invites vertical blow-up at nu_r=2*nu_z and nonlinear distortion, smaller wastes separation.
Source, quote & tabletop applicability
In practice, a coherent radial oscillation amplitude of the same size as the incoherent amplitude, is a good criterion for efficient extraction.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 7
Tabletop: If a next machine's radial beam half-width is ~2-3 mm, aim for a ~2-3 mm coherent amplitude, no more.
-
Keep the deliberate radial oscillation to a few mm and cross the nu_r=2*nu_z (Walkinshaw, n=0.2) and nu_z=1/2 resonances in as few turns as possible to preserve vertical stability.
Source, quote & tabletop applicability
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
Tabletop: In a weak-focusing field the last turns sweep n from ~0.1 to ~0.5; keep energy gain high there so n=0.2 is crossed in <~5 turns.
-
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 & tabletop applicability
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
Tabletop: Gauss-level azimuthal field asymmetry matters at 0.59-0.89 T: it is both the knob (deliberate shim/coil bump) and the hazard (uncontrolled bumps de-center the beam).
-
Brute-force first-harmonic extraction needs big bumps: in a 1.7 T field a 1 G bump adds only ~0.2 mm radial gain per turn.
dR/dn(brute force) = 0.5*R*b_N/(N*B0)Source, quote & tabletop applicability
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.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 14
Tabletop: Scaled to 0.6-0.9 T and r~0.1 m, tens of gauss of first harmonic would be needed to force mm-scale separation - precession is far cheaper than brute force.
-
Crossing nu_r=1 with a first harmonic builds coherent amplitude over an effective resonance width of ~10 turns; after crossing, extract where nu_r has fallen to ~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 & tabletop applicability
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
Tabletop: A classical (weak-focusing) machine never has nu_r>1, so create the amplitude by ion-source off-centering instead and use the same nu_r~0.8 fringe region for precession.
-
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 & tabletop applicability
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
Tabletop: At 350 keV a 100 mrad kick over 10 cm of arc needs only ~5.6 kV/cm - about 2.8 kV across a 5 mm gap; at nanoamps the septum needs no cooling (~0.1 mW).
-
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 & tabletop applicability
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
Tabletop: A 3-5 kV, 5-10 kV/cm tabletop deflector sits ~300x below this limit; the practical amateur ceiling is set by feedthrough and edge-radius engineering (the ~26 kV/cm working rule), not bulk breakdown.
-
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 & tabletop applicability
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
Tabletop: Direct amateur precedent: a 1 T / 472 keV university tabletop deflector at 28-32 kV; a next machine needs only ~1/10 the voltage, so generous edge radii make sparking a non-issue.
-
Limit stored energy into deflector arcs: a 30 kV supply plus cable stores ~0.1-0.4 J, enough to pit electrodes - add series resistance at the feedthrough and keep the HV cable short.
E_arc = 0.5*C_cable*V^2Source, quote & tabletop applicability
~0.1 Joules at 30 kV ... ~0.4 Joules at 30 kV ... The bottom plate and deflector electrode - no pitting on the electrode noticed.
Tabletop: Rutgers arced a 30 kV-rated feedthrough run at 35 kV and had to rebuild with the feedthrough inside vacuum plus a corona adapter - rate a next machine's feedthrough 2-3x over operating voltage.
-
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 & tabletop applicability
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
Tabletop: Scaling by 2T: a next machine at 350 keV needs ~1/45 of MIT's voltage for the same geometry ratio - about 1-3 kV across a 3-5 mm entry gap, rising if a faster peel (larger DR) is wanted.
-
Expected efficiency ladder for turn-separated extraction: ~10% for early synchrocyclotron precessional extraction, up to 25% of internal beam for a well-tuned classical cyclotron deflector, 75-80% for IBA self-extraction, >90% only with well-centred beams and modern precessional/acceleration schemes.
Source, quote & tabletop applicability
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
Tabletop: Plan a next machine around 10-25% extraction efficiency; with nA internal beam that is 0.1-0.25 nA external - still a countable, PIXE-usable beam. (Ladder rungs: botman p.2, jongen CYC2004 p.1.)
-
Multi-turn extraction energy spread is ~2*q*Vdee; single-turn extraction requires RF phase width |phi| < sqrt(2/N) (a few degrees for hundreds of turns) and field stability better than dB/B ~ 2e-4.
|phi| < arccos(N/(N+1)) ~ sqrt(2/N)Source, quote & tabletop applicability
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
Tabletop: Do not chase single-turn extraction: accept multi-turn with dE ~ 2*e*Vdee (~20 keV at 10 kV dee), which PIXE tolerates. (Spread and dB/B: botman p.11-14.)
-
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 & tabletop applicability
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
Tabletop: A next machine with R~10 cm and half-gap 1.27 cm allows only ~9 turns (needs ~17 keV/turn); shrinking the half-gap to 6-7 mm at the edge allows ~30 turns - borderline reachable with a 5-10 kV LDMOS dee.
-
H- stripping extraction is 100% efficient with a trivial device (carbon foil 50-200 ug/cm2, lifetime >2e4 uAh) and energy variable by foil radius, at the price of an H- source and stringent vacuum.
dT/T = 2*dr/r sets extracted energy spread from radial beam widthSource, quote & tabletop applicability
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
Tabletop: At sub-MeV a 50 ug/cm2 foil costs ~10 keV of energy and some scattering; every other extraction problem (septum, HV, turn separation) vanishes if an internal-source H- beam and <=1e-6 Torr can be achieved.
-
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 & tabletop applicability
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
Tabletop: A next machine's H- variant spends its whole life at the cross-section peak: ~25 m of path at 1e-6 Torr loses of order 5-10%, at 1e-5 Torr most of the beam - vacuum, not physics, decides this option. (70 MeV data: cyclotron_vacuum_model p.3.)
-
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 & tabletop applicability
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
Tabletop: 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.
-
Precessional extraction preserves beam quality because few turns separate the nu_r=1 amplitude creation from the septum, so HF phase mixing stays small - put the bump (or off-centering) as late as the field allows.
orbit-centre azimuth spread theta = 2*pi*integral (nu_r-1) dnSource, quote & tabletop applicability
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
Tabletop: If a next machine uses source off-centering (amplitude created at turn 1), expect full phase mixing over 30-100 turns: the amplitude survives but its direction smears - a trim bump near the extraction region is cleaner.
-
Verify turn separation before building the deflector: a differential radial probe with ~2 mm finger spacing resolves the turn pattern and the precessional oscillation near extraction.
Source, quote & tabletop applicability
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
Tabletop: The reference machine already probes the internal beam; adding a two-finger (or shadow-bar) differential probe turns the existing radial probe into the diagnostic that decides septum placement.
-
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 & tabletop applicability
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
Tabletop: The reference machine's source will sit at the bottom of the cold-cathode range (tens-hundreds of mA); crossing into the self-heated regime (AMIT saw it at ~250 mA) flips the V-I slope negative, so the arc supply must be a stiff current source in both regimes.
-
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 & tabletop applicability
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
Tabletop: Means ion energy hitting the cathodes ~ full arc voltage (sputtering scales with it), and the chimney (anode) can be grounded to the chamber with the cathodes run negative — one floating supply only.
-
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 & tabletop applicability
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
Tabletop: The reference machine's 0.59 T and a higher-field successor's ~0.9 T are both comfortably above threshold — the PIG will ignite and run without any special field tailoring, and cyclotron field tuning won't detune the arc.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Arc voltage rises as gas flow drops (the arc compensates missing particles), until the discharge goes unstable and extinguishes; the practical gas window for steady operation is set from the high-flow side by pumping and from the low-flow side by arc instability.
dV_arc/d(gas flow) < 0 at constant I_arc; instability at starvation limitSource, quote & tabletop applicability
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
Tabletop: Run current-regulated and watch arc voltage as the health/flow indicator — creeping arc voltage at fixed current means gas starvation (or a worn cathode), long before the arc actually drops out.
-
Cold-cathode arc power is limited to about 1 kW per cathode by the onset of thermal emission; for higher power the source must be pulsed or accept transition to the hot regime.
P_arc,max(cold, dc) ~ 1 kW per cathodeSource, quote & tabletop applicability
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
Tabletop: The reference machine's 50-150 W arc is 10x below this ceiling — pure secondary-emission operation, cathodes stay "cold" (no filament economics), and dc operation is fine.
-
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 & tabletop applicability
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
Tabletop: Cathode buttons are the only consumable: a 3 mm thick disc with a ~3 mm bore anode lasts until ~3 mm of crater. Make them screw-in Ta (hydrogen, low power, may run warm) and stock spares; lifetime is hours-to-hundreds-of-hours depending on arc power, not the tens of hours a bare filament source gives.
-
Wolf Table 5.5 canonical operating data, cold-cathode column: arc 1-5 kV at 1-5 A, ignition 5 kV, duty <=25%, B >= 0.4 T, gas pressure 1-10 Pa in source, 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. Hot-cathode column: 0.3-1.3 kV at 5-10 A dc, ignition 3 kV, B <= 1.2 T, gas 0.2 sccm, <=25 mA, aperture 1 x 25 mm, canal 8 mm, cathode 12 mm, spacing 10 cm.
see rule; gas consumption 0.2-0.6 sccm across all PIG types in the tableSource, quote & tabletop applicability
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
Tabletop: The headline for the reference machine is the gas line — full-size accelerator PIGs run on 0.2-0.6 sccm, a 3-10x reduction from its current 2 sccm open filament feed, because the chimney confines the neutral gas where the ionization is. Dimensions scale down for a 38 mm pole gap (its chimney will be shorter than the 6.5-10 cm cathode spacings listed, which are for big-gap machines).
-
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 & tabletop applicability
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
Tabletop: Plumb the MFC line into the chimney base near a cathode (AMIT feeds through the cathode cavity itself), not into the chamber — this is where the chamber-pressure win over the bare filament comes from.
-
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 & tabletop applicability
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
Tabletop: For the symmetric cold-cathode chimney just strap both cathodes together on one HV feed; a floating anticathode also works if the second feedthrough is awkward, at some cost in control.
-
PIG beam energy spread is 10-50 eV — an order of magnitude worse than a low-voltage filament arc (0.2-5 eV) but irrelevant next to per-turn energy gain in a cyclotron.
dE(PIG) = 10-50 eV; typical currents 5-500 mA classSource, quote & tabletop applicability
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
Tabletop: A 10-50 eV spread against a few-keV first gap is a phase-space nonissue for the reference machine; do not trade source simplicity for energy spread.
-
Cold-start ignition recipe (verified across three independent sources): raise arc voltage to ~3 kV open-circuit and simultaneously boost gas flow (up to ~10 sccm); background ionization starts the discharge within seconds; the supply's current regulator (or a ballast resistor) takes over and voltage falls to the 300-2000 V running band; then throttle gas back to the operating point.
V_ignite ~ 3 kV (Wolf table gives 3-5 kV); V_run = 0.3-2 kV; gas boost then reduceSource, quote & tabletop applicability
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
Tabletop: Corroborated by AMIT (up to -3 kV and 10 sccm, strikes in seconds, sustains <1 kV) and Forringer (3 kV/1 A Glassman in current limit). Spec the arc supply for 3 kV compliance even though running voltage is ~500-1500 V, and automate: gas up -> HV on -> detect V collapse -> gas down.
-
Internal-source extraction: the anode/chimney is grounded and the dee's RF does the extraction via a puller/feeler at 30-100 kV of RF in full-size machines (10-30 kV dc for external sources with anode biased positive).
internal PIG anode at ground; extraction field = dee RF via puller; 30-100 kV RF (big machines)Source, quote & tabletop applicability
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
Tabletop: The reference machine extracts with its few-kV dee — 10x less voltage than any literature machine. Compensate with a small source-puller gap (1.5-2.5 mm, cf. Siemens 2.3 mm, K100 2.9 mm) since extracted current scales ~V^1.5/d^2, and expect proportionally lower beam than published uA figures.
-
PIG cathode maintenance interval in heavy service 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 & tabletop applicability
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
Tabletop: That figure is for 1-15 A heavy-ion arcs; sputter erosion scales down with arc power and hydrogen sputters far less than argon/xenon — the Siemens PET machine (0.27 A, H2) gets 120-300 h. At the reference machine's <=150 mA expect hundreds of hours per cathode set.
-
Fully-dimensioned bench PIG (Rovey): iron cathode body machined from 5.1 cm rod, SmCo magnet (~0.3 T surface field) in an SS sleeve, folded 0.13 mm SS-sheet anode cup, 3.2 mm thick iron faceplate with 6.4 mm axial exit hole — produces a continuous 1 mA H+ beam at 1 mTorr with 5.4 kV / 32.4 W, or 1 mA at 0.4 mTorr and 10.5 W with downstream focusing optics.
1 mA H+ at 5.4 kV, 6.0 mA discharge, 32.4 W, 1 mTorr; ignition <= 1 kV; 100 kOhm/100 W ballastSource, quote & tabletop applicability
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.
Tabletop: Existence proof that mA-class hydrogen PIG output needs only tens of watts and home-shop fabrication (spot-welded sheet anode, epoxied alumina tubes). The axial-extraction geometry differs from a cyclotron chimney but the discharge economics transfer directly.
-
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(beam)/discharge current utilization is ~25% for H2 (21% He); H2 flow-to-pressure in Rovey's small system: 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 & tabletop applicability
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%
Tabletop: The 25% utilization is for axial extraction of the whole column; radial slit extraction runs ~0.1-0.5% (Forringer) because the slit samples a sliver of the plasma. Use the right figure for the right geometry when predicting a next machine's beam.
-
Forringer chimney/slit trade (measured, 40 kV dc puller, 3 sccm H2): 0.25 x 5.0 mm slit gives 52-227 uA protons at 50-450 mA arc (I_beam/I_arc ~ 0.001-0.0005) with radial emittance ~25 mm-mrad independent of current; 0.51 mm slit gives 230-590 uA at only 50-150 mA (~0.004 x I_arc) but emittance grows with current (47->65 mm-mrad). Wider slit = more current per arc-watt, brighter is narrower.
I_beam ~ (1-5)e-3 x I_arc for 0.25-0.5 mm slits at 40 kV extractionSource, quote & tabletop applicability
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
Tabletop: Start a next machine with the 0.5 mm x 5 mm slit: at 50-150 mA arc it made 230-590 uA at 40 kV; even derated ~30x for a 4 kV dee (V^1.5 scaling at fixed gap) that is ~10-20 uA available — four orders of magnitude over the present 3 nA best.
-
Chimney slit machining details that matter: slits chamfered 10 deg, relieved to a 0.010" (0.25 mm) land in a 0.020" (0.5 mm) chimney wall; the K100-style round hole is 0.047" (1.19 mm) dia with a 60 deg chamfer. Slit chimneys emit a beam ~70% of slit height with a flat plasma boundary; hole chimneys emit a diverging beam from a concave boundary and ~50% larger emittance.
slit land 0.25 mm; chamfer 10 deg (slit) / 60 deg (hole); beam height ~ 0.7 x slit heightSource, quote & tabletop applicability
The chamfer in both of the slit chimneys tested was 10 [deg] ... was 0.010" deep (out of a 0.020" thick chimney wall) leaving a 0.010" [land]
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 77, 84, 95-97
Tabletop: These are the actual machining callouts for a chimney a home shop can cut — thin land so the slit doesn't collimate away the beam, chamfer opening outward toward the puller.
-
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"; cathode prep is just 100-grit sanding (early screwdriver-scratching proved unnecessary); water cooling of cathode rod and anode base is essential — copper parts melted without it.
cathode-anode gap 1.9-3.8 mm, non-criticalSource, quote & tabletop applicability
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.
Tabletop: Generous mechanical tolerance — the chimney stack-up doesn't need precision fitting. But take the cooling warning seriously even at 100 W-class arc power; provide a conduction path sized for continuous arc wattage or plumb water.
-
Cold-cathode PIG H+ vs H2+ control (measured): at normal operating points (50-350 mA arc, >=2.0 cc/min H2, arc supply in current limit below 3 kV) the extracted beam showed no detectable H2+; starving the gas to 0.5 cc/min flipped the arc into the 3.5 kV voltage-limited mode (current fell to 90 mA) and H2+ appeared.
H2+ suppressed for flow >= 2 cc/min and arc current-limited; H2+ appears at starved 0.5 cc/minSource, quote & tabletop applicability
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.
Tabletop: Species purity is a tuning knob the reference machine has never had: run the PIG current-regulated at healthy gas flow for a clean proton beam at f = qB/2*pi*m, or starve it deliberately to hunt H2+ on harmonics. Removes the H+/H2+ ambiguity that has dogged the reference machine's run interpretation.
-
This cold-cathode source family operates from 0.5 T (test-stand low-field checks) to 4.5 T (Harper K100) unchanged; it needs base vacuum in the 1e-6 Torr range (gas off) to start consistently, and 2.5 sccm H2 put the test-stand chamber at 4e-5 Torr with 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 & tabletop applicability
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
Tabletop: The reference machine's 0.59 T sits just inside the demonstrated envelope, and its existing turbo + 1e-6-ish base pressure meet the start requirement as-is.
-
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 & tabletop applicability
The minimum gap between the chimney and the puller is 2.9 mm [K100 geometry]
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 78, 85
Tabletop: Gap scales with voltage to hold gradient — at a few kV dee the builder can close the chimney-puller gap to ~1.5-2 mm to recover extraction field, still an easy gradient (<2 kV/mm) against vacuum breakdown limits.
-
For orbit-code initial conditions, model ions leaving a slit chimney from a flat plasma boundary at ~35,000 K plasma temperature (4.5 eV central starting energy); hole chimneys need a concave boundary. This recipe reproduced measured emittance well enough "that construction of actual cyclotrons can proceed".
T_plasma ~ 35,000 K -> E_start ~ 4.5 eV; flat boundary (slit), concave (hole)Source, quote & tabletop applicability
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)
Tabletop: Drop-in starting condition for the reference machine's central-region orbit models — start protons at 4.5 eV from a flat sheet across the slit, not from rest at a point.
-
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 & tabletop applicability
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
Tabletop: 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. Note it makes H-; a positive-ion version at the same point yields substantially more H+ since H- is the minority species.
-
Leave a "cool ring" between the plasma column and the anode wall: widening it from 0.5 to 0.7 mm (collimator 4.0 -> 3.8 mm) gained +6% beam; grooved molybdenum anodes gave +20% beam at -7% arc power; a cesium getter pill in the cathode gave +26% beam at -25% arc power; thoriated-tungsten cathodes were a net loss.
plasma-to-wall gap 0.5-0.7 mm (H- volume production); Mo grooved anode +20%; Cs pill +26%Source, quote & tabletop applicability
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
Tabletop: The cool-ring and Cs tricks are H--specific (volume/surface production of the minority ion); for the reference machine's positive-ion source the transferable lessons are the material one (Mo anode fine, fancy cathode materials not worth it) and that geometry near the slit dominates output.
-
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 & tabletop applicability
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
Tabletop: For a machine starved of axial acceptance a hole source wastes less injected beam, but total current favors the tall slit. The weak-focusing reference machine with a 1.5" gap has generous axial acceptance — use the slit.
-
Cold-cathode PIG V-I regimes (measured, AMIT): below ~250 mA arc the cathodes supply electrons by secondary emission and the impedance is high/positive; above, ion back-bombardment self-heats them into thermionic emission, the V-I slope turns negative and voltage saturates at high current. Arc power vs gas flow passes through a minimum near 4 sccm.
transition secondary->thermionic ~ 250 mA (this geometry); dP/dflow = 0 at ~4 sccmSource, quote & tabletop applicability
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
Tabletop: If the builder keeps the arc <=150-200 mA it stays in the well-behaved positive-impedance regime where a simple current-regulated supply plus modest ballast is unconditionally stable.
-
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 & tabletop applicability
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
Tabletop: Scale to the reference machine's ~100 W arc — cathode heads still run incandescent (they are meant to), so mount them on refractory stems; the chimney body dissipates tens of watts, manageable by a copper stalk conduction path to a water-cooled or finned feedthrough flange.
-
Anode (chimney) bore optimum is 7-8 mm for a hydrogen PIG: 7 mm ID maximized electron/plasma density in simulation, 8 mm gave the highest beam current in the real KIRAMS-13; above ~9 mm secondary- electron production efficiency falls. Cathodes: Ta discs 7 mm dia x 2 mm thick; anode length 20 mm in a ~2 T field.
anode ID 7-8 mm; cathode disc ~7 mm dia x 2 mm TaSource, quote & tabletop applicability
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
Mu et al., Simulation of Electron Behavior in PIG Ion Source for 9 MeV Cyclotron (2015) — p. 3, 5
Tabletop: Direct chimney-bore callout for a next machine — 7-8 mm ID copper or Mo tube, matching Ta cathode discs. At 0.59 T the electron column is fatter than at 2 T, so err toward 8 mm.
-
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 & tabletop applicability
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
Tabletop: 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 of ~ +/-2 deg with sub-degree feel for slit-to-puller aiming — set-and-lock, in-vacuum.
-
A commercial 10 MeV PET-cyclotron power budget allocates 1.5 kW to the internal PIG ion source against 26 kW magnet coil and 14 kW RF; beam after the third accelerating gap is ~197 uA at 190 keV from a 40 kV dee.
P_ion_source ~ 1.5 kW (commercial); ~4% of machine wall powerSource, quote & tabletop applicability
Ion Source Power [kW] 1.5 (Table 1)
Tabletop: Sets the ceiling-class datum; the reference machine's design point (~0.1-0.2 kW) is a deliberate 10x derating of commercial practice, consistent with uA-class rather than 100-uA-class internal beam.
-
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 & tabletop applicability
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
Tabletop: The half-step option — chimney-over-filament keeps the reference machine's existing filament supply and adds gas confinement + defined emission aperture. Worth knowing it exists, but a PIG chimney gets the same geometry benefits and deletes the filament.
-
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 & tabletop applicability
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
Tabletop: General magnet practice, fully transferable - a next machine's pole/yoke/shim geometry can be optimized on a small bolt-together model before buying full-size steel.
-
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 & tabletop applicability
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
Tabletop: General magnet economics, transferable - pick a next machine's coil proportions near the cost/power optimum, then adjust freely for winding or cooling convenience.
-
Shim the pole-face contour so the field falls approximately linearly from the center to ~96.7% of the central value at ~96.5% of the pole radius, corresponding to magnetic index n = 0.2.
n = -(r/H)(dH/dr) = 0.2 at working edge; H(0.965R) = 0.967 H(0)Source, quote & tabletop applicability
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
Tabletop: Directly applicable weak-focusing target - same n=0.2-class profile is the textbook goal for an 8-inch fixed-frequency machine's shim program.
-
Do not count on holding the field up beyond 90-95% of the pole-face radius; the limit is pole cross-section starving just below the face, so thicken the pole there if the field must extend farther.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - budget usable beam radius at ~90% of the 8-inch pole (r_max ~ 3.6") unless the pole is generously sized below the face.
-
Develop shims with a relative field measurement along a radius good to 0.1%; build that measuring capability before starting detailed shim studies.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - a 0.1% relative radial map (differential Hall probe or flip coil) is the entry ticket to meaningful n(r) shimming on the next machine.
-
Expect the poles to deflect toward each other under magnetic load - 0.002 to 0.004 inch even on a model magnet - and measure/budget the gap change between field-off and field-on.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - mil-level gap closure at 0.6 T shifts field and n(r); shim and map the next machine at operating excitation, not cold.
-
High-saturation alloy edge shims (Hiperco) do hold the field to larger radii, but verify dimensional stability before committing - CIT dropped Hiperco after finding it dimensionally unstable.
Source, quote & tabletop applicability
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
Tabletop: Cautionary and transferable - exotic Co-Fe edge rings for the next machine's pole edge need a stability check; plain steel shims are the safe default.
-
Before freezing the design, machine a final pair of model poles from the same steel forgings (same heats) as the full-scale poles and re-verify the shim performance.
Source, quote & tabletop applicability
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
Tabletop: Transferable principle - steel-to-steel permeability variation is real; test a next machine's shim stock from the same material lot as the poles.
-
Hold pole-tip machining to +/-0.0025 inch on essentially all dimensions.
tolerance: +/-0.0025 in on pole tipSource, quote & tabletop applicability
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
Tabletop: Directly applicable - a few-mil pole tolerance is achievable in a good hobby/job shop and is what the field uniformity budget assumes.
-
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 & tabletop applicability
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
Tabletop: Directly applicable craft rule for any welding or brazing done near a next machine's coil insulation or on the coil case.
-
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 & tabletop applicability
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
Tabletop: Directly applicable packaging rule - make the next machine's chamber removable (or serviceable in place) without unbolting pole tips or shims.
-
Support the dee on insulating columns so a DC bias (CIT planned 1000-2000 V) can be superimposed on the RF for discharge control.
dee DC bias 1000-2000 V (NYO-780 summary, p.75)Source, quote & tabletop applicability
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
Tabletop: Directly applicable - a DC-isolated dee mount costs little at design time and gives the multipactor-suppression knob the Berkeley reports show is essential.
-
Perforate pole-tip liners and any large sheet-metal RF liners with numerous holes so the volume behind them is pumped instead of trapping gas.
Source, quote & tabletop applicability
Numerous holes are drilled in them to facilitate vacuum pumping.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 19
Tabletop: Directly applicable - virtual leaks behind liners and skins are a classic small-chamber trap; drill the next machine's liners generously.
-
Helium leak-test every vacuum subassembly individually after manufacture, before installation into the machine.
Source, quote & tabletop applicability
Each assembly was leak-tested with a helium mass spectrograph after manufacture.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 20
Tabletop: Directly applicable - bench-test each next-machine spool, duct, and feedthrough with a helium sniffer (or pressure/soap plus rate-of-rise) before it disappears into the stack.
-
In a well-welded chamber the residual leaks are the gasketed joints, and the specific failure mode is non-uniform gasket thickness - use uniform gasket stock and suspect gaskets before welds.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable leak-hunting prior - on a next machine's chamber, check O-ring/gasket joints first and control gasket thickness uniformity.
-
Benchmark vacuum health by pump-down curve from cold: the 15,000-liter CIT chamber reached 1e-5 mm in 1.75 h and 3e-6 mm in 2.5 h; log your own curve and watch for degradation.
15,000 L system, cold start -> 1e-5 mm in 1.75 h, 3e-6 mm in 2.5 hSource, quote & tabletop applicability
The vacuum reached was 3 x 10-6 mm of mercury. Starting with cool pumps and the system at atmospheric pressure ... 1 hour, 45 minutes to reach 10-5 mm mercury.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 24
Tabletop: Transferable practice - a recorded reference pump-down curve for the next machine's chamber is the cheapest early-warning leak/contamination diagnostic.
-
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 & tabletop applicability
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
Tabletop: Oscillator/transmission-line practice, transferable - lossy coupled loads and mode traps work identically on a fixed-frequency dee resonator driven by an LDMOS chain.
-
Do not trust sub-scale oscillator models for power or tube count: the 3/4-scale CIT model predicted six 880 tubes where the full-scale system needed four; final RF numbers come only from full-scale mockups.
Source, quote & tabletop applicability
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
Tabletop: Transferable caution - stray C, proportions and device parameters do not scale cleanly; validate a next machine's dee voltage vs drive on the real geometry, treating models as guides.
-
Stack removable radiation shielding in two staggered layers so no straight-through cracks remain; magnetite concrete reaches ~200 lb/ft3 with 3000 psi crush strength where density matters.
magnetite concrete ~200 lb/ft3, 3000 psi at 28 days, ~10% waterSource, quote & tabletop applicability
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
Tabletop: Transferable - stagger any shielding blocks on a next machine (concrete, water, borated PE) so seams never line up with the beam plane.
-
Interlock access doors/enclosures so they cannot open unless the oscillator is off or the magnetic field is off its resonance value (no acceleration possible).
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - interlocking RF-enable (and optionally magnet current) to the next machine's enclosure/cave door is a cheap, classic protection scheme.
-
In a mixed copper/aluminum/steel water cooling loop, add a corrosion inhibitor (CIT: 1/3 oz sodium chromate per gallon) because trace dissolved copper attacks aluminum and steel.
1/3 oz sodium chromate per gallon (historic; chromate now restricted)Source, quote & tabletop applicability
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
Tabletop: Directly applicable chemistry for any next machine's water loop touching Cu plus Al; use a modern inhibitor (chromate is toxic/regulated today).
-
Water-cool high-current terminals and fit them with thermal switches that trip the supply before the terminals overheat.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - thermal cutouts on a next machine's coil terminals/lugs (and dee stem cooling) are cheap insurance against a loose-joint meltdown.
-
Guard diffusion/high-vacuum pumps with gauge-controlled automatic valves that isolate the chamber or a failed pump line in under a second (compressed-air actuation, ~50 psi).
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - an interlocked isolation valve (even a spring-loaded solenoid gate) protects a next machine's diff/turbo pump from a chamber let-up.
-
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 & tabletop applicability
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
Tabletop: Directly applicable - the cheap 1948 equivalent of RF finger stock for every removable panel, dee-stem clamp, and line cover on a next machine.
-
Copper-plate every steel surface exposed to RF fields; bare steel halved the system Q in the 184-inch model tests.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - 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.
-
Size dee-to-ground vacuum clearance from RF voltage: the 184-inch used a 3-inch minimum gap for 50 kV RF (~17 kV/inch) at the hot open edge, relaxing to 2 inches near the low-voltage supported end.
~17 kV/inch design clearance at full dee voltage; taper clearance with local voltageSource, quote & tabletop applicability
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.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 10
Tabletop: Directly applicable scaling - at 13 kV the same conservative ~17 kV/inch rule wants ~3/4" dee-to-liner clearance; tighter gaps must lean on the 0.080"/50 kV bench data with derating.
-
Qualify feedthrough/support insulators before installation on a high-Q quarter-wave resonant test line that develops full RF voltage from a small driver under simulated vacuum conditions; air-blast cool insulators under severe RF.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - a bench quarter-wave resonator lets the builder soak-test a next machine's dee-stem insulators at full 5-13 kV RF with only tens of watts of drive.
-
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 (40 kV was the design value), but the discharge-roughened operating unit held only ~30 kV over 0.06 inch.
bench ~50 kV per 0.080 in (copper, polished, 5e-6 mm, 13 Mc); design at ~80%; expect ~60% after conditioningSource, quote & tabletop applicability
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
Tabletop: Directly applicable breakdown data for setting a next machine's dee-to-liner and puller gaps at 5-13 kV - and a warning that discharge-roughened surfaces lose ~40% of bench hold-off.
-
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 & tabletop applicability
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
Tabletop: Directly applicable if the next machine's dee or stem is water-cooled while DC-biased - length of insulating hose plus DI water sets the leakage current.
-
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, all L and C divided by 4, and 2x power for the same voltage.
1/n scale -> f x n, L and C / n (quarter scale measured: power x2, Q x 1/2)Source, quote & tabletop applicability
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
Tabletop: Transferable method - a next machine's resonator can be prototyped at reduced scale with a VNA, remembering effective dee capacitance is not the static capacitance (500 vs 1000 pF on the 184-inch).
-
Expect small dimensional errors in RF models and layouts to accumulate: ~2 inches of cumulative model error shifted the 184-inch frequency band ~1 Mc and forced removal of a whole transmission line; build in adjustment range (movable shorts, extra line sections).
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - give the next machine's resonant line/tank a deliberate tuning range (trombone section, tuning vane, trimmer C) instead of trusting calculated dimensions.
-
Check for a re-entrant cavity mode between the two magnet pole pieces with the vacuum tank walls as the return circuit; if it lands near the operating band, suppress it by strapping the pole pieces together at their outer edges.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - the pole-chamber geometry of an 8-inch machine forms the same parasitic cavity; copper straps pole-to-pole (or liner-to-liner) are a one-hour fix worth doing preemptively.
-
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 & tabletop applicability
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
Tabletop: Directly applicable - the complete 1948 recipe for the RF discharges that plague small chambers at kV-level dee voltages; perforated shields keep pumping speed.
-
Anywhere magnetic field threads an RF gap, a positive dee bias can ignite a Penning (Philips-gauge) discharge; in such geometries the dee bias must be negative.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable - the entire next machine's dee sits in 0.59 T, so if bias is used to kill discharges, start negative; positive bias risks a permanent Penning discharge.
-
Mount brittle ceramic insulators so they carry only pure tension or pure compression, never shear: the 184-inch dee/condenser insulators so mounted gave no trouble in a year despite evident fragility at assembly.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
this shielding was found sufficiently effective, the field being cut from 140 Gauss to less than 20 Gauss.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 20
Tabletop: Transferable - LDMOS amps, fans, and ferrite-cored parts near an 0.59 T magnet want a steel housing; remember the housing itself feels a large attractive force.
-
Calibrate dee-voltage-per-watt expectations from the 37-inch: a grounded-grid oscillator (4x304TL) produced 15 kV peak on the dee at 10 Mc (9 kV at 20 Mc) for 6 kW input at ~70% average efficiency.
15 kV dee at 10 Mc for ~6 kW input, ~70% efficiency (37-inch dee, C ~ 300 pF)Source, quote & tabletop applicability
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
Tabletop: Directly applicable benchmark near the reference machine's 9 MHz - scaled by its much smaller dee capacitance and Q, it frames how many LDMOS kW the 5-13 kV goal really needs.
-
Provide a tuning vane - a movable copper sheet with flexible end connections facing the resonant line's center conductor - to trim the resonant frequency about 6% without rebuilding the line.
vane travel -> ~6% frequency trim of the resonant lineSource, quote & tabletop applicability
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
Tabletop: Directly applicable to a fixed-frequency machine - a vane gives the few-percent trim needed to land the dee resonance exactly on the magnet's cyclotron frequency.
-
Orient demountable RF-housing joints so current flows parallel to the joint wherever possible (such joints need no special contact care), and back copper sheets with sponge rubber where current must cross a joint.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable enclosure craft - plan a next machine's panel seams along the RF current direction and spend the contact-strip effort only on the seams that cross it.
-
Steel in the RF path was tolerable bare at 10 Mc but had to be copper-plated at 20 Mc: heating scales with frequency, so at ~9 MHz either keep steel out of high-current paths or plate it anyway for margin.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable at 9 MHz - bare steel may survive, but plating (or copper construction) is cheap insurance for Q and hot spots.
-
Build low-inductance grid/bypass capacitors as flat metal rings with radiused (1/8 inch) edges over 0.010-inch polystyrene: good for >15 kV DC and ~1500 V RF, but only while the metal stays cool - water-cool the ground side if hot air impinges.
0.010 in polystyrene sandwich -> >15 kV DC, ~1500 V RF when coolSource, quote & tabletop applicability
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
Tabletop: Transferable construction recipe for homemade HV bypass/blocking capacitors in a next machine's RF chain (modern Kapton/PTFE substitutes upgrade the polystyrene).
-
To prevent intermittent (grid-blocking) oscillation in a self-excited oscillator, keep the grid-leak RC time constant below one-tenth of the resonant system's own time constant.
tau_resonant (≈2Q/omega) > 10 x R_grid C_gridSource, quote & tabletop applicability
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
Tabletop: Transferable oscillator rule - the same criterion governs bias-network time constants in any self-excited driver on a next machine's dee resonator (tube or transistor).
-
In loop-coupled oscillators, minimize non-mutual loop inductance (large-diameter tubing, shortest leads) and cancel the residual ~20 degree plate-cathode phase shift with a small series capacitor (~220 pF on the 37-inch), trimmed for minimum plate current.
series C in cathode/filament loop; adjust for minimum DC plate currentSource, quote & tabletop applicability
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.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 9
Tabletop: Transferable to any self-excited or feedback-coupled driver in a next machine - minimum-plate-current (minimum-DC-input) trimming is a meterable, practical phasing procedure.
-
Make sure no secondary resonance of the RF system (plate-loop or housing mode) coincides with a harmonic of the operating frequency; a coincidence at the first harmonic dumped most of the beam and was cured with 15 pF of detuning capacitance.
keep f_parasitic well away from n x f_operating; 15 pF moved 38 -> 34 Mc hereSource, quote & tabletop applicability
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.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 10
Tabletop: Directly applicable even at fixed frequency - sweep the next machine's system for modes near 2x and 3x of 9 MHz and detune any found; harmonic coincidences sap dee voltage and beam.
-
Put a controllable series element (37-inch: an 893 triode with 20 kW dissipation) in the oscillator HV supply lead as an emission/current limiter so tank or condenser discharges cannot destroy the RF power stage.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable principle - fast current limiting/foldback in the LDMOS drain supply (plus VSWR trip) is the modern form of this arc protection.
-
Expect an electron-oscillation (multipactor-type) discharge that exists only below an extinction voltage near 500 V RF and blocks voltage build-up even at 1e-5 mm Hg; quench it with a DC sweeping bias of a few hundred volts on dee, line, and stator.
discharge sustained only below ~500 V RF; any sweeping DC field kills itSource, quote & tabletop applicability
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.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Tabletop: 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 - plan a DC bias supply on the dee from day one.
-
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 & tabletop applicability
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.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Tabletop: 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.
-
If bias alone cannot quench the low-voltage discharge, use a small independent 'tickler' oscillator to drive the dee through the critical low-voltage region until the main self-excited oscillator takes over.
Source, quote & tabletop applicability
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
Tabletop: Transferable start-up trick - with an LDMOS chain this becomes a driven start (external exciter) that rides through the multipactor band before handing over to normal operation.
-
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 & tabletop applicability
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
Tabletop: Conditionally applicable - a bipolar, current-limited bias supply on the next machine's dee lets the builder try both polarities safely and keep whichever helps beam.
-
Characterize your RF circuit cold: measure dee/anode-to-ground capacitance with an impedance bridge using a scope as null detector, and subtract measured lead capacitance (29 pF here) - +/-2 pF accuracy is achievable.
Source, quote & tabletop applicability
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
Tabletop: A modern LCR meter with lead-nulling does the same job on the reference machine's dee stem; knowing C-to-ground before pump-down predicts the ~9 MHz resonance and flags assembly errors.
-
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 found the hottest spots (21 and 13 mR/hr) on the foil-holder edges, not the 18.5 mR/hr foil itself.
Source, quote & tabletop applicability
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
Tabletop: At nA/sub-MeV there is no activation to survey - but the lesson stands: always check holder edges and apertures for beam strike (film, phosphor, or discoloration), since a large fraction of beam can miss the target.
-
If the beam dies short of design radius, first check the n = 0.2 radius: the 184-inch beam vanished at 81.5 in (design 85 in) exactly where magnetic measurements put n = -(R/H)dH/dR = 0.2, vertical oscillations dumping it onto the dee.
n = -(R/H)(dH/dR); vertical blow-up at n = 0.2Source, quote & tabletop applicability
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.
Tabletop: Fully applicable to fixed-frequency machines: map B(r) on the bench, compute n(r), and put the target/septum radius inside the n = 0.2 point; if the reference machine's beam stalls early, this is suspect number one.
-
Measure vertical beam envelope with zero electronics: bombard U-slotted 1/16-in copper targets (slot widths 2.5-4.5 in bracketing the beam) for 1-3 minutes and radioautograph them - beam that spreads vertically tags the slot arms.
Source, quote & tabletop applicability
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.
Tabletop: Copy the C-target geometry but read it with phosphor screen or dental X-ray film instead of activation; a set of slotted witness targets at different radii gives the whole vertical envelope in a few runs.
-
Multiple 'pips' per beam pulse on one probe are precession, not source noise: a second probe 155 degrees away showed the same structure with the expected phase shift, and current simply transferred between probes as the inner one moved from 28.25 to 27.56 in.
Source, quote & tabletop applicability
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.
Yeater, 184″ Cyclotron: Synchroscope Beam Pictures on Two Probes — MDDC-987 (1947) — p. 3
Tabletop: The FM pulse envelope is synchro-specific, but the two-azimuth probe comparison transfers: any structure that keeps a fixed phase relation between azimuths is orbit dynamics; anything common-mode is source or RF fluctuation.
-
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 & tabletop applicability
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
Tabletop: Exactly the right probe pattern for the reference machine's chamber: an O-ring/Wilson-sealed sliding shaft with grounded shield tube; unshielded probes near a 9 MHz dee read RF pickup, not beam.
-
For first detection of a weak deflected beam, photographic film on the probe beats an ion chamber: compare exposures with deflector on and off; Berkeley's ion-chamber 'detection' could not be reproduced but film showed the displacement.
Source, quote & tabletop applicability
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
Tabletop: A next machine's extraction commissioning should start with on/off comparison images (film, phosphor, or CCD) at the channel exit; integrating detectors see sub-nA deflected beams that electrometers lose in RF noise.
-
Do not build a deflector septum from 0.002-inch unsupported copper foil: sparking between the HV electrode and septum locally heated and badly warped it in one run - size the septum to survive spark heating, not just beam heating.
Source, quote & tabletop applicability
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
Tabletop: A next machine's septum should be thicker (>= 0.010 in), tensioned, or heat-sunk at both edges; conditioning sparks are inevitable and each one dumps its energy into the nearest thin edge.
-
An in-tank DC electrostatic deflector electrode held about 60 kV (fed through a 20 Mohm resistor) in the operating 184-inch cyclotron - a realistic ceiling for deflector voltage amid magnetic field, RF, and beam.
Source, quote & tabletop applicability
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
Tabletop: A next machine needs only a few kV/cm over a few cm of channel - an order of magnitude below what 1947 in-tank hardware sustained, so deflector voltage should not be the limiting risk; the series resistor for spark current limiting is worth copying.
-
Do not fight the n = 0.2 resonance for the last few percent: Berkeley abandoned accelerating past 82 in because the energy there was already within 5% of the machine's n = 1 maximum at 85 in.
E_max at radius where n = 1; usable beam ends near n = 0.2Source, quote & tabletop applicability
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
Tabletop: Budget a next machine's energy at the n = 0.2 radius, not the pole edge; shaving the pole-edge shims to push n = 0.2 outward buys more usable energy than chasing radius into the fringe.
-
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; A_z up to 2*A_rSource, quote & tabletop applicability
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.
Tabletop: The reference machine's few-kV dee means thousands of turns - the explicit worst case named here; keep dee aperture at least twice the expected radial oscillation amplitude and keep n < 0.2 over the whole usable radius.
-
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 & tabletop applicability
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.
Tabletop: No activation at tabletop energies - instead line the dee aperture with removable witness strips (paper, phosphor, anodized Al) and read burn/discoloration marks to find the loss radius; the localization logic is identical.
-
Probe-current fine structure is quantitative: the minor-pulse frequency equals the orbit-center precession frequency omega_prec = (1 - sqrt(1-n))*omega_0, so counting pips at a known probe radius measures n there.
omega_prec = (1 - sqrt(1-n))*omega_0Source, quote & tabletop applicability
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
Tabletop: 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 mode run makes precession directly visible on a scope.
-
Every working small classical cyclotron in the 1958 census ran 12.5-18.5 kG center field (ISSP 16-in: 14-19 kG; 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; iron near saturation is the cheapest energy.
K_p[MeV] ~ 48.2*(B[T]*r[m])^2; K_d ~ 24.1*(B*r)^2Source, quote & tabletop applicability
Mag. field, k-gauss 14 - 19
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Tabletop: The reference machine's 0.59 T is a factor 2-3 below the entire historical population; pushing a next machine's magnet toward 1.2-1.5 T multiplies energy 4-6x at fixed pole radius and is how every real small machine reached MeV.
-
Dee-to-dee voltage in the census scales with energy: 1-4 MeV machines used 18-30 kV (ISSP 16-in ran 10-18 kV and still held 100 uA internal; Stanford 27-in: 20 kV; Tokyo 25-in: 27 kV), while 7-11 MeV machines needed 40-90 kV.
Source, quote & tabletop applicability
Dee-to-dee, kv 10 - 18 ... Internal Beam, Stable, ua 100
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Tabletop: Proof that low dee voltage works at small radius: the 16-inch ISSP machine is the existence proof for a next machine's sub-MeV goal with a ~10 kV-class dee, provided the field profile keeps the many extra turns focused.
-
Oscillator budgets for 16-31 in machines were 10-50 kW, dominated by self-excited single-tube grounded-grid 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 & tabletop applicability
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
Tabletop: These kilowatts bought 20-90 kV dees at high Q, not beam power; a few-kV tabletop dee needs only ~100 W-1 kW, and the census shows simple self-excited oscillators (no synthesizer, no feedback loop) ran every one of these machines.
-
Magnet iron grows roughly with the cube of pole diameter across the census: 16-in -> 6 tons Fe, 18-in -> 6, 27-in -> 10, 28-in -> 17, 31-in -> 31, 90-cm-pole Copenhagen -> 35, 54-in-core Washington -> 70; copper or aluminum windings add 1-12 tons.
Fe tonnage ~ D^3 (very roughly (D[in]/9)^3 at the small end)Source, quote & tabletop applicability
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
Tabletop: Extrapolating down, an 8-in-pole machine wants ~0.5-1 ton of iron - hobby-crane scale; it also warns that every inch of extra pole diameter on a next machine is bought with steeply growing steel.
-
Census geometry template: pole gap 12-18% of pole diameter (2 in on 16-in, 3 in on 18-in, 5.5 in on 31-in), dee aperture 40-60% of gap, dee diameter 85-95% of pole diameter, and maximum beam radius 80-90% of pole radius.
Source, quote & tabletop applicability
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
Tabletop: Sanity template for a next machine on 8-in poles: expect ~1.0-1.4 in gap, ~0.5-0.8 in dee aperture, and plan energy at a 3.2-3.6 in beam radius, not at the pole edge.
-
Shim for only 2-4% total field drop-off from center to maximum beam radius - the census machines cluster tightly there (Copenhagen 1.75%, ANU 2%, ISSP 2.5%, BNL 3%, Tokyo 25-in 3%, Rochester 3-4%): enough for axial focusing without reaching n = 0.2 early.
total dB/B (center to r_max) ~ 0.02-0.04Source, quote & tabletop applicability
Field drop-off 3-4 %
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 164
Tabletop: Directly transferable target for shimming the reference machine's 0.59 T field: a measured 2-4% drop across the usable radius, smooth and monotonic, is what the entire fixed-frequency population converged on.
-
Internal beams of 100-3000 uA were routine on even the smallest census machines (ISSP 16-in: 100 uA d at 10-18 kV dee; BNL 18-in: 1-2 mA p; ANU 31-in: 3 mA), but extraction delivered only ~1-40% of that (Copenhagen 2%, ANU 8%, BNL up to 40%).
Source, quote & tabletop applicability
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
Tabletop: 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 even good 1950s machines lost most of the beam at extraction, so budget a next machine's external current pessimistically.
-
Hooded low-voltage arc ion sources with hot filaments were universal on census small machines (ANU: hooded arc, tungsten filament; BNL: hot cathode in copper arc house; Stanford: hooded arc; ISSP: hooded low-voltage) - no small machine ran a cold-cathode source.
Source, quote & tabletop applicability
Ion source, type hooded arc, tungsten filament
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 26
Tabletop: Strong population-level evidence for upgrading a next machine from cold-cathode PIG to a hooded filament arc; that single change is what separated 100 uA-class machines from starved ones.
-
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 & tabletop applicability
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
Tabletop: The cheapest extraction upgrade known: mechanical slits in the center region plus tight dee-amplitude regulation; for a next machine's turn-separation budget, orbit-center definition on turns 1-3 matters more than deflector finesse.
-
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 & tabletop applicability
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
Tabletop: First-turn loss at low dee voltage is a classic tabletop failure mode; a fine grid (or slit plate) on the dummy-dee aperture is a proven 1950s fix that costs an afternoon to try.
-
A variable-energy small cyclotron needs no re-shimming if the poles are shaped for a self-similar profile: ISSP varied 14-19 kG by coil current alone, keeping 1-2.5% drop-off at the 16-cm exit radius, with a variable-frequency self-excited oscillator (11-14 Mc/s d, 22-28 p).
Source, quote & tabletop applicability
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
Tabletop: The builder can trim B to match a fixed RF (or vice versa) and expect the shim profile to survive, as long as the iron is not driven into locally different saturation - measure n(r) at both ends of the intended current range.
-
Air-cooled magnet windings sufficed on small machines: Stanford's 27-in (12.5 kG, 10 t Fe) and Howard's 16-in (15-16 kG) both ran air-cooled coils; water cooling only became universal above ~30-in poles.
Source, quote & tabletop applicability
Air-cooled coils. Iron ore blocks for shielding
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 127
Tabletop: Supports keeping a next machine's coils air-cooled with duty-cycle management instead of plumbing water - two real machines at 12.5-16 kG did exactly that.
-
Whole working cyclotrons were built for $5k-$110k and about two years: Stanford 27-in cost $5000 plus $5000 improvements (1940 to first beam July 1941); ISSP 16-in cost $40k with first beam 26 months after construction start; BNL 18-in cost $110k.
Source, quote & tabletop applicability
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
Tabletop: Scope calibration: a garage-adjacent team building a 2-4 MeV, 16-27 in machine was normal in this era; a next machine at 0.3-1 MeV on 8-in-class iron is historically a modest, well-precedented project.
-
Make PA protection automatic and operator-proof: feed the dee-voltage modulator from a linear "or" gate of the dee voltmeter and per-tube cathode-current-limiting amplifiers, so whichever signal is highest takes control and mistuning cannot damage the power tubes.
control = max(dee-voltage error, PA cathode-current limit, driver cathode-current limit)Source, quote & tabletop applicability
As a result of these circuits improper tuning cannot damage the power tubes.
Tabletop: Directly transferable to the LDMOS upgrade in solid-state form - an ALC loop whose setpoint is overridden by drain-current/SWR limiters protects a 100-500 W pallet from mistuned-dee experiments exactly as it protected 50 kW tubes from inexperienced operators.
-
Let the current-limit reference track the RF plate (output) voltage so dissipation, not current, is held constant - then the amplifier is protected when the dee circuit is tuned off resonance yet full power is available when properly tuned.
I_limit proportional to V_rf so that P_diss = const (fixed reference acceptable only at conservative power levels)Source, quote & tabletop applicability
to let the reference voltage vary with the rf plate voltage so that plate dissipation would be limited to a constant value
Tabletop: The exact analogue for LDMOS is limiting device dissipation (drain current x voltage headroom) rather than a fixed current clamp, which either under-protects off-resonance or throttles available power on-resonance.
-
Pulse or modulate the beam electronically through the dee-voltage control loop rather than the source: a small current injected into 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 & tabletop applicability
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
Tabletop: A tabletop ALC loop gets beam pulsing for activation or timing experiments for free - inject an offset into the amplitude setpoint; no mechanical or source-side hardware needed. The 1%/10 uA constant is specific to their circuit, not a scaling law.
-
Interlock any automatic dee-tuning servo to engage only above an amplitude threshold, because phase detectors misbehave at low drive and the servo can run away in the wrong direction (their flip-flop detector stuck in one state below 15 kV; servo enabled at 20 kV).
servo enable at V_dee >= 20 kV on an 80 kV system (i.e. ~25% of full amplitude)Source, quote & tabletop applicability
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
Tabletop: Any auto-tune loop on a next machine (phase comparison of PA drive vs dee pickup) needs the same amplitude gate plus a manual jog mode to walk the tuner into range before handing over - the failure mode is detector-technology-independent.
-
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 (first-cut: full drive with plate/screen supplies off, null RF on the plate).
Source, quote & tabletop applicability
adjusting Cn for coincidence of maximum dee voltage and minimum plate current as the dee was tuned through resonance
Tabletop: Neutralization per se is a triode/tetrode issue, but the acceptance test transfers - on any amplifier-dee chain, dee-voltage peak and PA input-current dip should line up when sweeping through resonance; a skew flags feedback or coupling problems.
-
Keep DC supply voltage off any RF conductor that runs through the magnetic field in vacuum: a DC-biased line in the field sustains a Phillips-ion-gauge-type (PIG) discharge whose electrons migrate along the line and destroy the RF vacuum window; block the DC with a series capacitor instead.
Source, quote & tabletop applicability
a Phillips-Ion-Gauge-type discharge can start in the magnetic field inside the vacuum tank near the positive transmission line
Tabletop: 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 ion gauge and PIG source work), so any DC-carrying feedline, bias lead, or probe wire inside the field must be RF/DC separated; they melted an electron trap and a ceramic window learning this.
-
For sliding RF contacts, use heavy contact fingers (0.020-inch Eimac grid collet, twice normal finger-stock thickness) clamped by water-cooled copper blocks against a silver-plated water-cooled stem: this ran three years flawlessly at 110 A/in rms routine current density.
proven >=110 A/in (rms) contact current density; 0.020 in fingers vs 0.010 in standardSource, quote & tabletop applicability
no discoloration or other indication of heating of the contacts, despite routine operation to 110 A/in and occasional operation to higher current densities
Tabletop: A tabletop coaxial resonator tuning short carries far less current, so 110 A/in is a generous ceiling - but the recipe (thick fingers, positive clamping, plated surfaces, cooling on both sides of the joint) is the proven pattern for any movable-short tuner.
-
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 & tabletop applicability
vacuum capacitors have been used in various ways in its plate circuit. None has been found to stand up satisfactorily.
Tabletop: Dated in absolute terms - modern vacuum caps are far better and fine at a next machine's kW-class levels - but the underlying point stands; put lumped variable capacitors where RF current is low and do coarse tuning with distributed elements.
-
Squaring the dee waveform by adding a 1/3-amplitude third harmonic attacks the main beam-loss mechanism of a weak-focusing cyclotron: it reduces the axial electric defocusing force and even makes the residual force focusing during the early 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 & tabletop applicability
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
Tabletop: The reference machine's beam losses in the first turns are exactly this mechanism at nA scale; a flat-topped dee is likely too much RF plumbing for a next machine, but the rule explains why phase excursion and gap-crossing timing dominate small-machine transmission.
-
Adding the third harmonic does not spoil central ion bunching - ions still bunch to cross the gap near the peak of the fundamental, so flat-topping raises the average accelerating voltage seen during the phase excursion without losing the automatic phase grouping.
dominant term -w*t*sin(wt+theta) unchanged by third harmonic (Appendix I)Source, quote & tabletop applicability
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
Tabletop: Reassurance that waveform shaping and center-region bunching are separable problems; also a reminder that the bunching mechanism itself (Cohen) is what sets which ions survive the reference machine's center region. OCR note - theta prints as (c) in these appendix equations.
-
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 * (1/2 C V^2) * f = C V^2 f; 1e-10 F * (1e5 V)^2 * 1e7 Hz = 20 MWSource, quote & tabletop applicability
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
Tabletop: 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.
-
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; b13 = (3cot(a1) - cot(3a1))/(3cot(a2) - cot(3a2)); a1 < pi/3 < a2Source, quote & tabletop applicability
The extra current element can, however, be a second transmission line
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 18
Tabletop: 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.
-
Tune a dual-resonance system iteratively, one frequency at a time: null the input admittance at the fundamental with one stub, measure at the third harmonic, then trade length between the two stubs (keeping the fundamental nulled) until both frequencies null.
Source, quote & tabletop applicability
Tune the length of one of the lines for a null on the admittance meter.
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 21
Tabletop: The written five-step procedure is a model for documenting any coupled- adjustment RF tune-up (a next machine's coupling loop + trimmer interact the same way); interpolating from precomputed tables to know which way to tune is the transferable trick.
-
A single quarter-wave coupling line can feed both the fundamental and third harmonic to the resonator, because a 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 & tabletop applicability
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
Tabletop: Handy odd-harmonic identity for any coax-fed system - it also warns that a quarter-wave feeder presents transformed impedances to your amplifier's harmonics, which matters for LDMOS stability even in a plain sine-wave system.
-
Prefer a master-oscillator power-amplifier chain (oscillator + frequency tripler, separately controlled amplitudes/phases) over a self-excited oscillator for multi-frequency drive - a single self-excited diode-clipping driver worked at 4.77 Mc/s but harmonic amplitude and phase were interdependent and hard to adjust.
Source, quote & tabletop applicability
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
Tabletop: Mirrors the next machine's decision already leaning MOPA - independent control of each degree of freedom beats a self-excited loop whenever more than amplitude must be set, and a DDS + LDMOS chain is the modern MOPA.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Ion bunching by the RF displaces orbit centers by Delta-r = 2D sin(theta), equivalent in the ORNL Analogue I example to ~20 turns, ~2 kV, or ~1% energy spread at the exit radius: keep it small if a monoenergetic extracted beam matters, or remove the need by AVF/flat-topping.
Delta-r = 2*D*sin(theta), D = eV/(2*m*omega^2*d) characteristic bunching displacementSource, quote & tabletop applicability
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
Tabletop: Sets the physics floor on energy spread from central bunching for any future extraction work; at the reference machine's and a next machine's energies the effect is small in absolute mm but the ~1%-class energy-spread scale is exactly what a deflector/slit design must budget for.
-
Size a dee tuning servo to these proven numbers: loop gain such that 1 degree of phase error applies full power to the servo motor, slew rate such that the trimmer moves the dee resonant frequency 1% per minute, and total trimmer range of 2% in frequency.
full drive at 1 deg error; slew 1%/min of f_res; range 2% of f_resSource, quote & tabletop applicability
The loop gain should be such that one degree of phase error will apply full power to the servo motor.
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 7
Tabletop: Stated as easily-achieved perfect-performance values, not minima - a stepper-driven trimmer on a next machine's resonator can copy all three numbers directly; 2% range comfortably covers thermal drift on a machine holding ~5 G field tolerance.
-
Build the tuning-loop phase detector to null exactly at the desired phase with high, known sensitivity - theirs produced 0.76 V per degree of phase error around the 120-degree null, with sign indicating direction.
K_d = 0.76 V/deg at the nullSource, quote & tabletop applicability
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
Tabletop: A modern phase detector IC gives ~10-20 mV/deg, so their 0.76 V/deg shows how much detector gain a robust motor loop wants - budget amplification accordingly, and characterize K_d so loop gain is a number, not a knob.
-
Make the control loop's gain independent of machine operating level: heterodyne the dee pickups in a converter whose IF amplitude equals the local-oscillator level (not the RF level), and include an antinoise circuit to extract phase from arc-source and dee-vibration noise.
Source, quote & tabletop applicability
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
Tabletop: The same requirement is met today by limiting amplifiers or digital phase detection - the principle (servo dynamics must not change between 10% and 100% dee voltage, and the source arc is an in-band noise generator) applies verbatim to a next machine's tuning loop.
-
In any multi-electrode resonant system, unneutralized inter-electrode capacitance couples the control loops and makes servo stability unattainable - power flows dee-to-dee through the high-Q resonator, and shielding skirts and time-constant tweaks do not fix it; neutralize with transmission lines between the stems.
dee-dee neutralizing line load condition Vn = Va*w*CDD*Zo*sin(beta*l)Source, quote & tabletop applicability
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
Tabletop: Confirmed independently on the machine side in ucrl-3187 p.5,11 (dees could not be servoed individually until neutralized). A single-dee next machine dodges this entirely - which is itself the design lesson - but it governs any future two-dee or dee+dummy-dee variant with separate tuners.
-
Verify neutralization by exciting one electrode at a time and measuring the voltage induced on the others (neutralizing coefficient e_j/e_i, achieved below 3%), and do the adjustment with the machine vented to air: at low pressure the test drive multipactors.
N_ij = e_j/e_i < 3% achievedSource, quote & tabletop applicability
It was necessary to do this while the machine was down to air, in order to avoid multipactoring.
Smith, A Three-Phase Radiofrequency System for Cloverleaf Cyclotrons — UCRL-3153 (1955) — p. 18
Tabletop: Two transferable habits - quantify RF isolation as a measured coefficient with a pass number, and remember that low-level RF tests in vacuum sit exactly in multipactor territory (the reference machine has seen multipactor-like loading); atmospheric-pressure RF checks avoid it.
-
A 45-degree transmission line makes a constant-amplitude phase shifter: its input-impedance magnitude is independent of the terminating resistance, so driving it from a constant-current source and servo-varying a load pot (250-ohm, ~7 ft of RG-58 at 11.2 Mc) 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 & tabletop applicability
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
Tabletop: A DDS sets phase digitally today, but the lambda/8 trick remains a zero-active-parts phase adjuster for RF plumbing (e.g. trimming a pickup or reference arm) and a nice classroom demonstration of transmission-line properties for the educational-machine line.
-
Decompose a coupled multi-resonator RF system into independent single-phase subsystems before trying to control it: once the dees were electrically isolated by neutralization, the three-dee machine behaved as three separate single-phase systems, each with its own small amplifier and servo.
Source, quote & tabletop applicability
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
Tabletop: The architectural moral - decouple first, then control each loop as SISO - applies to any interacting set of tabletop loops (tuner vs coupling vs amplitude on a next machine); trying to servo a coupled system is how the programme burned months (ucrl-3187 p.5-6,11).
-
Move the ion source off-center and inject azimuthally into a dee: replacing a central open arc (3.2 mA protons at 8 in, severe dee-tip heating) with a hooded-arc source at ~1-3/4-in radius with a 1/8 x 3/4-in exit slot roughly doubled the beam to 6-7 mA and eliminated the dee-tip heating.
source radius ~1.75 in on a 20-in machine (~0.2 of pole radius); slot 1/8 x 3/4 inSource, quote & tabletop applicability
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
Tabletop: The geometry lesson is scale-free even though these are milliamperes of internal beam - a doubled capture fraction and cooler dee tips from source position/orientation alone; for the reference machine's filament source, radial position and slot azimuth are cheap, high-leverage experiment variables (directly relevant to a planned source-species test).
-
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 & tabletop applicability
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
Tabletop: At the reference machine's nA scale calorimetry is unavailable, but the doctrine - never trust one beam-current method, and expect tens-of-percent disagreement between independent methods - is exactly the Faraday-cup vs electrometer-background cross-check discipline already used; OCR note - the 75% figure was verified on the page image.
-
Use a positive probe bias (+450 V here) as a purity test on beam-current readings: at full radius the reading was bias-independent (true fast-ion current), but inside 6 inches the unshielded-probe current rose steeply and was reduced by bias, flagging low-energy/secondary contamination near the center.
reading valid where dI/dV_bias ~ 0; +450 V test biasSource, quote & tabletop applicability
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
Tabletop: Directly usable on the reference machine's Faraday cup/probe - sweep a modest positive bias and accept the current only where it is bias-flat; near the source, gas ions and secondaries can dominate an unshielded collector by large factors. Scale the bias to the machine (tens of volts suffices for nA beams).
-
Beam current should scale linearly with peak dee voltage (and with DC amplifier power) once running, and beam loading is a free diagnostic: turning the source on raised final- amplifier plate currents two- to threefold over the source-off condition.
I_beam approximately linear in V_dee; plate current 2-3x source-off under full beam loadSource, quote & tabletop applicability
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
Tabletop: The linear beam-vs-dee-voltage check transfers to nA scale and is a good run-log plot for the reference machine; the 2-3x loading signature does NOT - milliampere beams absorb real RF power, whereas a nA beam is invisible in amplifier current, so use it only as an upper-bound sanity argument.
-
Protect the RF finals in layers: interlocked cooling, spark gaps at both ends of the transmission lines to the dee stems, and an rf-dc fault circuit that compares RF output with DC plate voltage and removes excitation whenever RF fails to build up or drops out.
fault = (V_dc present) AND (V_rf below threshold) -> remove excitationSource, quote & tabletop applicability
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
Tabletop: The rf-dc comparison is the tube-era ancestor of modern SWR/output-detect foldback and ports directly to the LDMOS upgrade (DC applied but no RF developing = arc or detune, kill drive); spark gaps at the feedthrough remain cheap insurance at 5-13 kV dee voltage.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Expect thermal detuning plus ion lock after shutting down from high-power running: the machine would not re-excite ("ion lock"), and had to be retuned by grid-dip-oscillator measurement of each resonator; plan a low-level resonance-check capability into the system.
Source, quote & tabletop applicability
thermal effects detuned the machine sufficiently so that ion lock prevented the rf from being restored
Heusinkveld et al., Studies with a Three-Dee Three-Phase Proton Cyclotron — UCRL-3187 (1955) — p. 12
Tabletop: The reference machine already shows warm-up drift; the transferable practice is a permanent low-level sweep capability (VNA or dip meter on a pickup loop) so resonance can be found cold without RF power, plus logging tune position vs temperature - cheap now, standard then.
-
Do not use amplifier efficiency as a proxy for electrode phase: peak final-amplifier efficiency did not correspond to 120-degree phase difference between the dees, so phase must be servoed from dee pickup signals directly, with separate efficiency servos trimming the amplifiers (five loops total on this machine).
Source, quote & tabletop applicability
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
Tabletop: Same programme's RF paper (ucrl-3153 p.7) draws the identical moral - measure the quantity you care about at the electrode, not a correlate at the amplifier. For a next machine - derive tuning/phase feedback from the dee pickup, not from LDMOS drain current or forward power, which optimize at subtly wrong points.
-
Size deflector gaps by the VE relationship: for equal sparking probability with given materials, gap voltage times cathode gradient is constant. Experimentally valid from 0.2 mm to at least 8.5 cm, so it covers any tabletop deflector gap.
V(kV) * E(kV/cm) = const; equivalently V ~ K*d^0.5Source, quote & tabletop applicability
for equal probability of sparking with given materials, the product of gap voltage and cathode gradient is a constant.
Tabletop: Directly. For a next machine's deflector, pick a VE number and the gap/voltage trade falls out; a 3-mm gap at VE=1.5e4 (kV)^2/cm predicts ~67 kV and ~220 kV/cm.
-
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 & tabletop applicability
In order to provide an adequate margin for day-to-day operation, a design value of 1.5 X 10^4 should be used.
Tabletop: The single most quotable deflector design number, from an operating cyclotron with an in-tank vacuum no cleaner than an amateur's. Design a next machine's electrodes to 1.5e4 and treat anything above as commissioning margin.
-
Electrode material ranking by measured spark damage in a magnetic field: 316 stainless, 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 (stays in the gap region).
best: 316SS/inconel/Mo/K-monel/Ti/Ni > Cu/Ta/Al > Ag; carbon anomalousSource, quote & tabletop applicability
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.
Tabletop: Make the next machine's deflector electrode 316 stainless (cheap, machinable, on the best-tier list); avoid copper or aluminum HV surfaces even though they are handy shop stock.
-
There is a critical magnetic field for each electrode material, ranging 4-15 kG, above which spark damage is severe and below which it is negligible; the field does not lower first-spark voltage, but crater damage accumulated in-field lowers holding voltage. Consider conditioning at reduced magnet current.
B_critical = 4-15 kG depending on material; bake in below it when possibleSource, quote & tabletop applicability
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.
Tabletop: The reference machine's field (~6 kG) sits at the low edge of the 4-15 kG damage band, a real advantage. Conditioning the deflector at reduced field, then raising B, is nearly free insurance.
-
Spark energy has an optimum, not a minimum: a 24-pF gap baked in to only 10 kV, adding 0.0125 uF raised it six-fold to 60 kV, but 0.5 uF cut it to 5 kV with severe craters. Bake-in is surface heating - too little spark energy leaves sharp pits, too much digs craters.
breakdown 10 kV @ 24 pF -> 60 kV @ 0.0125 uF -> 5 kV @ 0.5 uF (dc, no B field)Source, quote & tabletop applicability
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.
Tabletop: Directly sets deflector-supply philosophy - provide an adjustable, limited energy per spark (see UCRL-10655 crowbar) rather than either a stiff low-impedance supply or one that quenches sparks entirely.
-
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; 316 stainless needs about ten times as many sparks as other materials to reach ultimate voltage.
~30 sparks/cm2; ~30 s/cm2 bake-in time; x10 for 316SSSource, quote & tabletop applicability
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.
Tabletop: A palm-sized tabletop electrode (~100 cm2) conditions in under an hour - or ~10 h if 316SS. Write conditioning into the next machine's ops checklist as a scheduled activity, not a nuisance.
-
Minimize high-voltage electrode surface area by tailoring the field to the beam cross-section; less area means less bake-in sparking and less contamination collection. The 88-Inch used a 0.5-in-high field for a 0.25-in-high beam (2x margin for misalignment and median-plane shift).
field height ~ 2x beam height; radial field extent from incoherent oscillations (0.1-0.4 in at the 88-Inch)Source, quote & tabletop applicability
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.
Tabletop: Directly. Measure the next machine's beam height at extraction radius, size the deflector field window ~2x that, and keep the HV bar as small and short as the trajectory allows.
-
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 & tabletop applicability
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.
Tabletop: Direct machining rule - for a next machine's 3-mm deflector gap, radius every HV edge to at least 1.5 mm and polish.
-
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 & tabletop applicability
At the smaller gaps the electrode vibrated like a tuning fork in a tuning-fork oscillator.
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: Cheap upgrade that scales down perfectly - line the grounded surfaces opposite the next machine's HV bar with thin tungsten (or at minimum molybdenum) sheet, edges overlapped.
-
With spark-current control at the supply and tungsten anodes, deflector capacitance from 67 to 580 pF made no significant difference in VE; at least 600 pF is tolerable. Lower capacitance wants higher crowbar current and vice versa. VE was also independent of magnet current over the full 167- 2500 A range.
VE independent of C_deflector 67-580 pF and of B over full range, crowbar re-optimized per pointSource, quote & tabletop applicability
we could compensate for deflector capacitance; at lower capacitance we could crowbar at higher spark currents, and vice versa.
Tabletop: Frees the mechanical design - cable runs and feedthrough capacitance in a tabletop deflector (tens of pF) are a non-issue provided the supply has adjustable spark-energy limiting.
-
Carbon septa hold ~75% of metal-septum VE with no beam, but beam heating evaporates carbon onto the HV electrode and collapses voltage-holding (to ~25% of normal in the worst case), requiring a vent and solvent cleaning. A 500-uA, 32-MeV deuteron beam did not destroy the carbon septum thermally - contamination, not survival, is the failure mode. Use metal septa.
carbon VE ~1.7e4 = 75% of metal, beam-off only; contamination can cut deflector VE to 25%Source, quote & tabletop applicability
When we increased the beam current, the carbon evaporated from the septum, contaminated the high-voltage electrode, and very little voltage could be held.
Tabletop: 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 contamination mechanism is temperature-driven, so thin-foil hot spots still apply. Default to tungsten/molybdenum septum, revisit carbon only with septum-temperature data.
-
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 & tabletop applicability
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.
Tabletop: The reference machine and a next machine use oil diffusion pumping, so expect the dirty-system dark-current regime; the ion-scrub recipe needs only a variac, a 480-V transformer, a limiting resistor, and the existing H2 feed - a directly copyable conditioning procedure.
-
Diagnose whether a deflector is sparking-limited by plotting voltage vs gap on log-log: if the points follow a VE line, sparking phenomena limit; departures indicate an extraneous cause (supply parasitics, vibration, contamination). Insulate each ground electrode and meter intercepted beam current to align the deflector to the trajectory.
log V vs log d following slope of VE line => spark-limited; insulated ground electrodes as alignment monitorsSource, quote & tabletop applicability
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.
Tabletop: Both halves are free instrumentation for a next machine - a three-point V(d) test during commissioning, and an insulated septum/ground-electrode current readout for beam steering (same trick as the reference machine's Faraday-cup practice).
-
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 & tabletop applicability
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
Tabletop: The governing philosophy for any next machine's deflector supply - low stored energy is also the personnel-safety property. A sub-joule store at 50-100 kV is achievable and sufficient.
-
A high-frequency Cockcroft-Walton from cheap parts is the right architecture for a sparking deflector load: six stages of 100 series silicon diodes per board (600 piv, 0.75 A each), each diode shunted by 250 pF/500 V ceramic to grade inverse voltage, 900 pF 30-kV TV-type ceramic capacitors between decks, driven at 100 kc; delivers 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 & tabletop applicability
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
Tabletop: The 1963 'inexpensive silicon diodes + TV ceramic caps' recipe is today a standard multiplier stack; keep the two design features that matter - per-diode grading capacitors and high drive frequency (small energy per stage, fast regulation).
-
Crowbar the oscillator screen grid, not the HV: a 3D22 thyratron grounding the screen stops power flow to the deflector within a few microseconds of spark detection (30-ohm ground-return shunt, capacitively coupled, RC-filtered against rf), recycles in 1 s, and the crowbar bias knob IS the spark-energy control - from invisible sparks to heavy arcs.
crowbar senses I via 30-ohm return shunt; cutoff in a few us; recycle 1 s; spark duration = f(bias setting)Source, quote & tabletop applicability
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
Tabletop: The feature to replicate in a modern build - a solid-state inverter driving a CW stack gives the same microsecond drive-kill for free (gate shutdown on an overcurrent comparator), and the threshold should be an operator knob used during bake-in, per UCRL-10654.
-
Space multiplier decks ~2 in for a nominal maximum design gradient of ~10 kV/in (4 kV/cm) along the open-air column, and arrange the diode pattern so board-level gradients are minimized, with components on opposite board faces where deck-to-deck potential (up to 20 kV) appears.
air-insulated column design gradient ~10 kV/in; 12 boards in 8-in-OD lucite tube, 27 in tallSource, quote & tabletop applicability
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
Tabletop: A conservative, corona-quiet air-gradient number for amateur HV column layout; at 60 kV total a next machine's stack wants ~6 in of creep/clearance headroom or potting/SF6-free oil.
-
Silicon-diode storage time does not matter when rectifying into a capacitive load: the ~2-us junction-storage overshoot at 100 kc still charges the load to peak. (For operation above 100 kc, 5-MeV electron irradiation - 400 uA/cm2 for 17 min - improved rectification, cutting apparent back resistance 10x to ~200 Mohm with no change in ~900 V avalanche voltage.)
t_storage ~2 us OK at 100 kc into C-load; irradiated diodes usable >100 kcSource, quote & tabletop applicability
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
Tabletop: Historical for parts choice (modern fast-recovery diodes moot the issue) but the design insight stands - CW stacks feeding capacitive deflector loads tolerate slow diodes; spend money on voltage rating and grading instead.
-
High carrier frequency buys regulation: 100-kc drive gives the regulator loop a 2500-c/s unity- gain frequency and 0.01% deflector-voltage stability, ultimately limited by the precision divider - 120 metal-film resistors (<36 ppm/C) need only ~3 C temperature uniformity (forced-air) to hold 0.01%.
f_carrier 100 kc -> f_unity 2500 c/s; 0.01% regulation; divider spec 36 ppm/C, dT < 3 CSource, quote & tabletop applicability
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
Tabletop: Deflector voltage stability maps directly to extracted-beam steering stability; the lesson - regulation is limited by the divider, so buy/build the divider first - applies at any scale, and 0.01% is far beyond what a next machine needs (1% steers by ~1% of the deflection).
-
Filter CW ripple using the deflector itself as the filter capacitor - a series resistor (here 100 kOhm into ~250 pF of deflector) forms a one-pole RC that attenuated 3% ripple by 15x at 100 kc, and the same resistor isolates supply-side stored energy from the spark (energy behind the resistor dissipates in it, not in the arc).
R_series=100 kOhm, C_defl~250 pF -> pole 6.7 kc, x15 attenuation at 100 kc; costs 500 V drop at 5 mASource, quote & tabletop applicability
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
Tabletop: Two functions from one cheap HV resistor - ripple filter and spark-energy isolator (the isolation claim was independently tested in UCRL-10654 p.25). Put a 50-100 kOhm non-inductive resistor in the next machine's deflector feed.
-
Magnetic shielding of glass tubes near the cyclotron is mundane but mandatory - 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 & tabletop applicability
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
Tabletop: Modern solid-state supplies mostly shrug at 150 G, but CRT-style meters, vacuum gauges, photomultipliers, and any remaining tubes near a next machine's yoke need the same treatment; mild steel is enough at this level.
-
Derive pulser rise time 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 deflecting voltage must rise 10-90% in ~0.1 us (about one ion transit) and the pulse must fire within +/-5 rf cycles of the exact frequency.
t_rise ~ (bar spacing / radius gain per turn) x T_rf; here 1 in / 0.1 in = 10 cycles at ~10 Mc -> ~0.1 us (verified on page image)Source, quote & tabletop applicability
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
Tabletop: Synchrocyclotron-specific hardware (a next machine's CW deflector needs no pulse), but the requirements chain - turn separation sets element aperture sets timing/rise budget - is the template for sizing ANY extraction element, including the next machine's septum entrance.
-
The 184-inch pulsed electric deflector needed ~75,000 V/cm (about 200 kV across bars spaced one inch) to shift the center of rotation of 200-MeV deuterons enough to enter the lowered-field magnetic channel - electric extraction fields at full synchrocyclotron energy are ~10x a CW deflector's gradient, which is why it had to be pulsed.
E ~ 75 kV/cm; V ~ 200 kV across 1-in (2.54 cm) bar spacing (verified on page image)Source, quote & tabletop applicability
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
Tabletop: Scale perspective - deflecting-field requirement grows with beam rigidity, and at a next machine's 300 keV-1 MeV the equivalent job needs only tens of kV/cm CW (cf. UCRL-10654's 150-200 kV/cm at 50 MeV). Sub-MeV extraction is in the easy corner of this trade.
-
Derate pulsed switches for what operation does to them, not the data sheet: 5C22 thyratrons rated 16 kV arced plate-to-grid and failed above 11 kV because the plate voltage reverses in 0.3 us each shot; and one tube switching 5000 A exceeds its peak current rating ~20x, so 8 tubes were paralleled per transformer (16 total) with small individual plate-lead inductances to force current sharing.
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 & tabletop applicability
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
Tabletop: 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 the exact role the 5C22 reversal limit played here.
-
To fire many parallel switches simultaneously, feed each from its own artificial transmission line: 1000-V, 20-ohm, 0.2-us triggers brought 16 thyratrons into conduction within 0.1 +/- 0.01 us, provided the trigger source impedance is low enough to charge all lines in parallel.
per-tube pulse-forming line, 1 kV / 20 ohm / 0.2 us; jitter < 0.01 us across 16 tubesSource, quote & tabletop applicability
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
Tabletop: Classic paralleling technique still used in pulsed-power; relevant only if a next machine ever adds a pulsed element (fast chopper, kicker for time-of-flight work), but then it is the reference method.
-
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 & tabletop applicability
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
Tabletop: Not needed for a CW deflector, but the de-aerated-oil corona cure, the 3x overvoltage proof test, and the interlaminar-voltage failure mode are transferable HV-construction craft for any oil-insulated amateur component.
-
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 & tabletop applicability
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
Tabletop: The two lessons that outlive the hardware - charge-reversal duty is what kills capacitors (modern pulse caps are still specced by % reversal), and ESL budgets, not just C and V, set rise time. Cable-as-capacitor remains a legitimate cheap trick for one-off pulse work.
-
DC resonance charging through the pulse capacitors' voltage reversal gives a free voltage step-up: an 11,000-V thyratron plate voltage was maintained from a 2,750-V supply (4:1, vs the textbook 2:1), because each shot leaves the capacitor reversed; ratios up to 10:1 were observed, the value depending on system losses.
V_plate/V_supply = 4:1 typical (10:1 observed) with post-pulse reversal, vs 2:1 classical resonant chargingSource, quote & tabletop applicability
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.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 15
Tabletop: Pulsed-modulator craft, not CW-deflector material; file under 'if a next machine ever needs a kicker' - it means the HV DC supply can be a quarter of the switch voltage.
-
Report and accept the shortfall: measured 10-90% rise was 0.15 us against the 0.1-us requirement (blamed on capacitor internal inductance), and the fix in operation was raising peak voltage rather than rebuilding - increasing the drive compensates for a slower edge.
t_rise achieved 0.15 us vs 0.1 us spec (+50%); compensate with higher V_peak (verified on page image)Source, quote & tabletop applicability
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
Tabletop: A general commissioning lesson - extraction elements have one strong knob (voltage/field) that can buy back deficiencies in the others; design in voltage headroom (UCRL-10654's derating serves the same end from the other side).
-
Any resonant/regenerative extraction scheme must satisfy three requirements: (a) arrest the precession so the radial-oscillation maximum recurs at one azimuth, (b) build enough radial gain per turn to step over the channel/septum wall, (c) keep axial blowup losses acceptable.
requirements: precession arrested; gain/turn > septum wall + entrance margin; axial losses boundedSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The siting logic transfers even though the numbers are synchrocyclotron pole-edge values - put the next machine's septum/regenerator equivalent just inside where the field map says the beam dies (n -> 0.2 walkout or resonance), and know that every mm inward is energy given away.
-
Design a regenerator by the seven-step procedure: nonlinear equations of motion -> amplitude- dependent radial/axial frequencies from the measured field (Krylov-Bogoliubov) -> matrix analysis of radial amplitude growth and required momentum kick -> field perturbation from the kick -> resulting axial kick -> axial growth -> pick position from the family of solutions. Gain per turn follows a = -sin(wr*th1)/sin(wr*(th2-th1)); a smaller crossing interval means more gain but a stronger regenerator.
a = -sin(wr*th1)/sin(wr*(th2-th1)), wr = wr(r>R); delta(p') = -p0''*sin(wr*th2)/ sin(wr*(th2-th1))Source, quote & tabletop applicability
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
Tabletop: The workflow (measured field -> amplitude-dependent tunes -> impulse-matrix tracking -> element strength) is exactly the CYCLOPS-lite pipeline planned for a next machine; the specific peeler-regenerator field shapes are synchrocyclotron machinery and need not transfer.
-
Express regenerator strength as integrated field-times-angle: B*theta = delta(p')*B0/(1+p) gauss-radians. Worked 184-inch example (B0 = 21,730 G): 5.6 kG-deg at 0.5 in radial displacement rising to 25.6 kG-deg at 2.5 in - i.e., bump fields of order 1% of B0 over tens of degrees suffice.
B*theta = delta(p')*B0/(1+p); table 0.5->5.58, 1->11.0, 1.5->16.5, 2->22.3, 2.5->25.6 kG-deg at B0 = 21.73 kGSource, quote & tabletop applicability
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
Tabletop: The gauss-radian bookkeeping is a handy unit for ANY azimuthally-localized field bump (harmonic coils, shims, channel compensation) on a next machine; the percent-of-B0 scale of effective perturbations is a useful sanity anchor. The specific values are 100+ MeV synchrocyclotron numbers.
-
A regenerator kicks the axial motion about twice as hard as the radial motion (for 1-in axial amplitude), and particles with large axial amplitude are lost; the beam survives because the impulse period and axial period differ and the radially-falling field damps axial amplitude - so regenerator azimuth and starting radius are the free knobs to optimize extraction efficiency.
delta(z') ~ 2x radial disturbance at 1-in axial amplitude; d(axial)/dr of Br from curl B = 0 -> Br = (dBz/dr)*zSource, quote & tabletop applicability
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
Tabletop: The general warning transfers - any radial-field-gradient extraction element has an off-midplane Br that pumps vertical motion, so check axial kicks in the next machine's tracker for the deflector fringe and any field bump, and expect to lose the large-axial-amplitude tail first.
-
The magnetic channel's own uncorrected fringe field perturbs the beam BEFORE it enters: compute that impulse like the regenerator's and fold its compensation into the regenerator field, rather than relying on maximum-effort corrective shimming of the channel (shimming is difficult and degrades the channel).
treat channel fringe as a fourth orbit region; adjust regenerator to compensateSource, quote & tabletop applicability
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
Tabletop: Direct analog for a next machine - the septum and exit-channel iron (or the deflector entrance fringe) perturbs the last internal turns; model that perturbation in the tracker and compensate upstream (harmonic coil/shim) instead of trying to null the channel's leakage to zero.
-
RF resonant extraction: apply a radial electric field with a linear gradient (force proportional to outward displacement) over a limited azimuth, at frequency omega = 2*omega0*sqrt(1-n)/l; the radial Hill equation then becomes absolutely unstable and amplitudes grow. Choose l = 1 - it needs the least precise frequency match, which matters where the edge field (and hence radial tune) changes rapidly.
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 & tabletop applicability
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
Tabletop: A genuinely tabletop-compatible extraction assist - an electrode pair driven by a small independent oscillator. For a next machine (nu_r ~ 1) the required frequency is near the orbital frequency's sidebands; worth a tracker experiment before committing hardware.
-
The rf gradient needed is modest: 4.3 kV/cm (design ceiling "less than 5 kV/cm") over a 60-deg azimuth sector was enough, in IBM 650 orbit calculations for 50-MeV deuterons at 17 kG (n = 0.1), to produce substantial turn separation - and such a field is easily made by 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 & tabletop applicability
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.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 8
Tabletop: kV/cm-class rf on a small electrode is trivially available at a next machine's scale (hundreds of volts across a few mm). The scheme was never demonstrated on hardware in this report - treat as a promising computed option, not proven practice.
-
The variable-energy argument for electric extraction elements: fixed magnetic perturbations (peeler/regenerator, channel iron) are set into the pole geometry and cannot follow a machine whose energy and field change, whereas an electrical perturbation's frequency and gradient are knobs - so variable-energy machines should extract with tunable electric systems.
tunable (f, E) replaces fixed (B-bump geometry) for variable-energy operationSource, quote & tabletop applicability
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
Tabletop: Directly supports the next machine's plan-of-record (electrostatic deflector, no fixed magnetic channel) - an educational machine that will run at more than one field/energy point wants its extraction strength on a knob, not in iron.
-
Vertical beat-frequency (VBF) loss is the destructive dual of rf extraction: when the axial- oscillation frequency satisfies the resonance relation with rotation and dee frequency AND a vertical electric-field component proportional to z exists (even the weak vertical component of the accelerating gap field), the axial equation is absolutely unstable and the beam is destroyed impressively fast.
resonance f_z = |h*f_osc - k*f0|-type condition + E_z proportional to z -> absolute axial instabilitySource, quote & tabletop applicability
In the weak vertical field component of the accelerating voltage in the 184-inch cyclotron the beam loss was impressively fast.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 5
Tabletop: A real design caution at any scale - dee misalignment or asymmetric liners give exactly the z-proportional E_z this resonance needs. Keep a next machine's dee/dummy-dee vertically symmetric and check whether nu_z resonates with any strong rf harmonic at operating field.
-
Do not expect an rf perturbation to kick particles out in one pass: orbits precess, take a few influential encounters, drift off the perturbation for several turns, then re-engage - but precession ultimately drives ALL particles to large radial amplitude, including those started with zero oscillation amplitude (some orbits are even temporarily damped).
amplitude growth is episodic over many turns; ultimately all phases perturbed to large amplitudeSource, quote & tabletop applicability
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
Tabletop: Sets expectations for any resonant/precessional scheme on a next machine - extraction is a many-turn statistical process, so judge schemes in the tracker by turns-to-extraction and septum-hit fraction, not single-pass kick size.
-
Condition the RF system past its design dee voltage and hold it there: the 63-inch reached 75 kV dee-to-dee under vacuum against a 60 kV design spec and only then was the RF problem declared solved — a demonstrated ~25% voltage margin, held "for long periods", was the acceptance criterion, not a momentary peak.
acceptance = sustained hold at ~1.25 x design dee voltage under vacuumSource, quote & tabletop applicability
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.
Tabletop: Directly transferable acceptance test for the reference machine's LDMOS upgrade — run the dees 25% above the planned operating voltage for hours before calling the RF done; a margin that survives only seconds is not margin.
-
Rectify the dee-voltage pickup signal with a vacuum tube, not semiconductor diodes, anywhere near the machine: germanium diode calibration drifted under neutron bombardment; a Type 2C40 vacuum-tube rectifier stayed constant, and the calibration holds as long as the probe-to-dee distance is unchanged.
Source, quote & tabletop applicability
the vacuum tube rectifiers are unchanged by neutron bombardment and, unless the probe-to-dee distance is changed, the calibration remains constant.
Tabletop: Two transferable halves: (1) semiconductor sensors near the chamber are a calibration-drift risk once neutrons appear; (2) a capacitive dee-voltage pickup is calibrated GEOMETRY — mechanically fix the probe-to-dee distance or every calibration is void. Bears directly on retiring the uncalibrated ~800 V nominal dee-voltage number on the reference machine.
-
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 & tabletop applicability
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.
Tabletop: The trick scales down perfectly — a nA-to-uA tabletop beam calorimeter (thermistor on an isolated cup) can be calibrated the same way with a surface-mount resistor dissipating known milliwatts. Electrical-substitution calibration converts any thermal sensor into an absolute beam-power meter.
-
Cross-check calorimetric beam power against electrically calculated power (beam current x accelerating voltage) at every operating point; the 86-inch table shows agreement within 5% across 0.4-1.0 mA and both energies — disagreement beyond that flags an instrumentation or beam-loss problem.
P_calorimetric vs P = I_beam x V_equiv; expect agreement ~5%Source, quote & tabletop applicability
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%.
Tabletop: The redundancy principle transfers even at nA — Faraday-cup current times computed energy should match any thermal or activation measurement; a persistent gap means secondary-electron error, wrong assumed energy, or beam missing the cup.
-
Ion-source axial (z) position is a first-order energy and beam-quality knob: raising the 86-inch source 1.5 in (to one inch below magnetic center, accelerating slit raised the same amount) took protons from ~19 to ~24 MeV at the same radius, because the beam had been scraping the dee from an off-center start.
Source, quote & tabletop applicability
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.
Tabletop: A 26% energy gain from moving the source — on the reference machine, treat filament/chimney height relative to the median plane as a tuned parameter worth systematic scans, not a set-and- forget dimension. Symmetric placement about the magnetic (not mechanical) midplane is the target.
-
Diagnose an off-center beam from where it strikes: on the 86-inch, beam hitting the periphery of the south dee when the target was lowered revealed the center of rotation was offset ~3 inches south; the fix included moving the dees 1/2 in south. Burn marks and asymmetric losses are orbit-center data.
Source, quote & tabletop applicability
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.
Tabletop: Fully transferable — witness marks on the reference machine's dee edges and probe shadows are a free orbit-centering diagnostic; an orbit center offset a few percent of pole radius is normal and correctable by moving source or dees.
-
Give the ion source a positive mechanical registration: a bracket on the liner fixes the 86-inch source at its correct height, guarantees the same position run to run, grounds the stem, and reduces RF pickup heating of the support tube.
Source, quote & tabletop applicability
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.
Tabletop: 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.
-
Measure the z-wise (axial) beam distribution with a multi-segment probe at several radii: a five-segment target probe on the 22-inch showed nearly all proton loss to the dees occurs during early revolutions, with only a small percentage lost beyond half the maximum radius — so central-region focusing, not outer-radius optics, controls transmission.
Source, quote & tabletop applicability
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.
Tabletop: Both the finding and the instrument transfer: stack 3-5 insulated foils as a segmented z-probe on the reference machine to see where the beam sits vertically, and spend tuning effort on the first turns — beam surviving to half radius will almost all reach full radius.
-
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). At low arc current the H3+/H1+ ratio is high; raising arc current increases both total H1+ and the H1+/H3+ ratio.
species peaks at B proportional to m/q for fixed f; H3+ energy = 1/3 H+ energy at same radiusSource, quote & tabletop applicability
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.
Tabletop: 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 dominate at weak arc — run the arc hard for protons. (Fig. 6, PDF p.18, shows the resolved peaks.)
-
Match arc-slit length to dee geometry: 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 — a long emission slit feeds ions the dees cannot accept and just loads the RF.
Source, quote & tabletop applicability
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.
Tabletop: On a tabletop machine where every watt of RF matters, an oversized source aperture wastes drive as ion loading; try a shorter emission slit on the reference machine's source and watch accepted beam per unit dee loading, not raw source output.
-
Negative dee bias can substitute weakly for an accelerating slit: on the 22-inch, increased dee bias raised full-radius beam by up to 30% — but only with no accelerating slit mounted; with a slit the effect vanishes, and the slit outperforms the optimum bias.
Source, quote & tabletop applicability
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.
Tabletop: Worth a cheap experiment on the reference machine (a DC bias supply on the dee), but the ORNL conclusion is that geometric phase selection (a slit) beats electrostatic tricks — put the effort into the puller/slit geometry first.
-
Declare a chamber vacuum-tight by rate-of-rise, not ultimate pressure alone: the 63-inch was accepted after leak-hunting brought it to 1e-5 mm Hg with a rate of rise of 0.00025 microns/sec (~0.9 mTorr/hr) valve-off.
acceptance ~ 2.5e-4 micron/sec (~0.9 mTorr/hr) rate-of-rise at 1e-5 mm Hg baseSource, quote & tabletop applicability
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.
Tabletop: The practice and even the number are usable — rate-of-rise normalizes out pump speed, so it is the honest leak metric for the reference machine's chamber; log it after every reassembly as a regression test. (Big-chamber outgassing makes their absolute number lenient; a small clean chamber should beat it.)
-
Re-measure the magnetic field with the tank evacuated before commissioning: 63-inch measurements under vacuum showed negligible distortion from atmospheric loading and a first harmonic inhomogeneity of ~0.03% — closing out the field question with the machine in its real mechanical state.
first harmonic target ~3e-4 of main field (63-inch as-commissioned)Source, quote & tabletop applicability
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%.
Tabletop: Two transfers: verify a next machine's field map with the chamber assembled and pumped (pole deflection under vacuum load is a real 1950s worry that proved negligible for them — measure once to confirm); and note 0.03% first harmonic as what a carefully shimmed classical machine actually achieved — consistent with the ~5 G field target for a next machine.
-
Budget real machine time for beam characterization during a commissioning period: of 50 bombardments on the 86-inch in the post-modification quarter, 10 were beam-profile and 5 were energy-measurement runs — 30% of all machine time spent measuring the beam rather than using it.
~1/3 of runs devoted to beam profile + energy measurement after any major changeSource, quote & tabletop applicability
The bombardments are tabulated below: Beam profile 10, Isotope production 8, Experimental 16, Energy 5, Physics 7, Radiation damage 4.
Tabletop: 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 before "physics" runs; ORNL treated characterization as scheduled work, not overhead.
-
Establish beam energy by at least three independent methods before quoting it: the 86-inch energy (~23 MeV at 30.5 in) was called well established only after foil-stack range measurements, 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 & tabletop applicability
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.
Tabletop: Directly actionable for the "~150 keV-class computed" number on the reference machine: convert computed to measured with two independent checks — Al foil range/transmission steps and, at higher current after the RF upgrade, cup calorimetry. One method is a claim; three in agreement are a measurement.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Track electrical efficiency (beam power / oscillator input) as a commissioning health metric and expect it to improve with beam level: the 86-inch reached 40% net ion-loading efficiency at 1.85 mA, twice that at 0.5 mA, because dee excitation and ion loading are fixed loads; the 1339 quarter quotes 9% of oscillator input on target at 1 mA vs 6% at 0.5 mA.
eta = P_beam/P_osc; fixed losses (dee excitation + ion loading) dominate at low beamSource, quote & tabletop applicability
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.
Tabletop: 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; on any small machine almost all RF power is overhead, so chase Q and coupling, not amplifier watts, for efficiency.
-
Use expendable grazing-incidence targets for high-power tuning: aluminum targets struck at grazing incidence spread the power density and withstood full 86-inch beam during the adjustment period, reserving real targets for production.
grazing incidence spreads P/A by 1/sin(theta_graze)Source, quote & tabletop applicability
grazing-incidence type aluminum targets were used because of the high beam intensities they withstand.
Tabletop: Scale-honest — the reference machine's nA beams cannot melt anything, but the geometry trick matters for beam VIEWING (a grazing phosphor or foil intercepts more turns and lights up at lower current) and becomes thermally real on any 5-13 kV / uA-class upgrade path.
-
Prove first beam with a radiation signature plus a physics argument, not just probe current: 63-inch first beam was a brass target at 21 in radius showing gamma count 8x background; since N+ ions at that radius would have only 2.5 MeV (below reaction thresholds), the activity itself proved the beam was N3+.
species/energy check = radiation only possible if q/m assumption correctSource, quote & tabletop applicability
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.
Tabletop: The reference machine's best-beam case (5.6x background on the Faraday cup) sits in exactly this evidentiary tradition — and the energy-threshold argument is the template for a source-species test: an observed nuclear signature whose threshold excludes the molecular-ion hypothesis is proof of species without a spectrometer.
-
Map internal beam current vs radius early and expect orders of magnitude of attenuation on an untuned machine: first-month 63-inch probe currents were 2000, 500, 170, 30 uA at 5, 10, 14, 18.5 in, unreliable beyond that, with ~1 uA estimated at the 25.5-in extraction radius — a factor of ~2000 from first turns to full radius.
commissioning-era attenuation: ~3 orders of magnitude center-to-edge is normal, not brokenSource, quote & tabletop applicability
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.
Tabletop: Calibrates expectations for the reference machine's and a next machine's first runs — nA at full radius from uA-class first-turn current is what a real machine did at first beam; log the whole I(r) curve, because its shape (where the loss happens) is the tuning roadmap.
-
Confirm beam energy and species by activation half-lives 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 — reaction thresholds then bound the beam energy.
Source, quote & tabletop applicability
A carbon (graphite) target gave rise to 112-minute and 15-hour activities which are assigned to F 18 and Na 24 respectively.
Tabletop: Below nuclear thresholds the 150-keV reference machine cannot use this — but it becomes the cheapest absolute energy check the moment any upgrade crosses a low-threshold reaction, needing only a GM counter and a stopwatch; the practice (identify by half-life, bound energy by threshold) is scale-free.
-
Make ion-source position adjustable from outside while the machine runs: the 86-inch added a Selsyn-driven rotator to optimize source orientation during operation, and 63-inch experience found source-to-field alignment "extremely critical", forcing external adjustments — manual set-and-pump-down positioning loses the optimum.
Source, quote & tabletop applicability
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.
Tabletop: Strong design input for a next machine: budget at least one live source degree of freedom (rotation or z) through the vacuum wall — both ORNL machines retrofitted it after finding the optimum could not be reached blind. On the reference machine, even a graduated feedthrough beats vent-adjust-pump iteration.
-
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 ~ -(1-2)% of dee RF voltage during startup (63-inch used -1 to -2 kV on 50 kV)Source, quote & tabletop applicability
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.
Tabletop: Transferable at proportional scale (tens of volts on the reference machine's ~1 kV dees, a few hundred on the LDMOS upgrade) — multipactor/ion loading during RF ramp-up is a classic small-machine failure mode and a bias supply is the classical cure.
-
Fit carbon (graphite) lips to dee edges where sparking limits voltage: installed on the 86-inch when dee-to-dee voltage rose to 400-500 kV; graphite's low sputter/vapor-metal contribution reduces spark initiation compared with bare copper edges.
Source, quote & tabletop applicability
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.
Tabletop: The 400-500 kV is MW-era and does not transfer; the material practice does — if the reference machine's 5-13 kV upgrade sparks at the dee gap, graphite edge pieces are the period-proven remedy and are trivially machinable.
-
Bench-test an ion source on a 180-degree beam path in the magnet before installing it in the machine: the 63-inch hot-cathode source was qualified dc by collecting after a half-turn — measuring the species mix (8 mA N+, 2 mA N++, 2 mA N+++), scanning the beam (peak 6x background), and estimating filament life (>10 hr) with no cyclotron time spent.
Source, quote & tabletop applicability
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+++.
Tabletop: 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.
-
When a source underperforms, look at where the drain current goes: the 22-inch dc injection source gave only 30 mA (vs 75 mA from the predecessor) and the diagnosis was that even in dc tests there was always high drain to the accelerating electrode — the same drain seen in rf tests, identifying interception, not production, as the deficit.
account for source output as beam + electrode drain; drain locates the lossSource, quote & tabletop applicability
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.
Tabletop: Current bookkeeping is free diagnosis — on the reference machine, meter the puller and chimney drains separately from the Faraday cup; a weak beam with a hot puller is a geometry problem at the source exit, and no arc-power increase will fix it.
-
Isolate radiation effects with matched control experiments: ORNL paired every bombarded corrosion specimen with a control given the identical thermal history, and when a thermal gradient was suspected as the real cause, built a control with the same 815 C-to-40 C gradient (specimen on a water-cooled tube in the furnace) — only then attributing the effect to protons.
Source, quote & tabletop applicability
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.
Tabletop: The control-experiment discipline transfers whole to any reference-machine or bench-scale target or activation claim — for every "the beam did X", run the identical setup minus beam; the 1339 quarter also flags their power-measurement accuracy as only +/-30%, a humbling uncertainty note worth copying into lab-book practice.
-
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 fixes V_dee; r_1 ~ sqrt(q*V_dee*m)/(q*B) must fit source/puller radiusSource, quote & tabletop applicability
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.
Tabletop: 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.
-
Distrust scale-model magnet studies at excitation extremes: the 0.275-scale ORIC model set the Davis central-region design but could not be operated at the lowest planned field (3.5 kG); full-scale mapping then revealed a defocusing radial-profile depression at low fields that the model never showed, forcing an iron redesign.
Source, quote & tabletop applicability
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.
Tabletop: 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.
-
Shape central-region iron with a plug and saturating caps so one geometry serves all 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 (disappear magnetically) at high field but fill in the central field hole at low field — passive, self-adjusting compensation.
Source, quote & tabletop applicability
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.
Tabletop: Deliberately-saturating iron as a field-programming element is a trick FEMM models well — for a next machine's central plug or shim stack, a piece sized to saturate at the main operating point gives low-field correction "for free" without trim windings.
-
Set isochronism-by-trim-coil acceptance at ~15 gauss: Davis computed trim-coil settings with a linear program against Smith-Garren isochronous standards, and accepted fields whose greatest deviation from isochronism was under 15 G — roughly 1e-3 of the working field — as good enough for acceleration through the central region.
max |B - B_isochronous| < 15 G (~0.1-0.4% of field), trim settings by linear programSource, quote & tabletop applicability
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.
Tabletop: A measured 1960s tolerance to calibrate the next machine's 5 G / 5-deg-RF-phase target against: an AVF machine accelerating hundreds of turns lived with 15 G deviation. A classical few-tens-of-turns tabletop machine tolerates proportionally more — the phase-slip integral, not the gauss number, is what to check in the tracker.
-
Get central-region starting conditions by backward tracking: Davis estimated ion starting conditions by placing ions on a known-good 12-in equilibrium orbit and de-accelerating them to the center, then used those conditions to launch forward acceleration runs — 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 & tabletop applicability
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.
Tabletop: Directly implementable in the Python orbit tracker — find the equilibrium orbit at modest radius (easy, well-conditioned), integrate backwards to the source region, and read off where the source slit and puller must be; cheaper and more robust than guessing forward launch conditions in the messy first gap.
-
A deliberate central field bump can beat strict isochronism: Davis start-up data with 42-MeV alphas showed ~10% more extracted beam running trim coil 1 at +22 A (central radial bump for focusing) than at -145 A (the computed isochronous profile) — early axial focusing bought more beam than early phase perfection.
Source, quote & tabletop applicability
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.
Tabletop: Validates the classical-cyclotron instinct for a next machine: a small positive field bump at center (field falling with radius from turn one) focuses the turns that the z-distribution studies (ORNL 22-inch) show carry all the loss; give away a little phase to get it. Empirically checkable on the reference machine with shim washers at the pole center.
-
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, and that the radial oscillation build-up "is not excessive and soon damps to 0.3 inch" — the resonance was accepted, quantitatively, rather than avoided.
compute amplitude growth through resonance; accept if bounded and damping (here to 0.3 in)Source, quote & tabletop applicability
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.
Tabletop: Method for the CYCLOPS-lite tracker: don't just plot nu_r(r) and forbid resonance lines — integrate through them and report amplitude growth in millimeters against the aperture; a fast-crossed resonance with bounded growth is a non-event even on a small machine.
-
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 & tabletop applicability
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.
Tabletop: The 1966 proof that a next machine's compute-first pipeline (field map -> tracker -> build) is sound — if the field is measured carefully and the tracker is honest, first beam on the first pump-down is a reasonable expectation, not luck. Also a period example of commissioning on H2+ rather than protons for shielding reasons.
-
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 & tabletop applicability
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.
Tabletop: Directly relevant to the plan's open shielding gate: species choice is a radiological control. Commissioning a new machine (or the reference machine's RF upgrade) on H2+ at the same B*rho halves the per-nucleon energy and keeps early tuning below neutron thresholds — the machine physics transfers to protons afterwards, exactly as Davis planned.
-
Design the magnet around four field premises: field produced in a steel/copper-free cylindrical "gap" whose diameter is about nine times its axial height; mid-plane symmetry; no azimuthal dependence; and field falling with radius gently enough that n = -(R/H)(dH/dR) << 1/5 at all used radii.
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 & tabletop applicability
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
Tabletop: 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.
-
Use pole-tip efficiency E (gap flux utilization referred to pole-base flux) as a design scorecard: the theoretical maximum is 1, coils-far-from-gap designs cannot beat 0.71, a pole that works at "any" field reaches 0.52, and E = 0.64 is a realistic experimental design goal.
E = pi*rho^2*H0/(phi_p*B_p) (Eq. 86); benchmarks E_max=1, 0.71 unobtainable, 0.52 any-field pole, 0.64 design goalSource, quote & tabletop applicability
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
Tabletop: Gives the next machine's FEMM loop a quantitative target - compute gap-flux/pole-flux efficiency for each candidate tip and expect ~0.5-0.65, not the naive 1.0; large shortfalls flag leakage-wasting geometry.
-
With a conventional raised-edge shim the useful field radius reaches ~92% of pole radius; cutting a groove into the pole face just inside the raised edge extends it to ~96%. A tapered pole is superior to a straight pole because it permits higher gap density.
useful radius ~0.92*R_pole (raised edge alone) -> ~0.96*R_pole (groove inside raised edge)Source, quote & tabletop applicability
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
Tabletop: On 8-in poles the difference between 92% and 96% usable radius is ~9% in energy (B^2R^2); the groove-plus-raised-edge profile is cheap to try in FEMM and on the real shims. NYO-780 pp.9-10 reached the same ~96% figure experimentally - cite both.
-
Treat the analytic equipotential shim shape only as a starting point; the final shim contour must be found experimentally by mounting an approximate shim on the otherwise-final pole, measuring the mid-plane field, and reshaping iteratively.
Source, quote & tabletop applicability
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
Tabletop: Directly the next machine's shim program - FEMM replaces some iterations, but finite permeability and saturation mean the last passes happen on the bench with a probe map, exactly as NYO-780 (p.7) did with its bolt-together model magnets. Cite both.
-
Estimate the field contribution of fully saturated shim features (spikes, buttons) by treating them as permanent magnets with magnetization M = Bs/4pi; cylindrical spikes act as point charges m = M*A at their tips plus their images in the adjacent poles.
M = (B-H)/4pi = Bs/4pi; m = M*A; mid-plane field from point charges at spike tips + images (Eqs. 7-8)Source, quote & tabletop applicability
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
Tabletop: Handy closed-form sanity check for any center-cone or button shim on the next machine before FEMM - saturated iron adds field like a permanent magnet of strength Bs/4pi, independent of excitation.
-
Keep magnet coils as small as a reasonable power budget allows, because three costs scale with coil size together: coil resistance grows with mean circumference, the steel to complete the circuit grows with (2x coil height + radial width), and pole/yoke reluctance grows similarly.
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 & tabletop applicability
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
Tabletop: 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.
-
In a high-current low-voltage magnet coil, insulation is needed only for mechanical separation of conductors; cool with a few large channels in direct contact with big conductors rather than many small ones, since coolant pressure rises rapidly as channels shrink.
Source, quote & tabletop applicability
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
Tabletop: Argues for the classic amateur choice - few turns of heavy bar/strap at high current with generous cooling passages beats many-turn fine-wire coils on space factor, insulation risk, and pumping pressure.
-
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 & tabletop applicability
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
Tabletop: Directly a garage-scale construction technique - cut flat copper sectors, stack into a helix with brazed/bolted joints (see the 10 kA/cm2 joint rule), no winding mandrel needed.
-
Choose coil outside diameter by minimizing total cost C = steel + copper + energy, with unit costs per cm3 of steel, per cm3 of copper, and per 10-year-watt of power; set dC/dx = 0 for x = OD/ID ratio. Their 1952 worked sample: steel 1.89e-3 $/cm3, Cu 5.88e-3 $/cm3, energy 0.333 $/10-yr-watt.
C = C'st*2pi*(B/A)*S^3*R0^2*r0*x + C'cu*pi*f*(x^2-1)*S^3*r0^2*t + C'p*(rho*S/(f*t*log x))* (100*H0^2/(8*pi*E^2)) + G (Eq. 114); minimize over x = r_out/r_in; nomograph Fig. 1.33 (p.100), cost-vs-x curve Fig. 1.34 (p.101)Source, quote & tabletop applicability
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
Tabletop: This collection's only explicit dollar-optimization of magnet proportions - rerun Eq. 114 with 2026 unit costs (scrap steel, surplus copper, $/kWh over expected machine life) to place a next machine's coil proportions. NYO-780 p.8 did the equivalent sweep by model; cite both.
-
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 & tabletop applicability
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
Tabletop: Licence to trade a few percent of cost-optimality for access, cooling clearance, or stock material sizes - the optimum is a plateau, not a peak. Same flat-minimum finding as NYO-780 p.8 (coil height); cite both.
-
The unit costs that drive magnet optimization can only be truly determined after the cyclotron has operated for years, so the first-pass optimization is always an estimate - do it with estimated costs, and do not over-refine.
Source, quote & tabletop applicability
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
Tabletop: A 1952 statement of the plan's own doctrine - cost models are gated on real operating data, so freeze the estimate, build, and revise with actuals rather than polishing the spreadsheet.
-
Expect the analytically computed optimum coil OD/ID ratio to be biased HIGH (the constant-E assumption inflates it), and note that the optimum ratio is scale-dependent - do not copy another machine's coil proportions across a size class.
Source, quote & tabletop applicability
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
Tabletop: Two cautions in one - shave the computed OD, and treat big-machine coil proportions (including TID-454's own x~1.4) as non-transferable to an 8-12 in machine without redoing the optimization at that scale.
-
One square centimeter of true metallic contact distributed over a coil joint carries 10,000 A with negligible resistance and temperature rise; adequate mechanical strength is almost a sufficient requirement for a coil-conductor connection. Do not over-engineer joints.
~10 kA per cm2 of metallic contact with negligible drop; joint requirement ~ mechanical strengthSource, quote & tabletop applicability
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
Tabletop: Frees a builder from soldering anxiety on bus joints - a clean bolted lap of a few cm2 is electrically invisible at the tens-to-hundreds of amps any amateur coil carries.
-
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 & tabletop applicability
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
Tabletop: When sizing a surplus supply for the next machine's coil (or the number of turns for a given supply), pick turns so the coil's hot resistance sits at the supply's V_max/I_max corner.
-
Keep the magnetic circuit short with wide, thin yoke sections (given inside circumference at minimum average circumference), and proportion coils so that (coil OD - coil ID)/(sum of both coil heights) ~ 1, minimizing the steel circuit around them - but treat both statements only as guides.
(r_out - r_in)/(h_coil1 + h_coil2) ~ 1; yoke sections wide and thinSource, quote & tabletop applicability
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
Tabletop: 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.
-
Put the magnetically good steel where it counts: the pole base is flux-critical (its optimum cross section is found from B/(dB/dH) equal to a cost ratio, landing near B ~ 21,000 gauss for low-carbon steel), while yoke steel quality matters much less. The optimum is insensitive to design tweaks, and practical factors argue for running the pole base BELOW the computed density.
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 & tabletop applicability
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
Tabletop: For a next machine's steel shopping - spend on clean low-carbon (1006/1008) pole and pole-base stock, accept structural mystery steel in the return yoke, and size the pole base to run near but not into the knee (~1.8-2.1 T).
-
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 & tabletop applicability
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
Tabletop: 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.
-
Measure field shape as a RATIO to the center-of-gap field using paired flip coils and a null-balanced long-period galvanometer, not as absolute point values; ratios are far less sensitive to excitation-current drift, so current regulation requirements collapse.
null condition (Eq. 147) gives flux ratio from resistance ratios; flip-coil pair on a shaft rotating 180 deg avoids commutatorsSource, quote & tabletop applicability
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
Tabletop: 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 rather than absolute B(r), and supply drift drops out of the shim iteration.
-
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 & tabletop applicability
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
Tabletop: The workhorse formula for every odd-shaped passage in a cyclotron - dee interiors, annular gaps around the dee, slots - where handbook circular-tube formulas do not apply. Directly usable for auditing the reference machine's pump path and sizing a next machine's ducts.
-
The A^2/OL duct formula UNDERESTIMATES rectangular-duct conductance: -11% at a/b=1, -15% at 2, -20% at 3 vs Clausing. Multiply by K (1.108, 1.126, 1.151, 1.198, 1.297, 1.400, 1.444 at a/b = 1, 1.5, 2, 3, 5, 8, 10) for accuracy - or deliberately omit K to keep pump sizing on the safe side, as this design did.
K vs a/b: 1/1.108, 1.5/1.126, 2/1.151, 3/1.198, 5/1.297, 8/1.400, 10/1.444 (Table 4.3); error without K: -11/-15/-20% at a/b = 1/2/3 (Table 4.2)Source, quote & tabletop applicability
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
Tabletop: The non-circular correction handbooks skip - and a ready-made margin policy; computing wide flat gaps (a/b 5-10, K~1.3-1.44) without K builds in ~30-45% pumping headroom automatically.
-
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 & tabletop applicability
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
Tabletop: With the duct rule, this is the complete kit for a chamber conductance budget - every baffle hole, dee mouth and internal constriction on the reference machine or a next machine reduces to a 75A element in the network.
-
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 & tabletop applicability
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
Tabletop: 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). Amateur systems routinely lose the same 40-60% to geometry; budget from the source outward, not the pump inward.
-
Perforate internal RF structures - dee back, stub-line walls, internal bracing - wherever structurally and electrically tolerable, so the enclosed volumes pump in parallel through many small paths instead of only through the dee mouth.
Source, quote & tabletop applicability
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
Tabletop: Dees are pumping dead-ends by construction - drilling the dee back and any stem shrouds (small holes, below RF-significant size) is free conductance exactly where the ion source dumps its gas.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The same arithmetic the builder runs with the MFC - P = Q/S plus pump ultimate. A 0.1-1 sccm hydrogen feed is 1.3e-3 to 1.3e-2 torr-l/s; divide by the honest effective speed at the chamber to predict running pressure before touching hardware.
-
Hydrogen conductances are sqrt(29/2) ~ 3.8x air values, but diffusion-pump speed for hydrogen at low pressure is only slightly above its air speed - so when the system is pump-limited rather than conductance-limited, the hydrogen bonus does NOT raise net speed appreciably.
S_H2/S_air = sqrt(M_air/M_H2) = sqrt(29/2) ~ 3.8 (conductances only)Source, quote & tabletop applicability
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
Tabletop: 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) is the bottleneck for H2 specifically.
-
Bound pump-down expectations analytically before build: their 15,000-liter chamber roughs 760 mm Hg -> 45 microns in 30 min, finishes 45 microns -> 4e-6 mm Hg in 3 min (33 min total, leak-free and outgassing neglected), and recovers from a 1e-3 mm Hg gas burst in seconds - 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 & tabletop applicability
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
Tabletop: The calculation pattern transfers at 1/1000 the volume - compute the ideal V/S time for the next machine's chamber; if observed pump-down is many times the ideal, the excess IS the outgassing/leak signature, a diagnostic the reference machine's logs can use today.
-
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; and all flexible connections go in VERTICAL pipe runs so oil cannot pool in them.
Source, quote & tabletop applicability
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
Tabletop: Both bites transfer verbatim to a garage system - an automatic vent on the roughing pump (or a check valve) prevents the classic oil-suckback chamber contamination, and bellows belong in vertical runs.
-
Give the vacuum system an automatic fault sequence keyed to forepressure interlocks (diffusion heaters off and high-vac valve closed at 50 microns forepressure; booster blocks at 160 microns), with thermal switches on pump casings, and cross-connected backing lines normally valved off so any surviving backing pump can serve all diffusion pumps.
Source, quote & tabletop applicability
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
Tabletop: 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 save an unattended amateur system.
-
Weld all direct vacuum connections; 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 two gaskets (permits leak checking the joint and guarding the inner seal).
Source, quote & tabletop applicability
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
Tabletop: The double-O-ring-with-interspace-pumpout trick is worth stealing for any large troublesome amateur flange (chamber lids especially) - the interspace can be sniffed for leak location or held at rough vacuum to null permeation across the inner ring.
-
Split a deflector/extraction trigger into two stages: a frequency-sensitive circuit that GATES, and a phase-sensitive circuit that TRIGGERS - because no frequency measurement can be accurate enough to also fix the RF phase of the firing instant.
Source, quote & tabletop applicability
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
Tabletop: The architecture for any timed kick against an extraction gap, on a next machine or a small synchrotron - a coarse condition (frequency, turn count, integrated field) opens a window, and the RF itself supplies the fine phase. Two easy measurements replace one impossible one.
-
To detect when a swept RF reaches a chosen frequency, do not build a stable tunable RF filter (it cannot be built stably enough); heterodyne the RF against a crystal local oscillator and detect the transient through a FIXED low-frequency band-pass filter, making the trigger point variable via the low-frequency side and crystal switching.
trigger when f_dee - f_crystal = f_filter (~1 Mc); variable 1-1.25 Mc filter + switched crystals covered 19-21.5 McSource, quote & tabletop applicability
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
Tabletop: Classic measurement doctrine - move precision to a fixed low frequency where stability is cheap. The same trick (mix dee RF down, detect at fixed IF) is how a modern amateur frequency/turn marker gets crystal accuracy with junk-box filters.
-
Enclose every frequency-critical element - crystals, oscillator tubes, and the band-pass filter components - in a thermostated oven set at the crystals' turnover temperature (140 F here), yielding one part in 10,000 frequency stability from ordinary parts.
crystal oven at turnover temperature -> df/f ~ 1e-4 (+/-2 kc at 20 Mc)Source, quote & tabletop applicability
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
Tabletop: The stabilization pattern transfers even where the parts are now silicon - put the reference AND the analog discrimination components in one controlled thermal box; the filter drifting is as fatal as the oscillator drifting.
-
It is theoretically impossible to filter a transient without introducing time delay - so do not fight detection delay, MEASURE it and compensate at the trigger threshold (they bias the trigger to fire earlier on the pulse rise).
Source, quote & tabletop applicability
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
Tabletop: General fast-timing wisdom for beam-pulse and kick timing chains - every smoothing stage costs latency; calibrate the chain end-to-end and remove the constant part in the threshold or delay setting rather than chasing zero-delay filters.
-
A swept signal peaks in a band-pass filter LATER than the moment it crosses the filter's center frequency, by a delay depending on filter bandwidth and sweep rate - so trigger calibration must be repeated per sweep rate (they provide a per-repetition-rate bias switch).
peak delay = f(filter bandwidth, df/dt of sweep); their sweep ~2500 Mc/sSource, quote & tabletop applicability
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
Tabletop: Matters wherever a resonant pickup watches a changing frequency - including a synchrotron RF ramp or an FM-tuned marker on a cyclotron; if the ramp rate changes, the timing calibration silently moves.
-
Reference a trigger threshold to the MEASURED critical firing voltage of the actual trigger device, not to ground - find the just-fires bias experimentally ("slide" it up until firing starts), lock it, and make all compensating adjustments relative to that point, so device aging drops out.
Source, quote & tabletop applicability
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
Tabletop: A self-calibration idiom worth copying into any comparator/discriminator in the DAQ - trim to observed threshold at session start (their multivibrator = today's comparator with drifting offset), and slow drift stops moving the physics timing.
-
Gain-stabilize a sparse narrow-pulse chain with a PEAK-reading automatic level control (average- reading AGC fails because the duty cycle is tiny), and put its detector at the FINAL trigger point so the loop compensates every gain stage at once, whatever the drift source.
Source, quote & tabletop applicability
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
Tabletop: Directly applicable to pulse chains fed by beam pickups or PMTs at low rep rate - stabilize on detected peak height at the discriminator input, and amplitude drift stops translating into time walk.
-
Suppress an unwanted (image) response by DISABLING the circuit during the time window when it occurs, rather than by building sharp switchable filters - simple time-gating was chosen precisely because high-frequency switching circuits invite unforeseen trouble.
Source, quote & tabletop applicability
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
Tabletop: A complexity-avoidance rule with 2026 force - blanking a known-bad time window (one line of firmware now) beats analog cleverness whenever the artifact's timing is predictable.
-
Benchmark for a home-built trigger discriminator, vacuum-tube era: from a 3 mV rms sample of the dee RF (50 ohm), fire within <1 microsecond of the chosen frequency on a 2500 Mc/s sweep, delivering 7 V / 1.2 us / 0.2 us-rise pulses into 73 ohms - achieved with 27 ordinary tubes.
input 0.003 V rms/50 ohm; output 7 V pk, 1.2 us, 0.2 us rise, 73 ohm; probable firing error <1 us; range 19-21.5 McSource, quote & tabletop applicability
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
Tabletop: Calibrates ambition - microsecond-class event timing off a tiny RF sample needed no exotic parts in 1952; any modern comparator + MCU implementation should beat it by orders of magnitude, so the architecture (not the hardware) is the thing to copy.
-
For a coil of fixed design (geometry ratios and current-density distribution), field scales with the linear size: h/(f*r0*j0) is invariant, so H ~ r0 at fixed j0 - but power and conductor volume both grow as r0^3. Field is cheap in the small and ruinous in the large.
h/(f*r0*j0) = design constant; P ~ h^2*rho*r0/f * const; V_conductor ~ r0^3 (Eqs. 1-2)Source, quote & tabletop applicability
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
Tabletop: SCALE-SCOPED (megagauss context) but the scaling itself is exact and explains amateur economics - it is why small bore air-core inserts and compact analyzing magnets are feasible while whole-machine air-core fields are not.
-
Match design effort to field class: near ~1 kilogauss, air-core coil power is small and complicated optimization is seldom worthwhile; only toward 1e5 gauss and above do power and maximum current density dominate and elaborate current-distribution designs (j ~ sin(theta)/r^2 kernels) pay.
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 & tabletop applicability
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
Tabletop: Locates amateur work far below the exotic regime - for sub-kG correction coils, steering windings and test solenoids, wind the simple thing; sophistication buys nothing until iron saturates and fields climb an order of magnitude.
-
Build and run a scale model of the RF system before committing to the full assembly: the 3/4-scale oscillator delivered the dee-voltage-vs-frequency curve, tuning-capacity range, drive power (75 kW at 12.5 kV, 50% duty) and the 27% efficiency figure that changed the final tube count - all before full-scale metal was cut. Frequencies scale as 1/size; their limits ran 5% off for the scale factor used.
model resonant frequencies ~ 1/scale (their 3/4-scale limits were 5% high for the scale factor used)Source, quote & tabletop applicability
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
Tabletop: 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.
-
Hunt and kill parasitic RF modes on the model, not the machine: identify the unwanted mode's frequency (a capacity-loaded half-wave resonance at ~50 Mc here), then suppress it by strapping the tube grids to points on the resonator AND loading the mode with a small coupling loop tuned to it.
Source, quote & tabletop applicability
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
Tabletop: Both suppression tools are amateur-accessible - a strap that shorts the parasitic mode's voltage pattern without disturbing the wanted mode, and a loop selectively coupling the parasite into a lossy load; relevant the moment the LDMOS upgrade raises the reference machine's gap voltages.
-
For a uniform field from a split coil pair at significant field strength, use coils whose cross sections are comparable to their radii squared - thin-winding Helmholtz pairs waste power - and set uniformity by a power-series expansion of the mid-plane field, choosing coil boundaries to null the 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 & tabletop applicability
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
Tabletop: Marginal for the cyclotron itself, but the right doctrine for any air-core uniform-field fixture - probe-calibration coils, a beamline corrector, or a small synchrotron's reference field - when tens of gauss or more are wanted continuously.
-
Derive an FM (frequency-vs-time) program from the constant-ion-phase condition and measured oscillator data rather than seeking an exact law - the required variation "is not very critical" - and mind the duty cycle: the return to start-of-cycle should take no longer than the acceleration time, since extra return time directly wastes average beam current.
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 & tabletop applicability
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
Tabletop: Synchro-only for cyclotrons, but the pattern maps onto a small synchrotron's RF ramp - program tolerance is loose if phase stability (not exactness) is the criterion, and cycle dead time is a direct beam-current tax.
-
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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: this is a 730-MeV 1-uA machine; at <1 MeV protons the spallation and (p,xn) channels behind it are closed and material activation is a non-issue. The principle activates only if the reference machine ever makes neutrons (d-D, p-Li) or exceeds a few MeV — then bake material choice in early, because it cannot be shielded in later.
-
Different structural metals leave different residual-nuclide inventories under the same irradiation: aluminum gives only 15-hr Na24 (dead in days); iron ends up 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 then 71-day 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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: nuclide-by-material bookkeeping from 730-MeV spallation; every one of these production channels is closed at sub-MeV proton energy. Value to the builder is the pattern — inventory follows alloy content (Ni -> Co58, Cr -> Cr51) — worth knowing when reading other labs' activation numbers or planning any future >MeV or neutron-producing work.
-
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 & tabletop applicability
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
Tabletop: The one activation rule that DOES apply 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 null check that sub-MeV operation activates nothing — useful evidence for licensing conversations and for catching surprises if beam or species ever changes.
-
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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: relevant only when neutrons exist to be moderated. Standard Cd-difference technique to keep in the toolkit for any future neutron-producing experiment; meaningless for pure sub-MeV proton running.
-
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 & tabletop applicability
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.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 18
Tabletop: ENERGY SCOPE: a sub-MeV reference machine or next machine produces no residual gamma fields to shield; 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 Pb around a NaI detector against room background (0.6 cm/HVL at 662 keV Cs-137 scale).
-
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 & tabletop applicability
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
Tabletop: Energy-independent technique. A 2-in lead collimator with a removable plug around a next machine's NaI turns it into a pointing instrument for finding X-ray leaks (RF multipactor, dee-liner discharge bremsstrahlung) on a running machine — the same aim/plug/subtract discipline at keV instead of MeV.
-
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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: Crocker's 10-24 MeV/nucleon beams at tens of uA made 100-500 r/hr targets; the sub-MeV reference machine makes none. But the instrument discipline transfers exactly: a logged GM/ion-chamber channel at the machine (the builder already logs Keithley current) gives prompt X-ray dose during RF conditioning and a defensible record for licensing.
-
Treat handling time as the primary dose control and choreograph it: target setup ~3 min, removal ~1 min, dismantling <1 min behind a 2-in lead-glass bench shield; crew practice alone cut average exposure from 0.165 to 0.1 r/man/week while workload rose.
dose = rate x time; Crocker trend 0.165 -> 0.1 r/man/week (1953-57) despite >1000 target changes in 1957Source, quote & tabletop applicability
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
Tabletop: ENERGY SCOPE: the r/hr numbers are 20-MeV-machine numbers. The practice — rehearse any hands-on task near a hazard until it is a one-minute drill, and put a simple bench shield where hot items are worked on — is the cheapest safety hardware there is, and applies verbatim to a next machine's HV, RF, and any future activated-target work.
-
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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: measured on multi-MeV activated targets. Transferable geometry lesson at any scale: dose goes as 1/r^2 and the hands are at r ~ 0; if the reference machine or a successor ever handles activated or tritiated items, tongs and a ring dosimeter are the response, and the same 1/r^2 logic governs hands near an energized RF dee stem.
-
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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: deuteron (d,n) activation at tens of uA and ~20 MeV; no sub-MeV analogue. Keep the scheduling pattern: batch the nastiest operations (SF6 handling, HV conditioning, any future neutron work) into planned windows with a defined stand-down, rather than interleaving them with routine bench time.
-
Expect the internal/in-vacuum components that the beam actually strikes to be the hottest objects in the building — Crocker probe targets and the exit strip read >10,000 r/hr against ~500 r/hr for the deflector — 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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: 10-24 MeV activation levels, closed channels below 1 MeV. The design ordering survives: whatever intercepts full beam (probe tip, Faraday cup, B11 target holder) concentrates all consequences — on a next machine that means heat and sputtering now, and would mean activation first if energy ever climbs.
-
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 & tabletop applicability
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
Tabletop: Boron is among the worst common elements to evaporate (needs ~2000 C+, attacks refractory-metal boats); carbon-rod stock is cheap and machinable with ordinary tooling. This is the boat design to copy for making B-11 films for the next machine's B11(p,alpha) experiment — the recipe is isotope-blind.
-
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 & tabletop applicability
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.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 6
Tabletop: Numbers verified on the page image. Scope honestly: this is EVAPORATION producing research-grade ug/cm2 self-supported films — exactly right for a p+B11 cross-section or resonance-yield measurement, and NOT the route to a thick sputtered/pressed target for a maximum-alpha-yield demo. 2.2 kW low-voltage supply and a 1e-5 torr bell jar are amateur-reachable.
-
Budget boron-evaporation boats as consumables — the slot clogs with boron carbide and a boat survives at most two evaporations — so machine boats in batches before a target campaign.
boat life <= 2 evaporations (B4C clogging)Source, quote & tabletop applicability
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
Tabletop: Hot boron converts the carbon boat itself to B4C — no boat material choice fixes this, it is stoichiometry. Plan the enriched-B11 evaporation campaign around several pre-machined boats and one plate per boat-load rather than debugging mid-run.
-
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 & tabletop applicability
the method found successful here was to float the boron off the plate with warm tap water.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 6
Tabletop: The entire film-recovery toolchain is kitchen-grade (dishwasher detergent, tap water, glass plates) — the skill is in the sequence, all of which is written down here (pp.6-8). Practice on natural boron before spending enriched B-11.
-
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 & tabletop applicability
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
Tabletop: For a next machine's B11(p,alpha) internal-target experiment a 50-100 ug/cm2 film costs ~2-4 keV of proton energy loss at 170 keV — thin enough to sit on or near the 675-keV-resonance tail measurements' energy-definition budget while being mechanically survivable. Double-fold is the practical sweet spot.
-
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 & tabletop applicability
increasing the current slowly over a period of 10 to 20 minutes so that the outgassing can occur quietly.
Hoke & Newman, Self-Supported Cyclotron Targets of Boron and Magnesium — ORNL-3021 (1961) — p. 9
Tabletop: Three generalizable tricks for any future target work — sacrificial carbon parting layers under fragile or reactive films, slow-ramp outgassing before full evaporation power, and a cheap glass hood (lantern-slide covers) so expensive enriched material can be scraped back and reused.
-
Never quote an internal-target beam energy from the B-rho calculation alone: the one lab that checked (ORNL 86-inch) measured deviations up to +/-10% from the H-rho value, and the energy of maximum intensity moved several hundred keV under MINOR changes 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 & tabletop applicability
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.
Tabletop: Verified on the page image, and 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. 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.
-
Measure internal-beam energy with photographic film behind a stepped absorber folded from aluminum foil: expose ~0.1 uA-sec (arc OFF, source-off current control, field deliberately detuned to throttle intensity), 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 & tabletop applicability
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.
Tabletop: At 150-170 keV protons the ranges are ~2-3 um Al, so foil steps become thin-film steps or the film is swapped for the next machine's PIPS behind a stepped degrader — but the architecture (stepped absorber + position-resolved detector + uncovered reference channel) and the arc-off/detune trick for nA-friendly intensity carry over directly. The film variant also maps radial beam width vs energy for free (p.9).
-
Know the accuracy floor of any absorber-based energy measurement: range-energy data and straggling limit the most-probable-energy determination to a few hundred keV, the high-energy edge of the distribution is nearly as good, but the LOW-energy side of the spectrum is largely unrecoverable.
Source, quote & tabletop applicability
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
Tabletop: Scale the absolute numbers down with energy, but keep the shape of the claim — quote the high-energy edge with confidence, treat the low-energy tail as semi-quantitative. Same asymmetry applies to a PIPS-plus-degrader spectrum on a next machine, and to interpreting any resonance-yield curve taken with a spread beam.
-
Turn a known activation excitation function into a beam spectrometer: bombard a stack of thin foils (Cu, ~6 mg/cm2) whose reaction — Cu63(p,n)Zn63, 38-min — is well measured, count each foil, and unfold activity-vs-depth into the energy spectrum; because the cross section drops steeply, the linear system is near-triangular and solves foil-by-foil in ~30 minutes.
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 & tabletop applicability
the energy distribution of protons in the cyclotron beam is readily determined by measuring this excitation function and comparing it with the published data.
Tabletop: ENERGY SCOPE: Cu63(p,n) threshold is ~4.2 MeV — closed on the reference machine and a next machine, so this exact reaction cannot be used below ~4 MeV. The transferable idea is using a steep, well-known excitation function as an energy discriminator: at a next machine's energies the B11(p,alpha) yield curve itself (or Al/Ni step degraders before the PIPS) plays that role, and the same triangular-unfolding trick applies to any stacked measurement.
-
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 & tabletop applicability
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.
Tabletop: Directly relevant methodological honesty for a next machine, where detector protection will likewise force attenuated or detuned beams for some measurements. Log the machine state (dee voltage, field, frequency, source position) alongside every energy measurement so diagnostic-mode and run-mode data are never silently mixed.
-
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 & tabletop applicability
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
Tabletop: ENERGY SCOPE: C12(p,pn) needs ~20 MeV — the counting scheme is closed below threshold. Keep the geometry, swap the readout: a probe-tip mosaic of insulated segments read as Faraday collectors (or a scorched-film/thermal-paper witness at nA-uA-sec fluence) gives the reference machine and a next machine the same one-shot 2-D map of where the internal beam actually lands — directly useful for placing the B11 target and sizing its hot spot.
-
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.
dr/r = 2*dE/E; dE = 4*V0*cos(theta) => theta = acos(E*dr/(2*r*4*V0)); measured (dr", Vd-d kV, theta_min) = A(0.29, 315, 60), B(0.19, 315, 72), C(0.22, 240, 60), D(0.40, 335, 50)Source, quote & tabletop applicability
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
Tabletop: Table verified on page image. Energy-independent physics: on the reference machine or a next machine a differential probe (shadowed double tip) or the sectioned-target map gives dr, and with the known dee voltage that is a measurement of ion RF phase — the quantity a next machine's 5-G field tolerance is protecting. A rare direct experimental handle on phase for machines with no beam-position monitors.
-
Control the ion-source ground connection deliberately — an ungrounded source floats toward the accelerating-slit (dee) potential, substantially changing the first-gap optics and widening the measured turn spacing toward no-slit theory; a floating source is a different machine configuration, not a small perturbation.
Source, quote & tabletop applicability
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.
Cohen, Spatial Distribution of Current on an Internal Cyclotron Target — ORNL-1348 (1952) — p. 9
Tabletop: Direct lesson for the reference machine's central-region debugging — the source body's DC potential is a real optics knob (or a real gremlin). Verify the filament/chimney ground path is defined and logged; an intermittent source ground would masquerade as day-to-day beam irreproducibility of exactly the kind ORNL-1347 warns about.
-
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 & tabletop applicability
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
Tabletop: Explains an observation class on the reference machine: probe current can look tolerant of field/frequency error while the beam's phase (and thus its energy at radius) shifts underneath — reinforcing ORNL-1347's rule that current on target is not evidence the energy is what B-rho says. Phase self-selection also broadens resonance-tuning curves; do not read their width as the true stability margin.
-
Set beam energy as an explicit compromise among cost, the physics value of higher energy, and the fraction of beam you can extract; set current from what the research program actually needs after resolution cuts.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Scale-free requirements-hierarchy discipline; the same three hard requirements (isochronism/weak-focusing law, focusing, power) apply verbatim to any cyclotron magnet trade.
-
Before committing to the full machine, build a cheap scaled analogue whose stated purposes are to test practicability, to reveal unexpected phenomena, and to demonstrate the single riskiest subsystem.
Source, quote & tabletop applicability
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
Tabletop: The electron-analogue idea (keV electrons stand in for MeV protons at equal T/mc2) is itself 810-MeV-motivated, but the three-purpose charter for any risk-retiring model or prototype is scale-free.
-
When rejecting alternatives in a trade study, enumerate each one's specific defects in writing rather than just naming the winner.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
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).
a*vr + b*vz = n; n = N gives essential resonancesSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Put the field-critical dimensions on iron geometry rather than on coil placement, plan from the outset to shim the finished magnet, and build adjustability into the trim-coil design to minimize shimming.
Source, quote & tabletop applicability
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
Tabletop: Directly scale-free: machined iron holds tolerance far better than wound copper at any size, and 'shim if necessary' should be a scheduled step, not a failure mode.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Match power-supply regulation quality to each coil's fractional contribution to the field: coils contributing under ~1% can share one regulated source with resistor trims; anything above that gets its own precision-regulated supply.
regulation stability ~ (field tolerance)/(coil's fractional field contribution)Source, quote & tabletop applicability
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
Tabletop: Scale-free budgeting rule (from the Analogue, a 42-gauss machine): spend regulation money in proportion to field contribution — main coil tightly regulated, trim/harmonic coils on cheap trimmed sources.
-
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 & tabletop applicability
Gap tolerance +/- 0.004 in.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 137
Tabletop: 810-MeV provenance: this is the spec for a 53-ft isochronous magnet with 4-in beam aperture; the transferable content is the relative-tolerance framing (fraction of gap), consistent with the next machine's 5 G / 5-deg-phase field-error budget, not the absolute mils.
-
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 & tabletop applicability
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
Tabletop: 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; treat resonator design as constrained cut-and-try — fix the dimensions the machine dictates, then adjust the free variables to a documented compromise (voltage-holding vs transit time; power loss vs volume).
Source, quote & tabletop applicability
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
Tabletop: Fully scale-free method: a dee-stem system is likewise a transmission line with machine-fixed dimensions and a few free ones; name each spacing's compromise pair when sizing the next machine's 5-13 kV dee.
-
Build a scale model of the resonator primarily to validate the design method: compare predicted vs measured frequency and Q, chase discrepancies to their cause, and use the same model to check for unexpected higher-order modes.
Source, quote & tabletop applicability
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
Tabletop: Scale-free: their 1/12-scale model both certified the three-step-line calculation (4% agreement) and caught a build error; a bench mock-up of a next machine's dee/stem before the LDMOS amp arrives serves the same double duty.
-
Budget RF power as computed resonator loss plus beam loading plus an explicit named contingency line (~20-25%), and provide driver capability several times the computed drive requirement.
P_total = P_cavity + P_beam + P_contingency (here 500 + 160 + 200 kW)Source, quote & tabletop applicability
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
Tabletop: The kilowatts are 810-MeV numbers; the budget structure — separate lines for copper loss, beam load, and contingency, plus >=4x drive reserve — sizes a next machine's 100-500 W LDMOS chain honestly.
-
Select the amplifier-to-resonator coupling by its behavior during a spark: prefer a scheme where a cavity arc reflects a load that reduces tube current, over-rate components against the unloaded-amplifier voltage rise, and layer protection (fast drive removal for routine faults, crowbar for tube-saving ones).
Source, quote & tabletop applicability
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
Tabletop: Scale-free fault-mode-first design: dees spark at every scale, so choose a next machine's amp coupling and protection for arc behavior, not just matched-condition efficiency — directly relevant to protecting an LDMOS pallet.
-
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 & tabletop applicability
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
Tabletop: Directly usable on the reference machine now: a dee-voltage threshold scan vs radius separates center-region problems from field-error problems with no new hardware.
-
Size the pumping system from the outgassing load rather than the volume, derate installed pump speed to ~25% of mouth speed for baffles and valves, and treat published outgassing data as conservative by up to an order of magnitude in early pumpdown.
S_net ~ 0.25 * S_mouth; Blears data vs measured: ~20x high at 1 hr, ~2x at 20 hrSource, quote & tabletop applicability
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
Tabletop: Scale-free sizing doctrine (their 2.6e6-liter tank is not): the 25% derate and outgassing-dominates logic apply verbatim to any diff-pumped chamber, including the reference machine's SI100 system.
-
Set seal policy by radiation dose and replaceability: metal seals wherever dose is high or replacement is difficult; elastomers only where predicted lifetime dose is acceptable and the seal is easy to change; pump the interspace of large double-elastomer seals.
elastomer allowed where 10-yr dose < 1e8 rad AND easily changed (their criterion)Source, quote & tabletop applicability
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
Tabletop: The 1e8-rad number is their 810-MeV flux environment; 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.
-
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 & tabletop applicability
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
Tabletop: At 150 keV protons (v ~ 5e6 m/s) the comparison runs the other way — modest electrostatic septum fields are equivalent to impractical coil fields — so amateur-scale extraction stays electrostatic; do this arithmetic before copying any big-machine magnetic channel.
-
Before believing an internal-probe beam-attenuation curve, rule out probe-edge scattering: compare probes of different materials and keep particle range in the probe small compared with the radial beam width.
artifact severe when (range in probe)/(radial beam width) >~ 1Source, quote & tabletop applicability
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
Tabletop: Direct transfer to the reference machine's probe/Faraday-cup work: an apparent current fall-off with radius can be instrumentation, not physics — swap probe material (their Al vs Ta test) before redesigning the machine.
-
In weak-guide-field machines or field regions, cancel the ambient (geomagnetic) field components; an uncompensated horizontal component can drive coupling resonances and eat the beam.
Source, quote & tabletop applicability
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
Tabletop: Their Analogue ran at 42 gauss central field, where Earth's ~0.5 G matters; irrelevant inside the reference machine's 0.59-T gap but real for any low-field electron-analogue experiment or long low-field injection path.
-
Investing in a well-collimated, well-defined injected beam pays off downstream: resonances that attenuated the poorly defined beam were traversed cleanly once injection quality improved.
Source, quote & tabletop applicability
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
Tabletop: Scale-free: central-region collimation and source definition (a planned source-species test on the reference machine) buy margin against every downstream loss mechanism; fix beam quality at birth, not at radius.
-
Assume your shielding estimate will prove low and your experiment space too small; design margin and expansion room in from the start because every predecessor facility needed both.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
Design shielding so the stricter general-population dose limit (10x below occupational) is met in all regularly occupied adjacent areas, even when regulations would let you use worker limits.
design limit = occupational MPD / 10 in inhabited adjoining areas (their practice: 5 rem/yr worker, 0.5 rem/yr public)Source, quote & tabletop applicability
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
Tabletop: Directly transferable posture for a residential-basement machine: the family upstairs is 'general population'; design to the public limit at occupied locations, not the worker limit.
-
Build the shield estimate as an explicit chain — dose limit, source term, attenuation, secondary buildup — and at each approximation record which direction the error runs, keeping the net conservative but only to within the precision of the input data.
Source, quote & tabletop applicability
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
Tabletop: Scale-free methodology (their 810-MeV cascade physics is not): a next machine's neutron estimate should carry the same per-step conservatism bookkeeping — deliberate, directional, and not stacked beyond what the data precision justifies.
-
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 & tabletop applicability
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
Tabletop: At amateur energies the split maps to fast neutrons (thickness/moderation) vs capture gammas and activation (materials choice near the target); the sort-by-question habit is scale-free.
-
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 & tabletop applicability
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
Tabletop: Scale-free research method, and a pointer: reactor-shielding texts (Price, Horton and Spinney 1957) remain the right source for any amateur duct/labyrinth question the accelerator corpus lacks.
-
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) (~0.1 per 90-deg bend with an extended 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 & tabletop applicability
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
Tabletop: The transmission algebra is for low-energy neutrons and is scale-free; their 27-ft legs are not. Any next-machine cable/utility penetration or entry labyrinth can be sized with exactly this product-of-elements method.
-
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 & tabletop applicability
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
Tabletop: Scale-free insurance move that costs nothing at design time — pairs with the 'initial shielding always proves inadequate' rule above.
-
Use stepped (labyrinth) joints on shield doors and plugs so ordinary construction tolerances are acceptable, and compensate any thickness lost to mechanisms (wheels, tracks) with locally denser material.
Source, quote & tabletop applicability
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.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 206
Tabletop: Their 800-ton plug is 810-MeV scale; the stepped-joint principle sizes down directly to block-wall doorways and removable concrete/poly plugs around a benchtop target station.
-
Trade shielding construction methods on delivered cost per attenuation: their study found solid low-strength concrete walls cheaper (about 2/3 the cost) than cored walls with compacted rock fill, and earth-over-arch the cheapest roof.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
Structure a project estimate as basic cost plus explicit adders: engineering ~15% of basic, contingency averaged ~20% but assigned per item from 15% to 40% according to estimate precision, and escalation per year of schedule.
total = basic * (1 + ~0.15 eng) + per-item contingency (15-40% by precision) + escalation (their 4%/yr)Source, quote & tabletop applicability
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
Tabletop: 1963 AEC percentages, but the structure transfers whole to any bill-of-materials estimate: contingency is not one number — catalog items get little, anything not yet fully designed (their rf cavity: 30%) gets a lot.
-
Ground every major cost line in evidence — several vendor bids with the median taken, catalog prices, or a documented past purchase — and sanity-check derived unit prices against what was actually paid for the nearest precedent, explaining any difference.
Source, quote & tabletop applicability
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
Tabletop: 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').
-
Design and cost probable future additions now, provision the interfaces, but keep their cost out of the baseline project.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
Put scheduling detail where the novelty is: network-plan (CPM/PERT) the machine and beam systems yourself, and leave conventional construction to the contractor's own planning.
Source, quote & tabletop applicability
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
Tabletop: Scale-free effort allocation: plan the risky subsystems (source, RF, field mapping) at fine grain; the workshop-and-bench logistics need no Gantt chart.
-
Treat the first schedule as a hypothesis: when the critical path gives an unacceptable duration, re-examine every activity on it — add resources or shifts, and resequence so long-lead assembly (magnet in the vault) overlaps remaining construction — then recompute.
Source, quote & tabletop applicability
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
Tabletop: Scale-free (their iteration cut 8yr10mo to 6yr9mo); note also what sat on their critical path: magnet iron, field plotting, and 'shim if necessary' — field mapping is schedule, not an afterthought, at any scale.
-
Resolve individual turns with a thin radial wire probe: a 0.020-in. tantalum wire scanned from 1.2 to 11.5 in. showed distinct current maxima for orbits 1 through 12, spaced 5/8 in. for inner orbits at high dee voltage — turn spacing measures real energy gain per turn, and the resolvable-orbit count is set by dee potential (22-inch test cyclotron).
turn spacing dr per turn ~ r*(dE/E)/2; resolved orbit limit set by dee voltageSource, quote & tabletop applicability
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.
Tabletop: Directly runnable on the reference machine with the existing probe hardware - measured turn spacing would convert the "~800 V nominal, uncalibrated" dee voltage into a calibrated energy-gain-per-turn number. Fig. 12 (PDF p. 41) shows the machine doing this at 9.2-12 kV dee-to-dee with 600 V dee bias.
-
Expect a spurious slow rise in wire-probe current with radius: proton bombardment heats the wire and thermionic electron emission adds to the collected current, growing with beam energy — separate this baseline from real beam structure before interpreting a radial scan (22-inch test cyclotron).
Source, quote & tabletop applicability
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.
Tabletop: Same artifact family as the reference machine's secondary-emission and background offsets on the Faraday cup; at nA scale a hot-wire thermionic term can dwarf the signal, so bias or shield the probe and log the baseline drift.
-
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 & tabletop applicability
A very effective adjustable beam deflector has been developed; under the best conditions, 38% of a 1000 ua internal beam has been deflected.
Tabletop: Sets expectations for any future extraction gate on a next machine - design the septum/deflector with in-vacuum adjustability and count a 30-40% extracted fraction as success on a first small machine.
-
Keep any dc injection potential below the dee voltage: with dees limited to 10 kV, injection potentials over 10 kV decelerated ions in the gap between the accelerating electrode and the dee; the fix was to raise the dee-side capability (redesign for at least 20 kV dee-to-ground) before raising injection further (22-inch dc-injection test unit).
V_inject < V_dee, else the electrode-to-dee gap deceleratesSource, quote & tabletop applicability
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.
Tabletop: Any reference-machine or next-machine source-bias or puller experiment must respect the same ordering - source extraction potential is bounded by the rf accelerating potential actually available at the first gap, or the first gap runs backward.
-
In a high-potential arc source for multiply charged ions, electrode alignment with the magnetic field is critical, and feeding gas collapses the mean electron energy by flooding the arc with low-energy secondaries — high arc voltage alone does not buy energetic electrons (ORNL fundamentals test source, 1-20 kV).
Source, quote & tabletop applicability
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
Tabletop: For the reference machine's filament source (and a planned source-species test) the lesson is that arc electron energy is gas-pressure-coupled - lowering flow raises mean electron energy, which shifts the H+/H2+ balance; align source slits to B before blaming the arc supply.
-
Ion-source output scales roughly linearly with effective slit length: two arc apertures of identical 3/32-in. width but 1/2-in. vs 2-5/8-in. length gave 35 vs 170 mA at identical arc (150 V, 2 A) and 10 kV extraction — to first order, lengthen the slit to buy current (22-inch cyclotron).
I_source ~ proportional to slit length at constant width, arc, and extractionSource, quote & tabletop applicability
The output of the ion source was found to be approximately proportional to the effective length
Tabletop: The reference machine's chimney-slit geometry is a free knob - but ornl-1339 (same machine, five quarters earlier) showed arc-slit LENGTH also feeds z-wise beam loss, so pair any slit lengthening with the z-distribution probe check.
-
Judge injector/source changes by transmitted beam at FULL radius, not by current near the source: near-probe current 1.5 in. out rose linearly to 8.5 kV injection while full-radius (10.5 in.) beam peaked at 1-3 kV — the divergence means the extra near-source current is badly focused and lost (22-inch cyclotron).
optimum V_inject (by full-radius beam) was 1-3 kV, arc-intensity dependentSource, quote & tabletop applicability
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
Tabletop: The reference machine's central tuning trap - a source tweak that fattens the inner-radius signal can starve the Faraday cup at full radius. Always score source changes at the outermost probe position.
-
Survey median plane and magnetic center with a floating current-carrying wire loop: a single #32 enameled loop at ~5 A dc, hung nearly friction-free, sits in unstable equilibrium at the median plane and self-centers on the magnetic center; loops of several diameters map the whole field (22-inch cyclotron).
Source, quote & tabletop applicability
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
Tabletop: A zero-cost magnet diagnostic for the reference machine or a next machine - enameled wire and a bench supply locate both the magnetic median plane (which need not be the geometric midplane) and the field center before any Hall-probe mapping campaign.
-
Acceptance numbers for a small-machine magnet survey: on the 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 & tabletop applicability
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"
Tabletop: Direct pole-scale match to the reference machine (8-in. poles) - an eighth-inch median-plane and quarter-inch centering tolerance were good enough for a working ORNL test machine; ornl-1345's B-sweep species analysis on this same machine presumed exactly this alignment quality.
-
Check dee-voltage clearances OUTSIDE the vacuum tank too: the rebuilt 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; a portable oscillator was built specifically so it could be direct-coupled to the dee stems (ORNL ion-source testing unit).
Source, quote & tabletop applicability
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
Tabletop: For the reference machine's LDMOS upgrade toward 5-13 kV dees, walk the whole rf path in air - feedthroughs, stem gaps, coupling hardware - because atmospheric-side spark gaps, not vacuum gaps, set the first ceiling.
-
Name and grow the machine around its magnet: the 1949 test cyclotron was called the "22-inch" for its maximum orbit; when a rework raised its ambitions, ORNL renamed it the "44-inch" after its pole diameter — the pole iron is the durable identity and investment, while orbits, dees, and rf are replaceable stages (44-in./22-in. test cyclotron).
Source, quote & tabletop applicability
Inasmuch as the equivalent diameter of the pole pieces is 44 in., the machine is more appropriately identified as the 44-in. cyclotron.
Tabletop: The reference machine's H-frame magnet is the analogous asset: energy upgrades (gap, shims, dees, rf power) can be staged around the same 757-lb iron for years, exactly as ORNL staged 1.5 -> 5 MeV -> (proposed) 48-in. heavy ions around one magnet line. Rename footnote: PDF p. 17.
-
DC accelerating-electrode geometry for a cyclotron source is an empirical search: geometries cannot be calculated (plasma boundary plus rf field), and of several dc electrode geometries tested on the 44-inch, NONE beat the standard rf accelerating electrode to full radius — budget for iteration and keep the plain rf gap as the benchmark.
Source, quote & tabletop applicability
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.
Tabletop: A caution for any puller-electrode or biased-extraction scheme on the reference machine - after four quarters of trials (ornl-1269 through -1531) ORNL's dc injection still lost to the ordinary rf gap; keep an unmodified configuration as the control in every source A/B test.
-
Shift the beam center electrically with "half-coils": an insulated conductor wrapped halfway around a pole piece (the pole completes the circuit) imposes a small uniform gradient; 600 A moved the 86-inch beam center 3.6 in. and swept fixed-target energy 18-23 MeV — a field-trim knob that steers orbits without touching iron.
600 A opposing half-coil set -> 0.5 oersted/in. gradient across an 86-in. poleSource, quote & tabletop applicability
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.
Tabletop: 86-inch numbers, but the trick scales - a few-turn half-wrap trim coil on a next machine's pole gives a first-harmonic/gradient control for orbit centering and effective-energy variation that FEMM can model directly; also a candidate cheap "variable-energy" feature for an educational machine.
-
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 & tabletop applicability
The extreme radioactivity induced in type 304 stainless steel makes its use undesirable, the use of an aluminum alloy is now being investigated.
Tabletop: At reference-machine and next-machine energies activation is negligible, but the selection logic transfers to the planned higher-power machines and to the business plan's licensing story - prefer aluminum/graphite for probes, septa, and slits anywhere protons above a few MeV are contemplated.
-
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 (via collimation plus magnetic analysis of the deflected beam) and 1-10 uA deflected current, at ~$1M 1953 cost — energy spread is fixed downstream, not in the machine.
energy definition < +/-10 keV via deflected-beam collimation + magnetic analysisSource, quote & tabletop applicability
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
Tabletop: Direct prior art for the plan's educational variable-energy accelerator concept - vary energy with field/frequency plus a movable target (cf. the 44-inch spacer), and buy energy DEFINITION with a simple analyzed beamline rather than machine perfection.
-
Braze beryllium (and similar hard-to-wet) targets in a vacuum furnace, not with flux: flux brazing left inclusions that impaired heat transfer and cost 40-60% of target efficiency as poorly bonded Be eroded; sandwiching 0.006-in. aluminum-silicon alloy and vacuum-furnace brazing gave 100% bonding without tinning (86-inch neutron targets).
0.006-in. Al-Si (11.5% Si) interlayer, vacuum furnace -> 100% bondSource, quote & tabletop applicability
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.
Tabletop: The corpus's targetry shelf is thin - this is a concrete bonded-target recipe. For a next machine's boron/beryllium targets on copper or aluminum backing, flux-free vacuum (or controlled-atmosphere) brazing with a thin Al-Si interlayer is the proven route to full-area thermal contact.
-
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 & tabletop applicability
a beryllium target is bombarded with protons, approximately 1 neutron for 50 protons is obtained.
Tabletop: 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.
-
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 & tabletop applicability
Since this circuit depends upon the electrical characteristics of the resonant dee system, it cannot be designed until these characteristics are determined.
Tabletop: 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.
-
One machine, two energies by mechanical reconfiguration: a removable 14-in.-class spacer (14.5 in. per ORNL-1670) between vacuum tank and dee faceplate shifts the dees and target so the working radius is 11 in. (1.5-MeV protons) or 20 in. (4.9-MeV), while the ion source position and orbit centering relative to the magnetic field never change (44-inch cyclotron).
fixed B and f; target radius 11 or 20 in. -> 1.5 or 4.9 MeV (E ~ r^2)Source, quote & tabletop applicability
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
Tabletop: Variable energy WITHOUT retuning B or rf - since E ~ r^2 at fixed field/frequency, a repositionable target (or dee assembly) gives an educational machine two calibrated energies for the price of one; the invariants to protect are source position and magnetic centering, exactly as ORNL did.
-
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 & tabletop applicability
The whole dee system is insulated from ground so that a bias potential may be applied to control ion loading.
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: 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 every millimeter given to voltage clearance is field (B ~ 1/gap) taken from energy. Decide dee voltage and gap in the same trade study.
-
Scaling datapoint - the revised ORNL 44-inch as specified: 44-in. dees, 6400 oersteds in a 13.5-in. gap, 9.7 Mc/sec, up to 100 kV dee-to-dee from a ~200-kW F-134 oscillator, 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, P_osc ~ 200 kW; E = 1.5/4.9 MeV at r = 11/20 in.Source, quote & tabletop applicability
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)
Tabletop: 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, scaled up in radius and voltage. Use it to sanity-check B-f consistency and to see what 100 kV (vs the reference machine's ~0.8 kV) buys in radius terms.
-
Develop cyclotron rf on an electrical model before metal is cut: the variable-energy oscillator study used an 8-ft section of the 63-inch dee-stem electrical model with capacitors simulating the dees, and selected a self-excited push-pull oscillator direct on the stems (two tuning controls, drive-insensitive frequency) from competing circuits tested on that model.
Source, quote & tabletop applicability
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.
Tabletop: 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.
-
Coupled-secondary (transmission-line) tuning works but watch the Q: a series coil-capacitor secondary magnetically coupled to the dee stems swept resonance 6-12 Mc, but the secondary's comparatively low Q made the dee-stem resonant impedance vary markedly across the band — tuning range and impedance flatness trade against secondary losses.
reflected impedance of coupled secondary shifts f0; low secondary Q -> impedance swings with fSource, quote & tabletop applicability
the resonant impedance of the dee stems varies markedly with the frequency due to the comparatively low "Q" of the secondary circuit.
Tabletop: 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; keep trim elements high-Q or mechanical.
-
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 & tabletop applicability
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
Tabletop: For a next machine's shim development (5 G ~ 5 deg rf phase target): 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 against an uncharacterized pole error. Also proof that hand tooling on installed poles was acceptable ORNL practice - no magnet disassembly required.
-
Outsource castings-and-weldments at your peril; keep leak-integrity parts in-house or design them repairable: ORNL sent liner, dees, and dee-stem housing to a contractor and made faceplates, stems, source, probe, and vacuum system locally — the contractor items came back late and defective (dee cooling-tube leaks "in very inaccessible locations", ORNL-1795 p. 19; liner delayed by "brazing errors", ORNL-1884 p. 19).
Source, quote & tabletop applicability
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
Tabletop: The three-report arc (1670 -> 1795 -> 1884) is this collection's cleanest outsourcing lesson - brazed/water-cooled vacuum parts are where contractors fail, and each failure costs a reporting period. For a next machine, buy simple machining, but keep brazing, leak-checking, and anything water-to-vacuum under your own torch, or specify inspection windows up front.
-
Commission at reduced energy and high current before running full energy: the 14.5-in. spacer's stated purpose was to let the rebuilt 44-inch operate at ~1.5 MeV "for test operation at very high proton currents" — shake down source, rf, and loading at low energy where activation and deflector stress are minimal, then remove the spacer for 5-MeV running.
Source, quote & tabletop applicability
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.
Tabletop: Mirrors a staged-gate development logic - plan a low-energy high-current commissioning configuration as a designed-in mechanical state, not an improvisation, so beam physics problems are separated from full-energy hazards.
-
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 on a capacitor, 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 & tabletop applicability
The error of the control in tuning the oscillator to the frequency of the secondary is of the order of 0.1%.
Tabletop: A 1954 peak-hold autotune implementable today in a microcontroller for the rf chain of the reference machine or a next machine - sweep the exciter, record the dee pickup peak, re-sweep and lock; 0.1% at 9 MHz is ~9 kHz, comparable to the tuning precision the next machine's 5-G field budget implies.
-
Design water-cooled dees so the cooling circuit is reachable: leaks in the contractor-built dees' internal water tubes sat in "very inaccessible locations", and repair required cutting windows through the dee side-walls and re-closing them by Heliarc (TIG) welding — assume cooling joints WILL leak and provide access or removable covers at the joints (44-inch cyclotron).
Source, quote & tabletop applicability
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.
Tabletop: If a next machine's dees carry water, route tubing so every brazed or welded joint can be reached, pressure-test the dee as a unit BEFORE it meets the liner, and treat a cut-window-and-reweld as a planned repair mode (it worked) - the recovery technique is as instructive as the failure.
-
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 & tabletop applicability
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%.
Tabletop: Calibrates expectations for a next machine - 5e-4 base-field uniformity is what sustained professional effort actually bought on 44-in. poles; set the shim budget assuming the ground pole delivers ~0.05% and the final trim to the 5-G target comes from shims, not from more grinding.
-
Build the model magnet for measurement access: the quarter-scale 114-inch model put the 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" — a model magnet's geometry should serve the probe and the shim swap, not mimic the final machine's orientation.
Source, quote & tabletop applicability
The pole tips are removable so that shims of any shape can be inserted readily.
Tabletop: 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. ORNL judged these features worth 14.4 tons of model.
-
Sliding rf joints: copper-plated stainless steel was the best material tested for a pneumatic-pressure movable rf contact, and at 100 A per lineal inch the joint held under a 10 degC rise with only 0.5 gpm of cooling water; once made, the joint was insensitive to contact (air) pressure (114-inch study).
~100 A/lineal in. rf current; <10 degC rise at 0.5 gpm; Cu-plated SS contactSource, quote & tabletop applicability
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.
Tabletop: 100 A/in. is a design allowable for any sliding or clamped rf contact (shorting planes, tuning bars) in a next machine's resonator - and the material lesson (plate the stainless with copper; bare SS is an rf resistor) applies at any scale.
-
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 & tabletop applicability
All other components of the present 44-in. cyclotron, oscillator, dee system, vacuum system, ion source, target-probe, and power supplies, would be utilized.
Tabletop: The strongest argument in this collection for clean interfaces between a next machine's subsystems (and for interface-control discipline generally) - ORNL could contemplate a heavy-ion machine for the price of iron and a tank because everything else unbolted.
-
Cantilever the whole dee system from the outer end of the dee stems, and put that single mounting on insulators: one support plane carries the entire resonant structure, so insulating one interface both defines the rf ground plane and permits dc dee bias — found satisfactory in initial inspections of the assembled 44-inch.
Source, quote & tabletop applicability
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.
Tabletop: The mechanical execution of the 1663 insulate-for-bias rule - for a next machine, one stiff cantilevered dee-stem mount outside the field region, isolated by insulators, is simpler than distributed insulated supports and keeps the bias feed and rf geometry clean.
-
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 & tabletop applicability
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
Tabletop: 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.
-
Design the rf for roughly twice the threshold voltage: the 48-inch conversion spec sets design dee-to-dee voltage at 200 kV against a 110-kV N5+ threshold (~1.8x), buying orbit-count margin, loading headroom, and species flexibility (proposed 48-inch heavy-particle cyclotron, Table 3).
V_design / V_threshold ~ 200/110 ~ 1.8Source, quote & tabletop applicability
Dee-to-dee r-f voltage (design), kv 200; Threshold voltage for N5+, kv 110 (Table 3, condensed)
Tabletop: Same margin philosophy as the 63-inch 75-vs-60-kV acceptance hold (ornl-1339) - for the reference machine's LDMOS upgrade, compute the threshold dee voltage for the intended turn count and buy amplifier/resonator headroom for ~2x it, not 1.1x.
-
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 & tabletop applicability
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.
Tabletop: Directly relevant to the plan's facility question and to any MeV-class educational machine - a basement corner with earth on two sides replaces feet of poured concrete, and siting next to existing utilities/controls is a cost line the ORNL study treated as seriously as the magnet.
-
Retire beam-dynamics risk with an electron-model machine: before committing to a 1-BeV proton AVF cyclotron, ORNL planned "an electron-model accelerator to be used in assessing the importance of imperfection resonances and the feasibility of their penetration" — electrons let you walk the same tune diagram at bench field, energy, and cost (1-BeV accelerator study).
Source, quote & tabletop applicability
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.
Tabletop: Historical validation of an electron-model approach and of risk-ordered development - when the open question is orbit dynamics (resonance crossing, field tolerance), a tabletop electron machine answers it before proton iron is bought. (Same page — Thomas-1938 AVF theory, ORACLE computing, MURA spiral sectors - sector focusing arriving in this collection's timeline.)
-
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 & tabletop applicability
The major components have been assembled and vacuum-tested (see Fig. 5).
Tabletop: Schedule realism for the next machine's campaign - a professional division with machine shops took four reporting periods from revision concept to vacuum test, and the long poles were exactly the ones a next machine faces (outsourced fabrication, field shimming, ion source). Halving subsystem count does not halve this arc.
-
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 & tabletop applicability
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.
Tabletop: DIRECT - this is the canonical two-stage architecture for any external line on a next machine. The optical condenser/analyzer analogy (illuminated slit as object) is the cleanest possible statement of why "focus first, analyze second" beats one clever magnet.
-
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 & tabletop applicability
A considerable amount of undesirable radiation will be produced by that part of the beam intercepted by the slit system.
Tabletop: DIRECT and cheap to honor at layout time, nearly impossible later. Even at 150-170 keV the slit is the hottest x-ray point on the line (thick-target bremsstrahlung at full beam power); a next machine should treat every defining aperture as a shielded component.
-
Prefer a strong-focusing quadrupole pair over a sector magnet for the condenser role: about 10x less space, at least 20x less iron/copper/excitation power, trivially simple straight-pipe vacuum, and - because the beam is undeflected - field and lens spacing can be retuned to maximize focused current without moving any downstream equipment.
Source, quote & tabletop applicability
the weight and power requirements would each be less than the corresponding sector-magnet requirements by at least a factor of ten.
Tabletop: 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.
-
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 is greater), and the horizontal angular spread is larger - so make the first quadrupole converge in the horizontal plane and design the doublet for a common (nonastigmatic) image.
Source, quote & tabletop applicability
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.
Tabletop: DIRECT design input for any next-machine transport modeling - the tracker should fit separate horizontal/vertical source points from measured beam profiles rather than assume a stigmatic waist at the extraction channel.
-
Size quadrupole aperture from the measured extracted-beam envelope with stacked margins: take the measured beam box (here 2 cm high x 6 cm wide), apply a 50% safety factor to get the design ellipse, then round the pole-defining constant up again (c^2 required 0.844 cm^2, built xy = +/-2.25 cm^2).
hyperbolic poles xy = c^2; effective aperture = circle of diameter 2a centered on axis; tangency of pole hyperbola to the 3:1 beam ellipse gave c^2 = 0.844 cm^2, built with a = 3 cm, c = 1.5 cmSource, quote & tabletop applicability
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
Tabletop: DIRECT method (not numbers) - measure the real beam first, then stack two explicit margins. A next machine's envelope must come from its own extraction simulations/measurements; the 50%-then-round-up discipline is what prevents an undersized bore discovered after winding.
-
Hyperbolic quadrupole pole profiles are not worth precision machining at this scale - the authors had custom milling cutters made to generate true hyperbolas and later concluded plain circular arcs would have been satisfactory.
Source, quote & tabletop applicability
Morley Machine Company, Rochester, N.Y., produced milling cutters conforming to this equation ... Subsequent work has shown that circular arcs would have been satisfactory.
Tabletop: DIRECT money-saver, stated as an explicit lesson-learned footnote in 1954 and standard practice ever since. A next machine's quads (if built) can use round stock or FEMM-checked circular-arc tips; spend the FEMM time on end effects, not profile exactness.
-
Use effective (not physical) magnetic length for quadrupole optics: measurements showed the effective length up to ~20% greater than the physical length (18.1 cm physical treated as 20 cm effective in the design).
l_eff ~ up to 1.2 x l_phys for these small-bore quads; all lens equations use l_effSource, quote & tabletop applicability
Measurements have shown that the effective length of the magnets is as much as 20% greater than the physical length.
Tabletop: DIRECT - for short quads the fringe extension is a first-order effect, not a correction. Modern practice: l_eff = l_phys + ~aperture radius; get it from the FEMM/tracker pipeline per magnet, and expect focal errors of tens of percent if ignored.
-
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 & tabletop applicability
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.
Tabletop: DIRECT - at a next machine's rigidity, transport-quad fields are hundreds of gauss at most, so air-cooled random-wound coils on unsaturated iron are the default. OCR trap - the text layer renders the B^1/2 exponent as B^2; page image verified B^1/2.
-
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. Size the winding with explicit margins: 5000 A-turns computed per kilogauss, designed for 6000.
NI = (10/(4pi)) * sum(l_i/mu_i) per gauss path integral; here NI = 5000 A-turns per kG, designed 6000; 3000 turns/coil ofSource, quote & tabletop applicability
the coils in each unit are connected in series since otherwise we would have extreme difficulty in maintaining uniform gradients.
Tabletop: DIRECT wiring doctrine for any home-built multipole - gradient symmetry comes from forced equal current, not matched resistances. The 20% ampere-turn margin and the use-the-wire-you-have coil design (surplus
-
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_saturation-limited; here 3.8e5 G-cm / 8 kG => 47 cm, built at rho = 49.7 cm, B = 7.6 kGSource, quote & tabletop applicability
For fields above about 8 kilogauss, saturation effects begin to set in, and the field becomes less uniform near the pole boundaries.
Tabletop: 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.
-
Correct wedge-magnet geometry for fringe field by shifting the effective pole boundary outward ~0.4 x gap (empirical term 0.4*G*(csc(gamma1)+csc(gamma2)) added to the pole-face spacing relation), and prefer the symmetric-wedge special case (equal entrance/exit angles): less iron, simpler machining and vacuum plumbing.
D = X + (sin(Omega)/sin(gamma2))*Y1 + 0.4*G*(csc(gamma1)+csc(gamma2)) (Eq. III-23); symmetric case eps1 = eps2 collinear bisectorsSource, quote & tabletop applicability
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
Tabletop: DIRECT - the 0.4-gap effective-boundary shift is the same magnitude modern codes assign (FINT*gap); for a next machine's analyzer designed in FEMM the rule is a sanity check that the simulated effective edge sits ~0.4 gap outside the steel.
-
Skip higher-order focusing corrections when your fringe-field knowledge is cruder than the correction: Rochester computed second-order double-focusing wedge designs but declined to build one because the fringe corrections to the entrance angle were "not sufficiently precise to warrant basing the magnet design on the second-order calculations" - and first-order let them reuse the existing magnet.
Source, quote & tabletop applicability
the methods for correcting for the fringe fields effects ... are not sufficiently precise to warrant basing the magnet design on the second-order calculations.
Tabletop: 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.
-
Commissioning lessons from the as-built line: individual quad alignment is critical (install a balance control to redistribute current between lenses); expect ~60-70% of the beam entering the condenser aperture through a 1 x 4 mm slit; test the analyzer before beam with the floating current-carrying-wire technique - it caught a 15% image-distance discrepancy from a small effective-wedge-angle change.
Source, quote & tabletop applicability
The operation of the wedge analyzer has been checked using the standard current carrying wire technique.
Tabletop: DIRECT trio of transfers: (1) budget alignment/tuning provisions into any multi-element line; (2) the floating-wire method (wire under tension carrying current I follows the trajectory of a particle with B-rho = T/I) is a superb zero-beam teaching-lab measurement of magnet optics; (3) their bottom line - 0.1 uA on target at ~0.2% energy spread (p.53) - is the achieved-performance benchmark for a first-generation small-machine analyzed beam.
-
A Buechner-Bainbridge 90-degree broad-range spectrograph (uniform field, source and focus each one characteristic radius R outside the field boundary) focuses 0.6-1.3 E0 in one exposure at dE/E < 0.2%; theory allows 0.34-2.9 E0 (lower limit focused at the field boundary, upper at infinity) but chamber size caps the top and single-focusing solid-angle loss punishes E > E0.
focal range practical 0.6 E0 <= E <= 1.3 E0 (theoretical 0.34-2.9 E0); hyperbolic focal surface; R = 50 cm here, 14 kG focuses 33 MeV p / 16.5 MeV dSource, quote & tabletop applicability
an extension of the energy range much beyond 1.3 E0 requires an unreasonably large vacuum chamber at the exit of the magnet.
Tabletop: SCALE-HONEST: geometry is energy-independent (it fixes E/E0 ratios, not E), so a palm-sized R ~ 5-10 cm version at a few hundred gauss would broad-range-analyze a next machine's ~170 keV protons identically - a compelling teaching-lab focal-plane instrument. The 5-ton, 14-kG original is MeV-class; copy the optics, not the iron.
-
Relax instrument specs to the actual measurement: because the spectrograph was for relative (not absolute) energies, Rochester dropped the 0.1% field-uniformity requirement, collapsed the yoke to a simple C, deferred the pole-tip spacers, and accepted the return yoke on the concave side - measured performance was not markedly affected.
Source, quote & tabletop applicability
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.
Tabletop: 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.
-
Reproducible field error is harmless error: uniformity maps at 6.8 and 14 kG showed few-tenths-percent nonuniformities - larger than spec - but identical in location and magnitude at both excitations, so they calibrate out for a relative instrument. Complementary flag: the NMR probe signal degrades above 14 kG, a free saturation-inhomogeneity alarm.
Source, quote & tabletop applicability
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
Tabletop: DIRECT pairing of two ideas the reference machine already half-uses - (1) an error that scales rigidly with excitation is absorbed by end-to-end calibration; (2) loss of NMR (or Hall-linearity) signal quality is itself a diagnostic of entering saturation. Worth writing into the next machine's field-mapping procedure.
-
Build the analyzing-magnet vacuum chamber out of the magnet itself: ground pole-tip faces form the chamber top and bottom (gap doubles as chamber height, 3/4" held uniform to 0.0001" with brass spacers), thin non-magnetic stainless strips welded to the tips form the side walls, and brass anti-scattering baffles line the pole faces.
gap 3/4 in uniform to 0.0001 in via brass spacers; 5-in-thick heat-treated C1010 tips, faces ground flatSource, quote & tabletop applicability
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.
Tabletop: DIRECT construction pattern for any next-machine analyzer or spectrograph - poles-as-chamber eliminates the gap-wasting separate tank (the alternative Bromley rejected for his condenser on machining/gasketing grounds, nyo-3823 p.6). The anti-scattering baffles and the tenth-mil spacer discipline are the details that make emulsion-grade spectra possible.
-
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 & tabletop applicability
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.
Tabletop: DIRECT and free at design time - a straight-through optical path (laser today) plus a permanent probe port turn alignment and field checks from teardown jobs into ten-minute jobs. A next machine's chamber/beamline port lists should include both.
-
To swing a multi-ton spectrometer around a target: run it on a circular track ground flat and level in place (0.01" over a 70" diameter, using a grinder swung about the center post), support the load at exactly three points (central thrust bearing + two roller-bearing wheels), and drive it through gear reducers with a hand crank.
Source, quote & tabletop applicability
The track has been rendered flat and horizontal to within 0.01" by a grinding machine rotated about the vertical post.
Tabletop: DIRECT machine-design lessons independent of scale: generate precision in place with the tool swung about the final axis (self-referencing, like Wilson's lapped dees), and use kinematic three-point support so a 5-ton instrument neither rocks nor requires a precision-flat floor. A next machine's scattering table wants exactly this architecture at 1/50 the size.
-
Calibrate a magnetic spectrograph end-to-end with a monoenergetic alpha source stepped through field settings: a 1 mm Po source at the object position exposed for equal times at each field gives (a) the radius-vs-focal-position map, (b) the relative solid angle vs focal position for free from peak areas, and (c) a linewidth check against source width.
Source, quote & tabletop applicability
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.
Tabletop: DIRECT teaching-lab gold - one sealed alpha source and one afternoon calibrate the whole instrument, no beam required, and the equal-exposure trick measures the acceptance function that theory only estimates. Their peak-position convention (intercept of the straight high-energy edge with the baseline) is also the right lineshape-robust choice.
-
Precompute the operating aids: nu*rho-vs-energy curves per probe nucleus, a nomogram connecting particle energy, NMR frequency, and focal-plane position by a straight line, and bulk kinematics tables for the reactions you expect - so setup and particle-group identification happen at the console, not the desk.
Source, quote & tabletop applicability
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
Tabletop: DIRECT for the teaching program - the 2026 equivalent is a small lookup app, but the doctrine stands; run-time decisions need precomputed inverse tables. (Their compute budget was an IBM 650; the curriculum can have students build the nomogram itself as an exercise.)
-
Design the focal-plane detector for exposure multiplexing: a cassette holding three 80x200 mm emulsions allows six different exposures without breaking spectrograph vacuum, and a 20-element solid-state counter array covers 5 cm of focal surface when only a few groups matter.
Source, quote & tabletop applicability
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.
Tabletop: DIRECT principle (vacuum cycles are the tax on focal-plane work; amortize them) with a modern translation: a movable frame of CR-39/film chips, or a silicon-strip array, behind the next machine's analyzer. Their two-detector split - survey in emulsion, precision groups in counters - maps to CR-39-survey vs SiPM/diode-array.
-
Mounting a spectrograph with its dispersion plane horizontal costs kinematic broadening of peaks (from the in-plane angular acceptance) when scattering off light nuclei, but can buy large-angle reach - here rotation to 165 degrees, needed for back-angle cross sections and DWBA tests. Know which trade you are making.
Source, quote & tabletop applicability
In scattering from light nuclei, this introduces appreciable kinematic broadening of peaks as the entrance aperture is opened.
Tabletop: SCALE-HONEST - kinematic broadening scales with (m_projectile/m_target) and aperture, not beam energy, so the trade is identical for a next machine's Rutherford-scattering station. The fix they note (close the entrance aperture when it matters) is the standard resolution-vs-count-rate knob students should learn to turn.
-
A cyclotron needs no beam sweeper for time-of-flight work: the beam is already naturally bunched into RF-phase packets (bunching established within the first few turns), so nanosecond timing structure comes free - unlike a Van de Graaff, which must be artificially swept or bunched.
Source, quote & tabletop applicability
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
Tabletop: DIRECT and foundational for the experiment catalog - every cyclotron, including the reference machine at 9 MHz, delivers ~10-40 degree phase bunches at the RF period. The bunch structure is a measurable, teachable property (phase width vs turn number) and the enabling fact for every timing experiment on the machine.
-
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 & tabletop applicability
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
Tabletop: The most directly transferable finding here: the machine's RF is a free timing fiducial at ANY scale. Reference-machine and next-machine experiments (beam-phase measurement, gated counting, TOF over cm-scale paths for keV protons) can clock everything off a capacitive sniff of the dee line; beam-derived triggers die exactly when you need them (low current).
-
RF pickup implementation: a short (~10") wire antenna inside the oscillator enclosure a foot or two from the tank/grid circuit, coax shell grounded to the oscillator house; deliberately keep fundamental + harmonics and tune their relative phases/amplitudes with one or two shunt coax stubs of variable length and termination until the edge is sharp (~10 V pulses, rise ~5 ns, best ~3 ns at 10 Mc).
rise time ~5 ns typical, ~3 ns best at ~10 Mc oscillator frequency; retune stub after any frequency change (takes under a minute)Source, quote & tabletop applicability
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.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 8
Tabletop: DIRECT recipe, buildable on the reference machine in an afternoon - loose capacitive coupling (never galvanic) plus stub-tuned harmonic mixing is how you sharpen a 9 MHz sine (55 ns rise as a sinusoid) into a few-ns edge with zero active electronics at the pickup. The check-the-pulse-shape-after-retuning discipline (p.9) carries over verbatim.
-
Order the time converter start/stop for rare events: START the time-to-pulse-height converter on the (rare) detector pulse and STOP it on the next RF reference pulse - and gate the reference channel so stop pulses are only generated after a detector event. The converter then runs only ~once per neutron instead of once per RF cycle.
Source, quote & tabletop applicability
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
Tabletop: DIRECT - this reversed (common-stop) architecture is still how RF-referenced timing is done; it inverts the time axis but slashes dead time and pileup. With a modern TDC or digitizer the same logic applies: trigger on the detector, timestamp against the next RF zero crossing.
-
Split slow pulse-height discrimination from the fast timing chain, and make the threshold resettable against a standard source: a slow side-channel discriminator gates the analyzer (rejecting low-energy-neutron and gamma background), and its dial is reset after any shutdown to the Cs-137 gamma peak so efficiency calibrations reproduce even if PMT gain drifted.
Source, quote & tabletop applicability
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.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 13
Tabletop: DIRECT twice over: (1) never let the background-rejection threshold live inside the timing path (they tried; timing and efficiency fought); (2) a $50 Cs-137 check source turns "what is the threshold today?" into a 5-minute standardization - the calibration habit every counting experiment on a next machine should inherit.
-
Time-resolution budget honesty: achieved 2 ns FWHM in the favorable case, 2-3.5 ns typically, at ~1 ns/channel - and the 1" detector thickness alone contributes ~0.8 ns (5 MeV neutron transit time), traded knowingly for counting efficiency. Wrong stop-pulse shape or low PMT voltage easily makes it worse.
FWHM ~2 ns best, 2-3.5 ns typical; detector transit ~0.8 ns per inch for 5 MeV neutrons (v ~ 3.1 cm/ns)Source, quote & tabletop applicability
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
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 11
Tabletop: 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.
-
Set flight-path length against the room, not just the resolution equation: paths were kept under 1.2 m so that neutrons scattered from the concrete floor (4 ft below the beam pipe) arrive outside the window, letting the counter run unshielded; the massive Pb + LiH-paraffin shield was left unused partly because its effect on counting efficiency had never been measured.
Source, quote & tabletop applicability
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
Tabletop: 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.
-
Anchor absolute counting efficiency to a well-known reaction and cross-check by an independent method: calibrate with D(d,n) (cross sections known to 4%), then verify via induced-activity counting - C-12(d,n)N-13 yield integrated over angle, N-13 positron annihilation flux compared against an NBS-calibrated Na-22 source - agreement within 10%.
Source, quote & tabletop applicability
Calibration curves were obtained by use of the D(d,n) reaction, the cross sections for which are known to 4% accuracy.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 12
Tabletop: DIRECT metrology doctrine - one calibration path is an assumption, two are a measurement. For a next machine's experiment gates (e.g., p-B or (d,n) yield claims), require a primary calibration plus an activation- or source-based cross-check, and quote the disagreement as the systematic.
-
A simple single-scattering model predicts organic-scintillator neutron efficiency to satisfactory accuracy: eff = (1 - E0/En) * (1 - exp(-nH*sigma_np*l)), where the first factor (fraction of recoils above threshold) is exact and independent of the scintillator response shape so long as response is monotonic; find E0 per threshold setting from a D(d,n) check and take sigma_np from Gammel's semi-empirical formula (good to parts in 10^3 up to 42 MeV).
eff = (1 - E0/En)(1 - exp(-n_H * sigma_np(En) * l)); assumptions - n-p single scattering only, effective length = geometric length, recoil range negligibleSource, quote & tabletop applicability
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
Tabletop: DIRECT for any neutron-counting next-machine experiment and a lovely teaching derivation - a two-factor closed form students can test against a calibration reaction. The identification of which factor is exact vs model-dependent is the transferable habit.
-
When slow neutrons from one beam burst can be overtaken by fast neutrons from the next (frame overlap), scale the beam-pulse rate down by electrostatically deflecting bunches at a subharmonic of the machine RF: ~3 Mc effective rate virtually eliminated the problem. Prefer odd division ratios - at even ratios bunches arrive at both zero crossings of the deflection voltage, changing the effective scaling factor (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 & tabletop applicability
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
Tabletop: SCALE-HONEST: frame overlap needs multi-MeV spectra over meter paths, so sub-MeV machines rarely hit it - but the tool is general: a pair of deflection plates driven at an RF subharmonic is the cheapest beam chopper a cyclotron can have (single-bunch selection, duty-cycle control, background gating), and the odd/even zero-crossing subtlety is real circuit-level physics worth teaching.
-
Design auxiliary RF systems with the minimum number of tuned circuits - here exactly one (the deflection-plate tank itself): the divider is an untuned locked multivibrator (locks on 2-200 V drive, 5-25 Mc) and the driver chain is untuned up to the 807 output pair, so changing cyclotron frequency requires retuning one circuit. When scaling makes three RF stop pulses per beam bunch, gate the correct one with the divider but keep the timing edge derived directly from the oscillator for accuracy.
multivibrator locks at f_cyc/3 for 2-5 Mc output over 10-15 Mc input; one tuned circuit total (deflector tank)Source, quote & tabletop applicability
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
Tabletop: DIRECT pair for a next machine's auxiliary electronics: (1) every tuned circuit is a knob someone must retune at every frequency change - minimize them by design (a lesson the reference machine's self-excited oscillator experience already rhymes with); (2) use derived/divided signals for SELECTION logic but always take the precision timing edge from the primary RF - never from a divider chain.
-
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 model resonates at 2x full-scale frequency; geometric ratios and line impedances are scale-invariantSource, quote & tabletop applicability
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
Tabletop: 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.
-
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 because they have no RF function. Known infidelities were listed, not ignored.
Source, quote & tabletop applicability
Only the radio frequency circuit was simulated in the model, the vacuum system and purely mechanical equipment was not included.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 7
Tabletop: License to mock up the next machine's RF cavity in bare copper/aluminum on a bench plate — no chamber, no pumps — provided every conducting surface that carries RF current (liner included) is reproduced.
-
Extrapolate model power to full scale as P proportional to V^2 with a sqrt(2) shunt-impedance credit for the half-scale model (skin depth: doubled size at halved frequency raises Q and R_sh by sqrt(2)). The printed numbers obey it exactly: 520 W at 1.5 kV on the model becomes 146 kW at 30 kV full scale (x400/sqrt(2)); oscillator efficiency held at 59-64% across the band.
P_full = P_model * (V_full/V_model)^2 * sqrt(s), s = model/full linear scale (=1/2 here, so divide by sqrt(2)); R_sh scales as s^(-1/2) at scaled frequency [scaling law implied by the printed 520 W -> 146 kW pair; verified against all four frequencies]Source, quote & tabletop applicability
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
Tabletop: The V^2 term is the live part for a next machine's power budgeting — measured drive power at a safe low dee voltage extrapolates as (V_target/V_test)^2 on the same hardware, since Q is voltage-independent until multipactor/breakdown; a 1500-V measurement predicts the 5-13 kV LDMOS requirement.
-
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 & tabletop applicability
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
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: The reference machine's lore confirmed at lab scale — final RF tuning of a next machine's cavity must be done with dummy dee, source structure, and probes installed, or budget a multi-percent retune.
-
Keep a two-sided trim toolkit for a cavity that lands off-frequency: a shorted stub (transmission line shorter than lambda/4 at the operating frequency) attached to the dee raises resonance; added dee-to-liner capacity plates lower it. Costs measured: stubs +3 mc for +25% 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 & tabletop applicability
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
Tabletop: The recovery plan if a next machine's fixed-frequency cavity misses 9-ish MHz after assembly; note both fixes tax drive power, so aim the design low in frequency and trim up with the cheaper capacitive side when possible.
-
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 & tabletop applicability
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
Tabletop: On a small machine the dee-stem-to-chamber-wall clearance is the same critical region — it sets both the resonant frequency and where I^2R heating concentrates; machine it to drawing, do not shim it by eye.
-
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 & tabletop applicability
The oscillator must be stable enough to sustain an arc drawn from the dee face (simulating discharges in that region).
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 12
Tabletop: The arc test transfers verbatim to the planned LDMOS amplifier — prove the driver (and its protection) rides through a real drawn arc at the dee before trusting it in vacuum, where sparking during conditioning is guaranteed.
-
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 & tabletop applicability
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
Tabletop: 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 expect inch-level sensitivity at low VHF.
-
Check every ancillary choke and feed for self-resonance near the operating band: the filament-heating chokes were self-resonant at 18 mc (in-band) and caused a sharp dee voltage drop; rewinding them to resonate at 60 mc — well above band — removed it.
place choke self-resonance >= ~3x operating frequency (18 mc in-band fault -> 60 mc fix)Source, quote & tabletop applicability
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
Tabletop: Filament, bias, meter, and interlock leads entering the reference machine's or a next machine's tank all need RF chokes whose self-resonance is measured, not assumed — a choke resonant near 9 MHz silently loads the dee.
-
Measure inaccessible element capacities by bridge subtraction: measure dee-to-liner and stub-to-liner with the moving element in and out, subtract to isolate each element, then series-combine. Model results: rotary condenser swing 1370 uuf max to 50 uuf min, ratio 27.6; bare dee-to-liner 1500 uuf.
C_element = C_(assembled) - C_(element removed); series C = 1/(1/C1 + 1/C2); measured swing 1370/50 uuf = 27.6Source, quote & tabletop applicability
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
Tabletop: Same differential technique as Koeth's Rutgers dee-capacitance note already in this collection — an LCR meter plus one disassembly step yields every lumped C in a next machine's tank model, feeding the resonance and Q predictions.
-
Power and efficiency can be measured with no RF instrumentation in the power path: calibrate tube-plate temperature (optical pyrometer on one spot) against DC input with RF excitation killed by shorting the line, then read true plate dissipation under RF from the calibration curve. Probe voltmeters were lab-built diodes, calibrated periodically, honestly rated +/-5-10%.
P_out = P_in(DC) - P_plate(from thermal calibration); probe error assumed +/-5 to 10%Source, quote & tabletop applicability
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
Tabletop: The thermal-reference trick survives translation — calorimetry on the LDMOS heatsink (or dee cooling loop) calibrated at DC gives dissipated power without trusting directional couplers; and publish instrument error bars the way Anderson did.
-
A scale model's known infidelities must be listed with the results: substitute 304-TL triodes have much larger internal inductance than the final 9C21s, the filament line's impedance changes where it enters the vacuum system, and mismatched plate capacities between the two tubes skewed early power measurements.
Source, quote & tabletop applicability
the inductance inherent in the 304-TL triodes is large compared with that in the 9C21 triodes to be used in the final oscillator.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 12
Tabletop: 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.
-
Model cyclotron acceleration as kick-plus-coast: an impulsive energy change at each gap azimuth followed by a static (coasting) trajectory to the next gap. Accelerated behavior is then inferred from static phase plots at a few energies, interpolated — validated throughout this study against fully accelerated runs.
per gap crossing dE = qV_gap; r and p_r unchanged at the kick (radial gaps); coast on the static map between gapsSource, quote & tabletop applicability
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
Tabletop: The core architecture for CYCLOPS-lite — thin-gap kicks alternating with magnetic coasting maps is 1961-validated practice, and MSUCP-12's analytic gap field upgrades the kick from a delta function to a distributed one when transit time matters.
-
Build the orbit toolchain as two codes: a closed-orbit finder using a linear transfer-matrix (Newton-type) search, and a general tracker integrating median-plane-exact equations with the field supplied as tables of Fourier coefficients versus radius, with acceleration switchable on or off.
B(r,theta) = B0(r) + sum_j [H_3j(r) cos(3j*theta) + G_3j(r) sin(3j*theta)] (field input format, Table I)Source, quote & tabletop applicability
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
Tabletop: 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.
-
To map the phase-space topology at an energy, locate the unstable fixed points first, then launch orbits displaced slightly from them and integrate both forward AND backward in time — the resulting trajectories trace the separatrices that bound every region of interest, far cheaper than blanketing the plane with orbits.
Source, quote & tabletop applicability
the general orbit code is employed to trace forward and backward in time orbits with initial conditions displaced slightly from the unstable fixed points.
Tabletop: Directly reusable in a Python tracker (integrate with negative dt for the backward branch); the efficient way to draw the r-pr stability picture of any field candidate for a next machine near resonances.
-
Median-plane-only tracking is a justified economy: the small axial aperture holds the beam where the field's z-dependence is linear, so off-median aberrations stay small relative to median-plane effects — but the assumption was spot-checked with a few off-plane trial runs, not just asserted.
Source, quote & tabletop applicability
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.
Tabletop: Permission to build the next machine's first tracker 2-D (r, pr, E, phase) and add axial motion as a linearized afterthought — with the same obligation to verify by a handful of full-3D spot checks.
-
Orbit studies can run on measured scale-model magnet 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, Fourier-analyzed assuming perfect 120-degree symmetry, flutter smoothed of measurement noise, average field isochronized, and harmonics above 99 dropped as negligible.
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 & tabletop applicability
The radial spacing of the table entrys is interpreted as increased by the factor 64/8.75 corresponding to the ratio of pole diameters
Tabletop: The historical analog of the CadQuery->FEMM->field-map pipeline, plus two habits worth copying — symmetrize and smooth measured maps before tracking, and document every cleanup applied to the field the tracker actually ate.
-
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 & tabletop applicability
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.
Tabletop: Cuts both ways at reference-machine and next-machine scale — shim asymmetries of tens of gauss are dynamically significant near nu_r = 1 (center and full radius), yet a deliberate few-turn bump coil is a powerful, cheap orbit-steering experiment.
-
Resonant extraction works by making the stable center of phase space jump: the first-harmonic bump causes the equilibrium orbit and an unstable fixed point to merge and vanish as energy rises, so the surviving stable point is elsewhere (S1) — the beam suddenly finds itself executing a large-amplitude oscillation, and that amplitude is the turn separation.
Source, quote & tabletop applicability
introduction of the field bump has caused a discontinuous jump in the location of the central stable orbit in the phase diagram
Tabletop: The conceptual mechanism to have in hand before any extraction attempt on a next machine; it needs nu_r to pass unity with a controlled first harmonic — both quantities a FEMM-fed tracker can compute for a candidate pole design.
-
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), twisting and filamentation are not (they mix filled and empty phase space irreversibly).
Source, quote & tabletop applicability
stretching and rotation are fine but not twisting, filamentation, etc.
Tabletop: The right figure of merit for any next machine's beamline or extraction simulation — track a small grid of particles and judge the deformed shape, not just the centroid; five to two dozen particles sufficed in 1961.
-
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 & tabletop applicability
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.
Tabletop: The doctrine transfers whole to any resonance-crossing scheme on a small machine — cross fast where the map is ugly; the diagnostic (superimpose the accelerated beam path on static phase plots) is a cheap tracker post-processing step.
-
Energy gain per turn is the master knob of resonant extraction quality: rerunning the same beam at half (140), design (280), and double (560) kV per turn showed the high-voltage case notably well behaved and the conclusion that substantially lower volts/turn sharply degrades BOTH extraction efficiency and optical quality — the beam must cross the bad region of phase space quickly.
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 & tabletop applicability
volts per turn substantially lower than the designed 280 kev/turn would result in sharp reduction of both extraction efficiency and optical quality.
Tabletop: The quantitative ancestor of "dee volts buy extraction" — the reference machine's ~800 V nominal dee is why it is internal-beam-only, and the next machine's 5-13 kV target is what would make any future extraction scheme even thinkable.
-
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 & tabletop applicability
The sinusoidal voltage, it is seen, shifts the final position of the beam spot but has almost no effect on the distortion.
Tabletop: 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.
-
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. The effect needs the two gap kicks to add coherently, which happens only when the field lacks 180-degree symmetry.
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 & tabletop applicability
the result is seen to fairly accurately predict the actual amplitude and 0 of this point of the grid
Tabletop: Two lessons — build point analytic cross-checks into a next machine's tracker test suite (transfer-matrix estimates vs tracked orbits), and note the physics is benign for a 180-degree-symmetric two-dee tabletop field where the paired kicks cancel.
-
Let the computation overrule the folklore: tracking showed beams entering the extraction region centered on the equilibrium orbit behave as well or better than deliberately displaced beams — contradicting the group's own earlier qualitative proposal (MSUCP-2) that displacement would help.
Source, quote & tabletop applicability
beams entering the extraction region approximately centered on the equilibrium orbit behave as well or better than beams entering with substantial displacement.
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: 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).
-
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.
general (eqs. 2-5): E_x = (V0/h)*Xv/(Xv^2+Xu^2); E_y = (V0/h)*Xu/(Xv^2+Xu^2); Xv = cosh(X1)*cos(Y1)*(1 + 1/(A*F^2)); Xu = -sinh(X1)*sin(Y1)*(1 - 1/(A*F^2)); F = sqrt(cosh^2(X1) - sin^2(Y1)); potential v = arccos(cos(Y1)/F), v = pi*V/(2*V0); solve X = X1 + sinh(X1)*cosh(X1)/(A*F^2) and -Y = Y1 + sin(Y1)*cos(Y1)/(A*F^2), with X = pi*x/(2h), Y = pi*y/(2h), A = a^2/(1-a^2).Source, quote & tabletop applicability
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
Tabletop: E_y(x,y) is exactly what a tracker needs for the Rose/Wilson electric gap-focusing term that dominates axial stability on the first turns of a sub-kV machine like the reference machine — available here analytically at any (x,y), no field map required.
-
Solve the gap-field transcendental equation with Gordon's Newton iteration, not Murray-Ratner's original (which converges slowly for small alpha and fails for large alpha): linearize tanh(X1) about the current guess; convergence is quadratic and works for all gap ratios given the two-branch initial guess.
eq. 9: X1_new = [X - alpha*tanh(X1*) + alpha*X1**sech^2(X1*)] / [1 + alpha*sech^2(X1*)]; initial guess X1 = X/(1+alpha) if (1+alpha) > X, else X1 = X - alphaSource, quote & tabletop applicability
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.
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 7
Tabletop: Copy the iteration and its initial-guess branch verbatim into the tracker's field routine; a handful of iterations reaches machine precision, cheap enough to call per integration step (or use once to build a spline).
-
The peak accelerating field at the gap center saturates at V0/h — it is 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, 0.3, 0.5, 1.0, 1.5, 2.0, 2.5, 3.0, 3.5. Narrowing the gap below about half the aperture buys almost nothing; in the k -> 0 limit the profile is exactly (V0/h)*sech(pi*x/(2h)).
E(0) = (V0/h)/(1+alpha), exact from eq. 6; k->0 limit E_x = (V0/h)*sech(pi*x/(2h))Source, quote & tabletop applicability
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
Tabletop: Sets the real ceiling on gap-field strength for any dee redesign — with a 1-inch aperture (h = 0.5 in) and 5 kV dee-to-dummy (V0 = 2.5 kV), peak field cannot exceed ~2 kV/cm no matter how tight the gap; widening the aperture for beam height costs peak field one-for-one.
-
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 at x/h ~ 1.8 (k/h = 0.1) to ~2.6 (k/h = 1.5) [from Table 1]Source, quote & tabletop applicability
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
Tabletop: Transit-time factors and gap-crossing phase errors for the tiny machine and a next machine must be computed on this extended profile — at low first-turn velocities the particle spends a large RF phase interval inside a field region ~2h long, which a delta-kick model at the gap centerline gets wrong.
-
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 & tabletop applicability
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
Tabletop: Kills the tempting back-of-envelope E = V_dee/gap for both breakdown margin and energy-gain 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 the tables.
-
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 & tabletop applicability
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
Tabletop: Unit-test targets for the tracker's gap-field routine AND an independent check on FEMM electrostatic runs — model the same idealized geometry in FEMM once and match these 5-digit values before trusting FEMM on the real next-machine electrode shapes.
-
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.
alpha < 4 corresponds to k/h < (2/pi)*(arccosh(sqrt(5)) + 4*sqrt(5)/5) = 3.77Source, quote & tabletop applicability
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
Tabletop: For use on a next machine, the real deviations to check against FEMM are finite dee thickness, the rounded/blunted tip, and the curved gap line near the source at small radius — expect the analytic solution to be excellent at mid-radius and approximate near center where the ion-source chimney dominates the field anyway.
-
Size shielding for the SECONDARY radiation, not the primary beam: the interaction of the beam with the target, the accelerator structure, or the shielding itself most often determines the type and magnitude of shielding required.
shield for secondaries (X-rays, neutrons) produced where the beam is lost, not for the primary ionsSource, quote & tabletop applicability
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.
Tabletop: For the reference machine and a next machine the primary protons never leave the chamber; the machine's entire external radiation field IS secondary — dee-gap electron bremsstrahlung today, 11B(p,alpha) products and any (p,n)-capable contaminants at a next machine's energies.
-
On positive-ion machines below 50 MeV, ignore primary-particle bremsstrahlung (it scales ~1/M^2 of the projectile mass) and look instead for the three real X-ray sources: 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 & tabletop applicability
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.
Tabletop: Confirms the program's standing model that dee-voltage electrons, not the proton beam, are THE radiation hazard on a sub-MeV proton cyclotron.
-
Even when characteristic/soft X-radiation poses a trivial shielding problem, plan the INSTRUMENTATION for it: survey meters must be able to detect and measure the soft component, which exists at any incident-particle energy.
instrument response must extend down to the soft X-ray band even when shielding is trivialSource, quote & tabletop applicability
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.
Tabletop: 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).
-
Lacking design detail, estimate 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; the authors label the assumption unreliable but note it still predicts "very considerable" X-ray production.
I_e(back-streaming) ~ 0.2 * I_ion at E ~ V_terminal/3, as a bounding source-term assumptionSource, quote & tabletop applicability
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.
Tabletop: Directly usable bounding recipe for a next machine's hazard analysis: treat the machine as an electron gun of 0.2x the circulating/source current at ~1/3 of peak dee voltage (multipactor and secondary electrons play the "back-streaming" role), then look up kV X-ray-tube output data for that current and voltage.
-
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 & tabletop applicability
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.
Tabletop: The conservative sizing pattern for any product-machine enclosure — bound the cyclotron by an equivalent electron machine at dee voltage and shield for that; at <=13 kV the "shield" is millimeters of steel/leaded glass, which is why chamber walls suffice on the reference machine.
-
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 & tabletop applicability
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
Tabletop: Sets the scaling logic (efficiency ~ Z and E) even though sub-MeV values must be extrapolated downward: keep stray electrons landing on LOW-Z surfaces (Al, graphite) rather than W/steel to cut X-ray yield several-fold — an argument for aluminum dee/liner surfaces on product machines.
-
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 & tabletop applicability
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.
Tabletop: For dee-gap electrons accelerated axially/radially in the chamber, expect the soft X-ray leakage to peak SIDEWAYS from the electron paths — survey all around the chamber midplane and windows, not just along any assumed "beam" direction.
-
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 1-40 MeV electrons only; below ~1 MeV take the source-term assumptions from this chapter but the output numbers from kV X-ray-tube data.
D(behind x cm concrete) = TableII-3(T,x) * W(kW)/R(m)^2, valid 5.5-40.5 MeV; below ~1 MeV use X-ray-tube output tablesSource, quote & tabletop applicability
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.
Tabletop: Scope honestly: this is this collection's only full X-ray shielding workflow, but its curves START at ~1 MeV. For the 5-13 kV dee upgrade, pair its 0.2*I/(V/3) source assumption with NCRP-49-class tube output data (R/mA-min at 1 m vs kVp) instead of Table II-3.
-
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 & tabletop applicability
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.
Tabletop: Closes the neutron question for the reference machine at ~150 keV-class energies EXCEPT via the light-nuclei exceptions the chapter waves off — which here are exactly the deliberate 11B(p,alpha) target and any deuterium contamination (see Ch. IV rule).
-
(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 only becomes the DOMINANT channel about 1 MeV above threshold (an emitted neutron faces no Coulomb barrier).
E_thr(p,n) > 0.78 MeV (stable targets), ~MeV for light nuclei; n-channel dominant at E > E_thr + ~1 MeVSource, quote & tabletop applicability
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.
Tabletop: 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).
-
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 & tabletop applicability
H2(gamma,n)H1 ... 2.23 ... C12(gamma,n)C11 ... 18.7 ... O16(gamma,n)O15 ... 16.3
Tabletop: Fully closed at the photon energies of the reference machine and a next machine (<=keV-class bremsstrahlung, 429 keV 11B(p,alpha) line region), but the table is the permanent reference for why nothing photonuclear can happen on these machines — useful verbatim in the product hazard analyses.
-
Neutron shielding is slow-down-then-capture: light nuclei (hydrogen) dominate energy loss, so concrete far outperforms lead, and a facility shielded in concrete for X-rays "generally contains adequate neutron shielding in the process" — the serious neutron problem arises only when the neutron hazard exceeds the photon hazard (proton and deuteron machines).
concrete X-ray shield ~ adequate neutron shield (rule of thumb, <30 MeV); capture gammas must be shielded in turnSource, quote & tabletop applicability
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.
Tabletop: For any future neutron-capable operation (a deuterium species test, or a >1.9 MeV machine) the shielding material answer is already decided — hydrogenous concrete/HDPE, not lead — and the X-ray shield does NOT automatically cover it, because the reference machine accelerates protons.
-
For first-pass neutron shield sizing use the reactor-derived removal-cross-section method: treat penetration as exp(-Sigma_r * x) with the empirically chosen removal cross section (roughly 3/4 of the total cross section at 8 MeV; Sigma_r ~ 0.094 cm^-1 for ordinary or barytes concrete), and reinforce thicknesses in the forward direction where high-energy anisotropy defeats the method.
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 & tabletop applicability
Experimental removal cross sections are roughly three-quarters of the total cross section for 8 MeV neutrons. For hydrogen this fraction is somewhat larger.
Tabletop: The one-line neutron shield calculator for any contingency planning — e.g. a D-D contamination source term attenuates ~10x per 24 cm of concrete; keep safety factors for cross-section uncertainty as the chapter directs.
-
Worked pattern for a neutron shield: 20-MeV protons on an optimized Cu target make ~6.5e10 n/s per uA; taking the flux at the shield, demanding six orders of magnitude attenuation, and inverting exp(-Sigma_r x) gives 146 cm of barytes (or ordinary) concrete — and a one-step inverse-square correction (144 cm) shows the slab-normal assumption is already good.
Y(20 MeV p on Cu) ~ 6.5e10 n/s/uA; x = ln(attenuation)/Sigma_r -> 146 cm for 1e6Source, quote & tabletop applicability
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.
Tabletop: The template to copy for any neutron-capable scenario: source yield -> 1/4pi*r^2 flux at shield -> required attenuation from the dose criterion -> x = ln(A)/Sigma_r. Also the scale anchor for why amateur neutron machines are enclosure-limited: five FEET of concrete for a 1-mA 20-MeV machine.
-
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 the source gas or beam-loaded surfaces makes neutrons with no threshold protection; every other common neutron-producing reaction is endoenergetic.
D(d,n)He3 Q=+3.27 MeV, T(d,n)He4 Q=+17.6 MeV -> no energy threshold; all common (p,n)/(gamma,n) are threshold-gatedSource, quote & tabletop applicability
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.
Tabletop: 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. It keeps a neutron survey requirement honest even though the expected yield at tabletop beam densities is tiny.
-
Induced activity around an accelerator is a two-step process (beam makes neutrons/photons in the target; those activate surroundings), and because absorption probability goes as 1/v the THERMAL cross section — not the fast one — should be used when estimating what gets activated.
activation A0 = M*phi*sigma_thermal*(1-exp(-lambda*t_irr)); slowing-down activation negligible by comparisonSource, quote & tabletop applicability
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.
Tabletop: The correct bookkeeping if a neutron-capable operation is ever run — inventory surrounding materials (Cu 3.9 b, W 34 b, Au 96 b thermal per Table IV-2) against thermal flux; also why activation on today's neutron-free machines is nil.
-
In ordinary concrete the only activation products that matter are Na-24 (15 h) and perhaps K-42 (12.4 h) — 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 the day but decays by a factor of several thousand overnight.
concrete activation governed by Na-24 (15 h) / K-42 (12.4 h); 3-5 day cooldown -> negligibleSource, quote & tabletop applicability
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.
Tabletop: Ready-made cooldown-scheduling logic for any future neutron-producing facility work; for the current machines it documents why the basement structure cannot become activated.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Long-lived photon-produced isotopes in shielding (Na-22, 2.6 y, from long bremsstrahlung irradiation above threshold) cannot be waited out — if large quantities build up the activated concrete must be physically removed, so plan wall design for that contingency up front.
above-threshold gamma flux + years of operation -> Na-22 inventory -> removable-wall contingency in designSource, quote & tabletop applicability
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.
Tabletop: Scope closed for the machine's photon energies (needs >12.4-MeV photons), but the design principle — never pour a monolithic shield you might someday have to demolish as radwaste — transfers to every enclosure decision.
-
Express every field measurement as DOSE EQUIVALENT: DE = D * QF * DF (rem), where D is measured absorbed dose, QF the LET-dependent quality factor, DF a distribution factor — dose in rads alone does not specify the hazard of a mixed or high-LET field.
DE(rem) = D(rad) * QF * DFSource, quote & tabletop applicability
The effective dose called the "Dose Equivalent" in units of rem is given by DE=D*QF*DF.
Tabletop: The reporting convention every run-log radiation entry should follow once a next machine operates — a Faraday-cup-adjacent photon reading and any neutron check must be weighted before comparison to limits (modern practice replaces QF with wR but the structure is identical).
-
The ICRP RBE-committee quality factor can be approximated in tissue as QF = 0.8 + 0.16 * LET (LET in keV/um of water) — a one-line way to convert any radiation's stopping power into its protection weighting.
QF ~ 0.8 + 0.16*LET(keV/um H2O)Source, quote & tabletop applicability
QF = 0.8 + 0.16 LET where LET is in keV/u.
Tabletop: Lets the program derive its own weightings for odd radiations (the 11B(p,alpha) alphas at ~1.7 MeV/each have LET ~100 keV/um -> QF ~17, consistent with the alpha QF 1-20 table entry) instead of guessing; flag as the 1972 formulation of what is now wR.
-
1972 practical quality factors: X-rays, gammas, electrons = 1; neutrons below 10 keV = 3; neutrons above 10 keV = 10; protons 1-10; alphas 1-20; fission fragments/recoils = 20 — use as the era's weighting set, noting modern wR for neutrons is energy-continuous and peaks at 20.
QF: photons/e- 1; n<10keV 3; n>10keV 10; p 1-10; alpha 1-20; fragments 20 (1972 values)Source, quote & tabletop applicability
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
Tabletop: HISTORICAL VALUES — cite for provenance but apply ICRP-103 wR in any real analysis (photons 1, neutrons 2.5-20 by energy, alphas 20). The photon QF=1 and alpha ~20 endpoints are unchanged, so the reference machine's photon surveys and internal-alpha reasoning carry over directly.
-
Flux-density-to-dose conversion for neutrons (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 QF peak (~11) near 0.5-1 MeV makes fast 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 & tabletop applicability
2.5 x 10-8 (thermal) 2 680 ... 5 x 10-1 11 27 ... 1 11 19
Tabletop: The number that turns any future neutron survey reading into a stay-time — a D-D contamination field of even a few n/cm2-s at 2.45 MeV is already a nontrivial fraction of a 1972 occupational week (modern limits tighten this ~5x for the public).
-
Derive dose limits by the CRITICAL-ORGAN method: identify the organ that governs for the radiation type — SKIN (skin-cancer endpoint) for relatively non-penetrating radiation, blood-forming tissue (leukemia endpoint) for penetrating radiation — then set the limit for that organ; note background (50-175 mrad/yr, locally >1000) makes a zero limit meaningless.
non-penetrating radiation -> skin is critical organ; penetrating -> blood-forming tissue; limit set per organ against background contextSource, quote & tabletop applicability
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.
Tabletop: Directly relevant to sub-10-keV dee bremsstrahlung, which barely penetrates the epidermis: the governing quantity for the machine's leakage fields is SHALLOW/skin dose, which is why survey instruments must be thin-window (Ch. VI) and why whole-body limits alone understate the right metric.
-
The 1972 occupational limits — accumulated whole-body dose <= 5 rem x (age-18), <= 3 rem per quarter, skin 15 rem/yr, hands/forearms 75 rem/yr (25/quarter), general public 0.17 rem/yr (10x reduction) — are SUPERSEDED; extract only the structure: occupational vs public tiers, quarterly pacing, separate skin/extremity allowances.
HISTORICAL: 5(N-18) rem accumulated; 3 rem/qtr; skin 15 rem/yr; extremities 75/25; public 0.17 rem/yr. MODERN: 5 rem/yr occ., 0.1 rem/yr public (10 CFR 20)Source, quote & tabletop applicability
shall not exceed 5 rems multiplied by the number of years beyond 18. The dose in per calendar quarter shall not exceed 3 rems.
Tabletop: 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."
-
Accelerator radiation differs from isotope radiation in three ways that break isotope-calibrated instruments: it is PULSED (cyclotron: 50-200 us macropulses with RF microstructure), strongly ANISOTROPIC, and a MIXED neutron/gamma field — choose and correct instruments for all three.
cyclotron pulse structure: 50-200 us macropulse + microstructure at RF frequency (Table VI-1)Source, quote & tabletop applicability
Cyclotron positive ions 50-200 usec ... Microstructure at RF frequencies
Tabletop: 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.
-
When counting radiation from a pulsed machine whose pulse length is shorter than the detector dead time (GM: 200-600 us dead; ion chamber 5-10 us; organic scintillator 0.01-0.1 us), the measured rate SATURATES AT THE PULSE RATE no matter how intense the field — a GM survey meter can read a grossly lethal pulsed field as a modest count rate.
for rho > pulse length, n'_max = pi (pulses/s); GM dead time 200-600 us (Table VI-2, Eq. VI-9)Source, quote & tabletop applicability
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.
Tabletop: THE classic accelerator-survey trap and the reason the program's survey doctrine should prefer current-mode ion chambers over GM counters for any pulsed operation: a counter that reads "60 cps" at a 60 Hz pulse rate is telling you its saturation value, not the dose rate.
-
Measure mixed neutron-gamma dose equivalent with PAIRED ionization chambers — one tissue- equivalent, one neutron-insensitive — and combine as DE = Gamma + 10*N (Gamma = gamma tissue dose, N = neutron tissue dose, 10 a conservative quality factor).
DE = Gamma + 10N (paired TE + neutron-insensitive chambers)Source, quote & tabletop applicability
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
Tabletop: 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.
-
Dose-equivalent-proportional neutron instruments are a solved problem: an Anderson-Braun BF3 counter in polyethylene/boron cylinders reads dose equivalent to +-10% from 0.04 to 10 MeV, and a properly made moderated-sphere rem counter holds +-10% for intermediate energies — use a rem counter rather than converting raw flux by hand.
Anderson-Braun rem counter +-10% over 0.04-10 MeV; moderated thermal detector rem-proportional +-10%Source, quote & tabletop applicability
They obtained an accuracy of +-10% in measuring dose equivalent of neutrons over the range 0.04 to 10 MeV.
Tabletop: Justifies planning on one moderated rem meter as the single neutron instrument — its energy band covers everything a D-D contamination source (2.45 MeV) or any near-threshold (p,n) could emit.
-
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 & tabletop applicability
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.
Tabletop: Any amateur-scale neutron leakage lives exactly in the worst band (keV-MeV), so never average it away with a thermal-flux conversion; modern wR moves the peak value to ~20 near 1 MeV, making this reasoning MORE conservative today, not less.
-
Photon survey instruments misbehave below ~150 keV where the photoelectric effect dominates: cavity-chamber response FALLS at low energy from wall thickness (lost particle equilibrium), can swing ABOVE unity just over that energy because wall Z exceeds air, and windowed detectors develop strong directional error — calibrate at the working energy and orientation before trusting soft-X-ray numbers; open-air chambers also drift 20-30% with large temperature changes.
below ~150 keV photoelectric regime -> wall-thickness response falloff + over-response band + directional error; open-air chamber +-20-30% over large delta-TSource, quote & tabletop applicability
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.
Tabletop: The measurement-side half of the reference machine's X-ray problem: the machine's entire photon spectrum sits BELOW this misbehavior threshold, so an uncalibrated chamber reading of dee bremsstrahlung can err either direction. Use thin-window instruments with a low-energy calibration point (e.g. Fe-55 or an X-ray tube set) and record orientation.
-
Harden detector electronics against the machine's own environment: mu-metal shields handle photomultiplier magnetic-field sensitivity, aluminum foil or screening kills RF pickup, and low-frequency EMI synchronous with machine pulsing demands well-grounded cable shields with a common ground at both ends — expect grounding to take "considerable effort."
PMT: mu-metal (B-field) + Al foil/screen (RF); signal runs: grounded shield + single common groundSource, quote & tabletop applicability
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.
Tabletop: Written for exactly such a bench — a scintillator PMT near a 0.6 T fringe field and a 9-MHz (soon LDMOS) transmitter. The Keithley 617 grounding lore in the reference machine's as-builts is this rule independently rediscovered.
-
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 & tabletop applicability
The most common cause of serious radiation exposures associated with accelerators, has been accidental (and sometimes intentional) entrance into the normally shielded target cell.
Tabletop: 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 minimum for exactly this machine class.
-
Estimate X-ray streaming through a maze/labyrinth by following successive 90-degree Compton scatters: assume conservatively that 0.05 of the incident energy scatters into one steradian at each bounce, I_p = (I_1/r_n^2) * prod[0.05*S_j*cos45/r_i^2]; the method matched a Co-60 measurement within a factor of ~2 (0.65 calculated vs 1 mr/hr measured on a 6-ft three-legged maze).
I_p = I_1/r_n^2 * prod_i [0.05 * S_i * cos45 / r_i^2] per 90-deg scatter legSource, quote & tabletop applicability
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.
Tabletop: Scales down perfectly — the same hand calculation sizes a cable/vacuum-line penetration dogleg or an instrument port baffle in a product-machine enclosure, where a straight-through hole would be the dominant leak.
-
Permit NO line-of-sight path for radiation through any access route or penetration, and then still evaluate the scatter path through the maze — geometry (not material) is the streaming problem, and the maze delay must be made at least as long as a heavy door would impose.
no line-of-sight through any penetration; scatter path evaluated per the 0.05/sr ruleSource, quote & tabletop applicability
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.
Tabletop: The audit rule for every feedthrough, window, and joint in an enclosure — check sight-lines from the X-ray source point (dee gap) outward, then bound the one-bounce leakage.
-
For neutron streaming through mazes use the albedo chain phi_p = (phi_s/(4pi r_n^2)) * prod[beta*Omega_i]: neutron albedo runs from 0.66 for thermal down to ~0.05 for fast (0.4 is a conservative fast-neutron choice), and boron-loaded concrete 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 & tabletop applicability
albedo for neutrons (from 0.66 for thermal neutrons to approx. 0.05 for fast neutrons)
Tabletop: Contingency reference only at current energies, but the boron-surface trick (borated HDPE sheet lining a duct) is the cheap fix if any future neutron source term streams through an enclosure penetration.
-
Interlock philosophy: the system exists to catch a minor lapse of memory or a wandering visitor, so keep it as SIMPLE as practical, subject personnel to minimum hindrance (or they will defeat it), make the temptation to short-circuit small — and never let an open interlock be remade from the console; someone must physically go to the position of the break and verify the hazard is gone.
simple + low-friction + no remote remake of a broken interlock (reset at the point of break)Source, quote & tabletop applicability
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.
Tabletop: 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.
-
Select interlock COMPONENTS with the same care as the protection system itself — only heavy-duty industrial-type limit switches, never light-duty switches — and account for the environment (radiation and corrosive ozone attack contacts), backed by frequent testing and routine maintenance.
heavy-duty industrial limit switches only; scheduled interlock test + maintenanceSource, quote & tabletop applicability
only heavy duty industrial type limit switches should be employed, avoiding light duty switches to insure durability and reliability.
Tabletop: 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).
-
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 & tabletop applicability
Teflon 5 x 104 ... Phenolic, Glass laminate >1 x 1010 ... Aluminum Oxide 1 x 1012
Tabletop: Counterintuitive and worth flagging in the next machine's design notes: PTFE, the amateur's default HV insulator, is the most radiation-fragile material on the list. Fine at the reference machine's dose rates, but in-chamber insulators near a future target station are better as ceramic or glass-filled phenolic.
-
Fail-safe circuit logic follows failure statistics: a BREAK is more likely than a spurious short, so require a complete path / presence of a signal (energized relay) to PERMIT operation, and let any open circuit or loss of signal disable the beam.
permissive = continuously energized circuit; any open/loss-of-signal -> beam offSource, quote & tabletop applicability
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.
Tabletop: The normally-energized interlock-loop architecture verbatim — the product safety chain should be a series loop holding an RF/HV enable relay closed, so broken wires, unplugged connectors, and power loss all land in the safe state. Also the right pattern for the 1-uA beam-current interlock.
-
Design so that every ANTICIPATED malfunction (power loss, broken wires, sticky relays, switches failing to make contact) results in shutting off the interlocked function; accept that fail-safe systems halt operations on false trips — "the loss of operating time must be preferred to the loss of safety" — while fail-active components of sufficient utility (pressure floor pads) may join an otherwise fail-safe design; add latching memory (SCR-style) so a door-open event persists until an operator reset even after the door recloses.
enumerate failure modes -> all anticipated failures trip safe; latching event memory + manual reset; downtime > riskSource, quote & tabletop applicability
For interlocks, however, the loss of operating time must be preferred to the loss of safety.
Tabletop: 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.
-
Interlock BYPASS is inevitable (maintenance, special setups), so pre-write the procedure: a two-key system with the second key held by the Radiation Safety Officer prevents one person from disabling a personnel-safety interlock, and a definite, REDUNDANT procedure must insure the bypass is corrected before release for routine operation — more important than the bypass procedure itself.
bypass = 2-key (operator + RSO) + written restore-verification procedure with redundancySource, quote & tabletop applicability
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.
Tabletop: For a school machine the "RSO key" is the instructor key — service mode needs a physically distinct credential from the student/operator credential, plus a restore checklist entry before the next class runs. For the home lab, a logged service-mode jumper with a checklist line does the same work.
-
Emergency-stop switches: locate and identify them so their purpose is immediately evident to employee and visitor alike; a person overlooked inside during lockup must be able to POSITIVELY defeat the beam (not just kill some unassociated apparatus), and must never hesitate for fear of criticism over shutting down the wrong equipment.
e-stops obvious to visitors, positively beam-defeating, hesitation-free cultureSource, quote & tabletop applicability
A person overlooked during the search before lockup must be able to positively defeat the beam instead of ineffectively shutting down some unassociated apparatus.
Tabletop: 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.
-
Search-before-lockup: after completing the lockup procedure the person performing the safety survey must have SEEN every position capable of hiding a man; overlooked maintenance workers in usually-unoccupied spots are the classic incident, and the number of survey stations must grow with facility complexity.
pre-startup search must sweep every human-capable volume; stations scale with complexitySource, quote & tabletop applicability
After completion of the lockup procedure the person who has performed the survey should have seen every position capable of hiding a man.
Tabletop: Trivially satisfied on a benchtop machine but a REAL checklist line for any walk-in enclosure a customer institution builds; belongs in the product installation manual's commissioning procedure.
-
Standardize alarms and status displays: distinct audible signatures per meaning (LRL: chimes = radiation, horn = beam on, steady klaxon = evacuate), light colors representing constant meanings with all ambiguity resolved, positive wording throughout, routine test alarms at programmed times — but not so frequent that they cry wolf — and status readily visible so users act with justifiable confidence.
one meaning per sound/color, consistent wording, scheduled (not excessive) alarm tests, visible interlock statusSource, quote & tabletop applicability
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).
Tabletop: 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.
-
Massive shielding doors carry their own hazards: slow travel with great momentum (engineer the stopping to avoid trapping personnel or cracking walls), and every door must be manually openable from BOTH inside and outside after a loss of power; doors must shield at least as well as the adjoining wall.
door shielding >= wall; manual egress inside+outside under power loss; engineered decelerationSource, quote & tabletop applicability
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.
Tabletop: Scale-invariant egress principle — even an interlocked benchtop lid or a walk-in enclosure door must never imprison anyone on power loss; spring-return or manually liftable closures only.
-
Two Morse principles anchor protection-system design: (1) human safety should not be entrusted to one or more persons following a written routine; (2) even mechanized systems become routine after a time and hence may lose their effectiveness — hence deliberate "nuisance modifications" to re-awaken attention, and guards-instead-of-interlocks judgments made only with extreme care.
no safety-by-checklist-alone; periodically perturb routine (nuisance modifications) to fight habituationSource, quote & tabletop applicability
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.
Tabletop: 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.
-
Accelerator accident history since 1944 shows two common threads — lack of education of the NON-accelerator worker (e.g., maintenance personnel) and the short-circuiting of established safety procedures — and every recorded potentially-lethal dose involved HIGHLY EXPERIENCED personnel, so run continuous education, not one-time training.
accident causes = untrained bystander OR bypassed procedure; experience does not protect -> recurring educationSource, quote & tabletop applicability
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.
Tabletop: 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.
-
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 & tabletop applicability
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.
Tabletop: The counterweight to over-trusting the product machines' interlock chains — the curriculum's radiation-safety module is a safety SYSTEM component, not documentation overhead.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
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 on top of ozone's toxicity; radiation-damaged electrical insulation likewise raises fire/shock risk and warrants more frequent inspection than normal wear.
LN2 trap + radiation -> condensed O2 -> O3 concentrate on warm-up = explosion hazard; inspect irradiated insulation on shortened scheduleSource, quote & tabletop applicability
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.
Tabletop: Directly applicable to any LN2 cold trap on the diff-pump line if machine energies ever rise, and worth a line in ops procedures now — never let a trap that has sat in a radiation + discharge environment boil dry unattended (ozone also forms from HV corona, no radiation needed).
-
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 & tabletop applicability
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.
Tabletop: A 1972 acknowledgement, with conditions, of the small-facility reality in which one person is both operator and radiation safety officer. The conditions transfer to any teaching installation, and documentation should name the RSO-equivalent role and its decision rights.
-
Ozone is the dominant toxic gas from irradiating air (G = 13.8 +- 0.7 molecules O3 per 100 eV in oxygen radiolysis, X-ray value); predict cell concentration with production rate 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, and set DELAYED-ENTRY times so personnel enter only below ~0.1 ppm.
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 & tabletop applicability
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.
Tabletop: At the reference machine's beam powers the radiolytic term is negligible, but the SAME balance-production-against-exhaust model covers corona/discharge ozone from the HV and RF systems in a closed basement — nose-level ozone (odor threshold ~0.01-0.05 ppm) is the practical indicator, and 0.1 ppm the 1972 occupational line.
-
Ozone decays by first-order kinetics with an effective indoor "half-life" of ~35 minutes (alpha_1 = 3.03e3 s, measured at Rensselaer, Yale, and Natick) — using the without-irradiation lifetime is conservative — so ventilation OR a half-hour wait, not time alone in seconds, clears an ozone-loaded room.
O3 half-life ~35 min indoors (alpha_1 ~ 3.03e3 s); C1 = C*exp(-(v1/V+1/alpha_1)*t1)Source, quote & tabletop applicability
noted an approximate "half-life" for the ozone in their measurements at Rensselaer and Yale of 35 minutes.
Tabletop: Practical basement rule: if ozone smell appears during an RF/HV session, a ventilated half-hour cooldown drops it ~2x, an hour ~4x — and the number lets the ops checklist give a real re-entry wait instead of "air it out."
-
Monitor exhaust filtration by PRESSURE DIFFERENTIAL: serious changes in delta-P across the filter bank indicate either clogging or rupture, and a detector (ion chamber or scintillator) mounted near the filter face continuously watches trapped-activity buildup — together preventing particulate release without sampling.
filter health = delta-P trend (clog = rising, rupture = falling) + detector at filter faceSource, quote & tabletop applicability
Serious changes in the pressure differential on the up and down stream sides indicate that the filter has either clogged or ruptured.
Tabletop: 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.
-
Air-activation species (13N, 15O) from (gamma,n) are a design concern ONLY for electron accelerators above about 15-20 MeV; 16N (7.1 s) matters solely inside recirculating ducting — below those thresholds, accelerator air handling is an ozone problem, not a radioactivity problem.
air activation ((gamma,n) on N/O) requires E > ~15-20 MeV; 16N (7.1 s) only a ducting concernSource, quote & tabletop applicability
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.
Tabletop: Cleanly scopes air activation OUT of every current and planned program machine (the reference machine and a next machine, tiny, the 700-keV synchrotron) — cite this when a reviewer asks about activated air, and focus the air-handling design on ozone instead.
-
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 & tabletop applicability
The process is a trial and error search, with general guidelines and test criteria for success.
Tabletop: Directly transferable design-process pattern for any pole/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 instead of a target field profile.
-
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 & tabletop applicability
first evaluated using the Smith-Garren formula, checked at critical places, especially at larger r, by exact orbit motion computer solutions.
Tabletop: Exactly the field-solver-plus-orbit-tracker pipeline an amateur design can run; the Nevis precedent says spend the expensive tracking only where the cheap formulae are least trustworthy.
-
Build adjustability into pole/sector iron: removable edge pieces and center tips for post-mapping touch-up machining, bolt patterns allowing azimuthal repositioning, and locating pins so a good position can be reproduced after disassembly.
removable edges + removable center tips + slotted repositioning + locating pinsSource, quote & tabletop applicability
a final "touch up" machining of these pieces, with the final iron in place on the basis of magnetic field mapping studies.
Tabletop: 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.
-
Harvest resonance lines to avoid from other machines' documented beam-loss experience before fixing the tune trajectory; Nevis avoided (3vr-vz)=3 and (vr+3vz)=2 solely because ORIC saw losses there.
keep (vr,vz) trajectory clear of (3vr-vz)=3 and (vr+3vz)=2 (plus the standard low-order lines)Source, quote & tabletop applicability
alerted by the ORNL studies of observed beam loss in the ORIC cyclotron to try to avoid
Tabletop: 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.
-
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 & tabletop applicability
a "Ferrofluidic" vacuum seal having ~ 0.005 in. radial gaps in which a ferrite loaded low vapor pressure liquid is held by magnetic fields
Tabletop: Transferable component class, already commercial in 1971 and cheap today — the clean answer any time an accelerator mechanism (chopper, rotating target, variable capacitor) needs rotary motion through the chamber wall.
-
Give mechanically dirty subsystems (rotating machinery, sliding parts) their own separately pumped vacuum envelope, coupled to the beam chamber only through insulating feedthrough barriers, so their gas load and debris never see the main volume.
separate turbopumped housing per mechanism + feedthrough insulator as vacuum partitionSource, quote & tabletop applicability
The capacitor housings have separate vacuum systems using turbomolecular pumps. RF feed through insulators separate them from the main cyclotron vacuum system.
Tabletop: Scales down well — a differentially pumped appendage for any mechanism (the reference machine already does this in spirit with the diff-pumped source region) keeps ion-gauge-clean chamber pressure honest.
-
Couple RF to rotating elements without sliding contacts: feed the stationary electrode, and hold the rotor near RF ground through small high-capacitance face gaps, 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 & tabletop applicability
the rotors are at low RF due to their < 0.010 in. high capacitance face gaps to ground
Tabletop: General lesson for any rotating RF machinery (choppers, tuners) at any power level; the rotating-capacitor FM tuner itself is synchrocyclotron-specific and does NOT transfer to a fixed-frequency tabletop machine.
-
When a resonator must tune over a band, taper the transmission-line characteristic impedance along its length to minimize the variable capacitor's required Cmax/Cmin ratio, and budget for structure inductance raising the effective Cmax at the low-frequency end.
Nevis: Z0 ~6 ohm -> ~2 ohm -> 8 ohm profile gave Cmax/Cmin = 6.5 nF / 1.3 nF (measured at 1000 Hz)Source, quote & tabletop applicability
The basic variation of line Zo along the resonator tends to minimize the capacitor Cmax/Cmin ratio needed.
Tabletop: FM machinery itself does not transfer, but the impedance-profile trick applies to any tunable tank, and to any RF cavity that needs a swept or trimmed frequency range.
-
Choose the resonator mode/geometry so that tuning and mechanical elements sit outside the main vacuum chamber, shielded from both magnetic field and radiation; iron housings (2 in. at Nevis) can finish the magnetic shielding of moving parts.
half-wave resonator puts voltage node / tuner outside chamber; 2-in. Fe housing shields rotorsSource, quote & tabletop applicability
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
Tabletop: 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.
-
Establish all adjustable RF-system parameters (tuning range, mode spectrum, coupling ratios, voltage distribution) on a reduced-scale model plus computer calculation before committing to full-scale construction; also verify the beam-excited cross mode stays clear of harmonics of the main mode.
1/2-scale RF model + computation -> full-scale build; cross mode kept well below 2x main mode over tuning rangeSource, quote & tabletop applicability
The design has used a 1/2 scale model, in conjunction with detailed computer calculations, to establish all parameters which can be varied
Tabletop: 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.
-
DC-float the dee/resonator and apply a negative bias sufficient to suppress multipacting; the bias sweeps free electrons out along B faster than they multiply and returns surface secondaries to their electrode promptly.
Nevis planning value: dee DC bias -500 to -2000 V (Part II, p.48)Source, quote & tabletop applicability
The dee resonator will be dc floating so a negative bias of amount sufficient to control multipacting can be applied.
Tabletop: Directly relevant at a next machine's planned 5-13 kV dees where multipactor bands are widest; corroborates the glow corner's multipactor-mechanism rules with a 1971 operating-lab remedy and a concrete bias magnitude to scale from.
-
Commission in activation-safe stages: first debug source and central region with the beam stopped at small radius in low-Z (graphite) targets below neutron-production conditions, 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 & tabletop applicability
stopping the beam at r < 10 in. radius in graphite targets. This avoids neutron production and induced cyclotron radioactivity
Tabletop: The staging discipline transfers to every machine even where activation does not — low-duty, small-radius-first commissioning is also how you protect septa, collectors, and instruments; at a few hundred keV and above the activation logic itself starts to matter.
-
Plan radiological teardown work formally: let components cool for weeks, strip auxiliary equipment first, and track per-worker weekly dose against a target — Nevis held a 2000-ton machine teardown to under 100 mrad/week per worker.
cooling delay + staged strip-down + weekly per-worker dose trackingSource, quote & tabletop applicability
with all workers averaging below 100 mrad/week, and most below 25 mrad/week for the 10 weeks of this activity
Tabletop: 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.
-
Line surfaces struck by lost beam with non-activating material (Nevis used marble pole liners) so that stray protons deposit in low-activation stone rather than in iron and copper.
marble (CaCO3) liners over pole/sector iron in beam-loss regionsSource, quote & tabletop applicability
We expect to use marble pole liners where possible, as in the past, to reduce sector iron, etc., activation
Tabletop: Below ~few-MeV protons activation is negligible, so this is a higher-energy note — but the general idea (choose what lost beam hits) already applies to sputter contamination and outgassing on any machine.
-
When a calculation needs an empirical constant (here the effective image factor of saturated pole iron), measure it directly with a precisely known conductor configuration in the real field environment rather than taking a handbook value.
septum fields = conductors + 5 image sets scaled by (mu-1)/(mu+1); measured fit gave mu = 5 to <1%Source, quote & tabletop applicability
The value of mu used was found experimentally by measuring the field from a precisely known configuration of conductors
Tabletop: A model-calibration pattern the FEMM-based pipeline should copy — one deliberate known-geometry measurement (a wire loop, a known coil) in the actual gap pins the permeability/saturation assumptions the whole field model rests on.
-
Taper an extraction-channel septum from thin at the entrance to thick downstream — once turn separation grows, thickness is free — cutting resistive power severalfold and multiplying coolant flow at the same supply pressure.
Nevis: 0.125 in. entrance -> 0.600 in. by 16 in. along channel; power 160 kW-equivalent -> 40 kW (4x)Source, quote & tabletop applicability
This septum will use only 40 kW of power, a factor of four smaller than if the original thickness were kept to the end
Tabletop: 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 deflector septum or foil design on a next machine.
-
Interlock actively cooled beam-intercepting conductors individually: give each element its own temperature sensor on the coolant that trips the supply, plus continuously filtered and de-ionized water, because a cooled conductor melts within seconds of flow loss.
per-wire thermocouple -> fast current trip; filtered + de-ionized cooling loopSource, quote & tabletop applicability
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
Tabletop: Per-element thermal interlocks scale down perfectly — the same philosophy belongs on the next machine's RF amplifier dummy load, water-cooled dee stubs, and any powered septum, and matches the fail-safe interlock doctrine in the 1974 ORNL safety survey.
-
Use adiabatic RF manipulation to damp longitudinal spread: park the beam where df/dt ~ 0 and turn the RF amplitude off slowly (linearly over hundreds of microseconds) so phase-oscillation energy spread shrinks near-adiabatically (~3x predicted at Nevis).
slow linear V_RF turn-off at df/dt ~ 0 "parking frequency" -> ~3x reduction in phase-oscillation dESource, quote & tabletop applicability
a slow linear reduction (turn off) of the RF amplitude there will result in a near adiabatic spreading out of the phase angle
Tabletop: Meaningless for a fixed-frequency CW tabletop cyclotron; it belongs to swept-frequency machines, where adiabatic capture and slow parameter ramps are the RF-program design space.
-
Buy shielding with geometry before mass: aim the primary beam stop away from occupied areas, take secondary beams off at ~90 degrees where neutron spectra are soft, and put multiple bends between production targets and experimenters.
beam stop aimed away + 90-degree takeoff + >=2 bends per secondary lineSource, quote & tabletop applicability
Since the underground beam stop is aimed away from the experimental areas, this greatly eases shielding, and subsequent background problems
Tabletop: 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; a first-class rule for any facility layout.
-
For forward-cone neutrons above ~100 MeV, attenuation flattens to roughly a factor 2 per 6 in. of iron (or ~18 in. ordinary concrete), while at >=90 degrees the softer (<100 MeV) spectrum gains nearly a factor 10 per 6 in. Fe — shield thickness must be budgeted per direction.
>100 MeV forward cone: x2 per ~6 in. Fe (~18 in. concrete); >=90 deg: ~x10 per 6 in. FeSource, quote & tabletop applicability
require - 6 in. Fe (or the equivalent) for each factor of 2 attenuation
Tabletop: Pure high-energy datum — no tabletop relevance except as a worked example of directional shielding budgets, but it anchors the energy scaling.
-
In any radiation environment, design internal components for blind replacement — Nevis made every dee support insulator removable and replaceable by remote handling tools from behind shields, accepting extra design effort up front.
activated-region components = pin-located, tool-accessible, removable without entering the chamberSource, quote & tabletop applicability
all support insulators have been designed so that they can be removed and replaced by remote handling tools.
Tabletop: 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.
-
Build accelerator safety interlocks to the 1974-era baseline or better: solid-state fail-safe logic with self-checking circuits, replacing electromechanical relays, so that component failure 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 & tabletop applicability
The trend seems to be toward more elaborate systems which utilize solid state devices, fail-safe circuitry and self-checking circuits.
Tabletop: Directly actionable for the next machine / tiny controls spec — an amateur interlock chain (door, HV, RF-enable, radiation monitor) should be fail-safe and self-testing; what was state of practice in 1974 is trivially cheap in 2026.
-
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 & tabletop applicability
techniques of dealing with problems such as relay races, sneak grounds and power-supply crossties
Tabletop: Fully transferable and cheap — one deliberate review pass asking "what unintended path can energize the HV or open the shutter" on the interlock schematic covers the classic amateur failure of a shared ground defeating an enable line.
-
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 & tabletop applicability
fixes the half-value thicknesses of ordinary concrete for neutrons from cyclotron targets at approximately 10 cm
Tabletop: The corpus's first concrete (literal) shielding number for MeV-class cyclotron neutrons — below the (p,n)/(d,n) thresholds the reference machine produces none, but this is the sizing constant the moment any future machine or D-beam work crosses into neutron production; measured for far harder spectra than an amateur will make, hence conservative.
-
Formalize the safety function as the program grows: a named safety officer, a review committee distinct from the builder, and written guidelines — the 1974 trend driven by accumulated accident experience, not regulation alone.
safety officer + independent review + written program (models in NBS 107, TID-23992)Source, quote & tabletop applicability
There is often a safety officer appointed. Many installations have safety review committees.
Tabletop: For a one-person program the transfer is external review — the archive's established cross-review protocol is exactly this committee function; for the planned educational-accelerator business a named safety officer and written program become literal requirements.
-
Adopt ALARA (As Low As Practicable) as the exposure design philosophy — not merely staying under limits but reducing further wherever technology and economics permit — and recognize it works only as a standing management commitment, since "practicable" is deliberately non-numerical.
design target: exposures as far below limits as practicable (AEC Reg. Guides 8.8/8.10 gloss on 10 CFR 20)Source, quote & tabletop applicability
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
Tabletop: The governing philosophy (now ALARA in modern regulation) that any licensing narrative for the business plan must speak fluently; for the home program it means shielding and interlock decisions justified as "as low as reasonably achievable", not "under the limit".
-
Measure shield attenuation with the machine itself as the source: place a slab of the candidate material (3 ft x 3 ft x thickness) in front of a detector recessed in a cavity in a thick concrete "igloo", and normalize every detector reading to a fixed beam monitor so source fluctuations divide out of the attenuation curve.
attenuation = (detector/monitor) vs slab thickness; slab 3'x3', detector in 1.5-inch cubical cavitySource, quote & tabletop applicability
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]
Tabletop: 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.
-
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 & tabletop applicability
The monitor and detector employed were aluminum-walled ionization chambers, with DC Amplification, indicating on microammeters placed outside the magnetic field of the cyclotron.
Tabletop: Analog meter movements, photomultipliers, and many GM counters misread in a stray field of even tens of gauss; separate the sensing volume from the readout and keep the readout outside the fringe field.
-
Expect transition (buildup) effects at the front face of any shield: attenuation only becomes exponential after the radiation reaches equilibrium with the secondaries it generates in the absorber, so fit half-value thicknesses to the displaced linear portion of the curve, never to the first readings behind thin 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 & tabletop applicability
The transition effects occur as the neutron beam approaches equilibrium with the secondary and scattered particles produced in the absorbing medium.
Tabletop: A dosimeter reading just behind the first inches of shielding measures the buildup region, not the attenuation slope; thin-shield tests systematically misestimate what a thick shield will do in either direction.
-
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.
dose behind paraffin layer = up to 2x dose entering it, when preceded by high-Z materialSource, quote & tabletop applicability
Paraffin yields a transition increase of 60% following Fe, and of 100% following Pb with similar geometry.
Tabletop: When adding polyethylene or paraffin outside a metal chamber wall, a survey reading taken between the layers or behind too thin a hydrogenous layer can exceed the bare-wall reading; the hydrogen layer must be thick enough to absorb the recoil protons it creates.
-
Threshold-activation detectors sandwiched between absorber slabs give cleaner attenuation half-values than ionization chambers: they are insensitive to the low-energy scattered background, immune to magnetic fields and electronics drift, and yield exponential curves with better precision.
activation of a threshold-reaction foil vs absorber depth -> half-value thickness; Moyer used C12(n,2n)C11, threshold ~20 MeVSource, quote & tabletop applicability
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.
Tabletop: 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.
-
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 & tabletop applicability
Because of the geometry employed, these measurements are neither a true determination of pure scattering nor pure absorption.
Tabletop: Handbook removal cross sections assume good (poor-geometry-corrected) conditions; a home measurement in tight geometry will read more optimistic than broad-beam reality because scattered radiation misses a small detector.
-
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 & tabletop applicability
one should seek substances which combine high density with low atomic number. Among convenient and practical materials none would seem better than concrete.
Tabletop: The shadow-effect argument is a >100 MeV argument, but the conclusion strengthens at low energy where hydrogen elastic scattering dominates moderation - concrete, water, and polyethylene beat any metal for neutron shielding per dollar and per pound.
-
Shield for machine-generated loss points, not just the target: beam grazing the interior of the dee sprayed fast neutrons in considerable intensity through 180 degrees of azimuth, in addition to the forward cone from the probe target.
Source, quote & tabletop applicability
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.
Tabletop: Wherever beam is lost - dee edges, septum, probe stalk, chamber wall - is a source; a survey plan that only looks downstream of the target will miss most of the emission solid angle.
-
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 & tabletop applicability
Measurements with a BF3 proportional counter have indicated diffusion of slow neutrons through various access openings from the enclosure.
Tabletop: Cable ways, viewport lines-of-sight, and door gaps are the paths that matter once any bulk shielding exists; thermal-neutron instruments answer a different question than fast-neutron ones and both belong in a survey.
-
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; dose scales linearly with current at fixed geometrySource, quote & tabletop applicability
These quoted measurements are made with Al-walled ionization chambers, and correspond to a deuteron beam of about 0.2 x 10-6 amp.
Tabletop: 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.
-
Scale-model law for RF resonators: 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 therefore needs 1.4x the proportional power for a given dee voltage — coupling taps and loops in the model must pick up 1.4x the relative voltage.
f_model = s*f_full, L,C /s, Q_model = Q_full/sqrt(s), P_model = sqrt(s)*P_full for equal V (s = scale factor 2 for half scale)Source, quote & tabletop applicability
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.
Tabletop: Bench-model a dee-stem or resonator geometry at reduced size before cutting full-size copper; apply the sqrt(scale) Q correction before comparing model power and coupling measurements to full-scale predictions.
-
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 electron transit time at the scaled frequency falsified oscillator behavior, then chose 1/2 scale where an Eimac 304TL (1200 V, 600 mA) scales the 9C21 (12 kV, 6-8 A) faithfully.
model frequency must stay low enough that tube transit-time effects remain negligibleSource, quote & tabletop applicability
It was not excited satisfactorily due to the fact that at 100 megacycles the transit time effects were quite noticeable on the fundamental mode.
Tabletop: Cold measurements (network analyzer) scale exactly, but any POWERED model test needs a driver whose parasitics and transit time scale with the geometry, or the model will exhibit modes the real system never sees and vice versa.
-
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 & tabletop applicability
dimensions can be calculated fairly exactly whereas in the system shown in Figure 5 one must depend on model tests (which are safer anyway).
Tabletop: 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.
-
Take a mode census before applying power: excite the cold system with a separate, loosely coupled oscillator, map the voltage distribution of every resonance, then kill unwanted modes with wavetraps — a pair slightly staggered in tuning covers a frequency band; six wavetraps were needed to clean one octave.
Source, quote & tabletop applicability
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.
Tabletop: 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, and a dee spark momentarily retunes the system into modes the clean census missed.
-
Suppress an unwanted mode by making it lossy rather than by shifting it: grounding the rotor supports forced the wrong modes to drive heavy currents through deliberately high-resistance supports, so they simply fail to oscillate in favor of the high-Q correct mode.
Source, quote & tabletop applicability
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.
Tabletop: Mode-selective damping - resistance placed at a current maximum of the unwanted mode and a current null of the wanted one - is cheaper and more robust than trying to tune the parasite out of band.
-
Any long conductor is a transmission line: metal support stems mounted on insulators act as open quarter-wave lines with the voltage maximum at the open (insulator) end — MacKenzie's rotor supports would have stressed their insulators at about 3x the rotor voltage.
open-ended support of length near lambda/4 multiplies RF voltage at its free end; here ~3x rotor voltageSource, quote & tabletop applicability
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
Tabletop: Check the electrical length of every support, cooling line, and instrument stalk inside the RF volume; a mechanically convenient standoff can sit at a voltage antinode and flash over at dee voltages its rating should easily hold.
-
When dee voltage dips to zero at one specific frequency, hunt for a hidden resonant structure absorbing the power: MacKenzie traced such a null at 20 Mc to the meshed condenser teeth acting as a folded transmission line — overlap length times number of meshed teeth came to a half wavelength.
folded-line parasitic resonance when (tooth overlap) x (number of meshed teeth) ~ lambda/2Source, quote & tabletop applicability
The oscillating circuit actually is a long folded transmission line consisting of the two rows of meshed teeth.
Tabletop: The diagnostic transfers whole - a sharp, frequency-specific dead spot in dee voltage means some conductor assembly (screen, liner seam, feedthrough array) is resonant there; fix it by shortening or breaking up the structure, not by driving harder.
-
Prove a parasitic stays out of band across the whole tuning range by checking the worst case: if the parasitic's frequency is still above the fundamental at the tuning extreme that brings them closest, it stays above at every intermediate setting.
Source, quote & tabletop applicability
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.
Tabletop: For any tunable element (trimmer panel, movable shorting plane), verify mode separation at the extreme of travel where the wanted and unwanted modes converge; monotonic behavior between extremes lets one measurement clear the whole range.
-
Couple the drive at a point whose voltage is insensitive to tuning: on the 3/4-wave system the stub-line voltage stays within ~40% of the dee voltage over about a 2:1 frequency range, so an oscillator tapped there needs no retuning of its coupling as the system sweeps.
Source, quote & tabletop applicability
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.
Tabletop: Even a fixed-frequency machine drifts with thermal expansion and plasma loading; feeding at a voltage-stable point of the resonator keeps drive impedance roughly constant as the resonance moves.
-
Empirical procedure for locating a drive tap: start at the open (high-voltage) end of the line and slide toward the shorted end until the tube draws rated plate current at rated plate voltage — that point is the impedance match.
Source, quote & tabletop applicability
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.
Tabletop: The same walk-the-tap procedure sets link or tap coupling on any dee tank - begin overcoupled-safe at high impedance and converge on rated loading, rather than computing a tap position and committing to it.
-
Build small mechanical length adjustment into every coupling line instead of calculating exactly: a factor-of-1.6 uncertainty in tube capacity moved the required line length only 15 inches, which is within what end effects and bends cause anyway.
Source, quote & tabletop applicability
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
Tabletop: Design connection lines and stubs with a sliding section or trombone worth a few percent of a wavelength; the calculation gets you to the right neighborhood and the adjustment does the rest.
-
In a grounded-grid drive chain, control phase shift by oversizing the grid-filament (input) capacity so the reactive current swamps the in-phase emission current; MacKenzie held the total filament-plus-plate-line shift to about 25 degrees, beyond which efficiency degrades seriously.
make I_reactive = V*omega*C_gf >> I_emission; total drive phase shift <= ~25 deg tolerableSource, quote & tabletop applicability
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.
Tabletop: The mechanism matters for any self-excited tube oscillator on a dee - drive phase error costs efficiency quadratically; padding the input capacity is the one-component fix, and the graphical Shanklin incident/reflected-wave construction (Fig. 15) checks it.
-
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 & tabletop applicability
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.
Tabletop: Dee power scales as voltage squared - measure watts-per-volt-squared on the bench, correct for Q, and the amplifier requirement for any target dee voltage falls out; joint quality and surface material shift Q enough to budget for.
-
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 & tabletop applicability
Total Operating Time 831.3 ... 60.1 ... Outage Total 551.2 ... 39.9 ... Scheduled Operating Time 1382.5
Tabletop: A run log that records why each session ended, in fixed categories, turns anecdote into a failure Pareto within a year; expecting 40% downtime even with full-time staff calibrates what a spare-time machine can achieve.
-
Power supplies and vacuum dominate unscheduled downtime: 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%). Reliability investment goes to supplies and pumps first.
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 & tabletop applicability
Vacuum 128.6 ... 9.3 ... R. F. 22.1 ... 1.6 ... Power Supply 140.4 ... 10.2
Tabletop: Matches the failure record of small machines - the exotic subsystems (RF, source) are not the availability drivers; unglamorous supply and pump maintenance is where uptime is bought.
-
Budget for transition overhead: start-up/shutdown consumed 5.6% and beam tuning another 4.0% of scheduled time — roughly a tenth of the machine's life spent getting into and out of running condition. Longer uninterrupted runs amortize this fixed cost.
NRL: start-up/shutdown 77.5 h (5.6%) + beam tuning 55.0 h (4.0%) of 1382.5 scheduled hoursSource, quote & tabletop applicability
Beam Tuning 55.0 ... 4.0 ... Start Up and Shutdown 77.5 ... 5.6
Tabletop: Pump-down, filament conditioning, and field settling are a fixed tax per session; batching experiments into fewer, longer sessions raises beam-on fraction more than any hardware upgrade of similar effort.
-
Develop in parallel with operation, but batch major modifications into a scheduled engineering shutdown rather than taking the machine down piecemeal: NRL ran routine improvements alongside physics and reserved one 360-hour shutdown for the big changes.
Source, quote & tabletop applicability
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.
Tabletop: 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.
-
Latch and display the FIRST cause of every trip: some faults (magnet overtemperature) clear themselves by cooling off after the trip, before the operator can find the sensor that caused it — so the protection system must store the fault location, not merely interrupt.
Source, quote & tabletop applicability
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.
Tabletop: Any interlock chain needs first-fault capture - even a latching relay or logged timestamp per sensor - or intermittent faults (thermal, flow, vacuum burps) become undiagnosable ghosts that waste whole sessions.
-
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 & tabletop applicability
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.
Tabletop: Hard-wire the safety-critical chain (radiation, HV enclosure, cooling on powered magnets) so it cannot be acknowledged away, and give everything else a bypassable alarm; a system where every fault stops the machine trains its operator to defeat interlocks.
-
Gate the beam by dropping dee voltage below the acceleration threshold - to roughly 50% of normal - rather than to zero: the reduced level still keeps the automatic tuning and dee-voltage regulation loops locked, so beam returns instantly and cleanly when full voltage is restored.
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 & tabletop applicability
the R. F. dee voltage was lowered to approximately 50% of its normal value which is less than the threshold voltage.
Tabletop: There is a dee-voltage threshold below which no ions survive to full radius; gating against it - by stepping the regulator reference, not by unkeying the RF - pulses beam for detector duty-cycle or background measurements without any retuning transient.
-
Protect big-tube filaments at both ends of the failure: ramp filament voltage slowly from zero so inrush current through the cold (low-resistance) filament never exceeds its limit, and trip the filament supply if current ever momentarily DROPS - a dip means an intermittent socket contact, after which reapplied full voltage hits a cooled filament.
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 & tabletop applicability
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.
Tabletop: Scales straight down to any transmitting tube or big thoriated filament - a soft-start (variac ramp or NTC inrush limiter) plus an undercurrent trip covers both the cold-start and the loose-socket failure modes that shatter filaments.
-
Gang mechanically what must track electrically: four tuning capacitors each on its own servo repeatedly lost synchronization and had to be removed and reset; one chain drive from a single motor eliminated the failure class outright.
Source, quote & tabletop applicability
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.
Tabletop: Wherever two adjustments must stay matched (paired trimmers, symmetric shorting planes), a shaft, chain, or belt enforces the constraint by construction; independent actuators plus software matching is a standing failure mode.
-
Measure dee-voltage modulation as a number and drive it down at the source: NRL defined it as peak-to-peak ripple as a percentage of peak RF, found the master oscillator itself contributed frequency-dependent amplitude and spurious components, and replacing it with a frequency synthesizer cut modulation from 1.5% to 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 & tabletop applicability
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%.
Tabletop: Dee-voltage ripple modulates turn energy and orbit phase; put the envelope on a scope, log the percentage, and remember the excitation source (a cheap signal generator's spurs included) is a candidate cause before blaming the amplifier or resonator.
-
Motion feedthroughs are a seal failure class of their own: chevron-stack elastomer seals on the source's radial and azimuthal drives were unreliable and short-lived; the durable replacement was two simple 1/4-inch cross-section O-rings, each in a polished, close-tolerance machined adapter ring properly fitted to the housing.
Source, quote & tabletop applicability
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.
Tabletop: For sliding/rotating shafts into the chamber, dual O-rings in polished glands (surface finish and land tolerance doing the real work) outlast fancier stack packings; seal geometry matters less than the finish it rides on.
-
Optically re-align the ion source to the median plane after every removal: NRL treated reinstallation as a survey operation, aligning the discharge aperture (0.09 x 0.50 inch slit) to the magnetic median plane and the dee electric field before pumping down.
Source, quote & tabletop applicability
the ion discharge aperture (0.09" x 0.50") was optically aligned with respect to the median plane of the cyclotron magnetic field and the electric field of the dee.
Tabletop: Source aperture height and tilt relative to the median plane set 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.
-
Magnetic forces on current-carrying structures deform them in service: the iron channel's internal copper walls collapsed whenever coil current exceeded 2000 A (found by remote instrumentation, costing ~60% of the extracted beam); the fix - G-10 glass-epoxy stiffeners - was verified by MEASURING deflection (0.002 inch at 3500 A) against the material elastic limit, and the balky drive motors were moved from 50 to 80 inches from the source, out of the field.
verify a structural fix by measuring deflection at above-operating excitation and comparing induced stress to elastic limitSource, quote & tabletop applicability
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
Tabletop: Every conductor near the pole gap feels J x B; thin walls, septa, and coil leads need either stiffening or a measured demonstration that deflection at full excitation stays elastic - and motors, encoders, and anything with a magnetic circuit belong outside the fringe field.
-
Cooling-water plumbing impedance can be the real limit on dee voltage: NRL could not reach high dee voltage at the top of the frequency range until a second return pipe separated the high- and low-pressure loops, raising anode flow from 42 to 60 gpm; a standby pump was then plumbed in parallel specifically to cut future outages.
shared return headers add series impedance to every branch; separate supply/return loops per pressure class; standby pump in parallelSource, quote & tabletop applicability
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
Tabletop: When an amplifier cannot hold rated dissipation, check hydraulic head losses in shared manifolds before derating the tube; and duplicating the single-point-of-failure pump is a reliability purchase the outage ledger justifies.
-
Availability benchmark from a mature research cyclotron: 1,680 hours of operation in one quarter — about 18 hours per day, sustained — with only four days of unscheduled loss.
1680 h / 92 days ~ 18.3 h/day operatingSource, quote & tabletop applicability
the cyclotron was in operation 1680 hours, or about 18 hours per day.
Harvard University Cyclotron Laboratory, Quarterly Progress Report, 1 June – 31 August 1964 — p. 1
Tabletop: An upper anchor for what cyclotron reliability can reach once a machine is mature and continuously staffed - useful for calibrating expectations against the NRL 60% figure from a machine mid-upgrade.
-
The accelerator's support equipment, not the accelerator, causes the downtime: the largest single loss of the Harvard quarter — three days — was the failure of the mechanical refrigerator serving the cold trap above the diffusion pumps.
Source, quote & tabletop applicability
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
Tabletop: Chillers, trap refrigeration, and compressed-air auxiliaries deserve the same spares-and-monitoring attention as the pumps they serve; when a trap warms, the machine is down just as surely as if the diffusion pump died.
-
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 & tabletop applicability
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
Tabletop: Oil charge in a diffusion pump depletes slowly by backstreaming and accident; a sight-glass check (or scheduled measurement) before each running block is the cheapest downtime insurance a diffusion-pumped machine can buy.
-
Batch invasive upgrades into one scheduled shutdown window: the Harvard quarter's only planned outage was a single ~1-week shutdown that installed the internal-beam pulsed-deflection apparatus.
Source, quote & tabletop applicability
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
Tabletop: Same pattern as NRL's engineering shutdown at a smaller scale - one planned vent, one reconditioning, all invasive work inside it; unscheduled opportunistic upgrades multiply pump-downs and conditioning time.
-
Check Faraday-cup material systematics by swapping stopping materials without breaking vacuum: Harvard modified the cup so blocks of different materials sat in electrical contact with the stopping plate, measuring collected charge per unit incident beam (normalized by an ionization chamber) versus stopper thickness and type.
collected charge per unit beam vs stopping-material Z and thickness = secondary-emission/scatter-loss systematic of the cupSource, quote & tabletop applicability
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
Tabletop: A Faraday cup's reading depends on its stopping surface through secondary emission and backscatter; measuring the same beam against two stopper materials bounds that systematic without any absolute reference.
-
Verify target areal-density uniformity before quantitative use: Harvard scanned a collimated beam across a carbon target and located the Bragg-curve tail at each point, resolving 0.2% density changes; reactor-grade rod stock showed 1%-per-quarter-inch gradients (2% near the edge) and was rejected in favor of pyrolytic graphite.
local areal density from range (Bragg-tail position) of a collimated beam through the target; sensitivity here 0.2%Source, quote & tabletop applicability
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
Tabletop: Ordinary graphite (and evaporated or pressed-powder targets generally) is not uniform at the percent level; a range-based or transmission-based density map of the actual target spot belongs in the error budget of any yield measurement.
-
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]; Corwin example 1e-7 A x 4.3e4 eV = 4.3e-3 W over A = 0.03 cm2Source, quote & tabletop applicability
In a typical charged particle experiment 100 na of beam loses 43 keV in a W = 380 ugm/cm2 PbCl2 salt target
Tabletop: 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.
-
Radiation limit (Corwin): a thin foil radiates from both faces, so the temperature needed to shed 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 requires 103 C but a more realistic e = 0.1 requires 345 C — and a thin film's effective emissivity may be lower still because the film is partly transparent.
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 & tabletop applicability
the target appears transparent and all of the radiating surface of a solid may not be present in a thin film.
Tabletop: 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 an equilibrium far above any evaporated-film melting point — which is why the spot must be enlarged, swept, or the target backed by a conductor.
-
Conduction limit (Corwin): heat conducted radially from a round beam spot of radius r_b to a target frame at radius r_t obeys P = 2*pi*k*h*dT / (1/2 + ln(r_t/r_b)) — note thickness h enters linearly. His example (h = 0.65 um, r_b = 0.1 cm, r_t = 0.64 cm): an insulator with k = 2 W/mC needs dT = 973 C to conduct the load, while a metal target (k ~ 200 W/mC) conducts the same load with only a ~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 & tabletop applicability
so a metal target could conduct the heat away with a 12 C rise in temperature.
Tabletop: 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. Thickness enters linearly — ultrathin films conduct almost nothing sideways.
-
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 of radius r_c 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 is dT = 65 C versus ~1000 C stationary, and conduction alone then holds 400 C — below the salt'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 & tabletop applicability
The equilibrium temperature of the beam spot circle for the high speed rotation limit is 65 C.
Tabletop: Target rotation or beam wobbling is worth an order of magnitude in survivable current on an internal target — mechanically trivial compared to any other way of buying the same factor, and Corwin built a three-target rotator to prove it.
-
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 (c = 0.068 cal/C g). 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 time is tau = r_b^2/alpha with alpha = k/(rho*c) the diffusivity (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))Source, quote & tabletop applicability
the temperature can rise only 39 C before that part of the target is out of the beam.
Tabletop: Sets the minimum useful rotation speed — the dwell time per pass must keep (P/mc) x t_dwell below the allowable rise, and successive passes must be spaced comparably to the diffusion time tau or the sawtooth ratchets upward.
-
Thickness scaling of the two limits (Corwin): making the target thicker leaves the conduction limit's temperature unchanged in his per-thickness formulation while the radiation-limited temperature rises (more power deposited, same radiating area). Thin targets are radiation-limited; thick ones become conduction-limited.
dE (hence P) grows with thickness; radiating area does not; conduction P grows with h in step with deposited powerSource, quote & tabletop applicability
With thicker targets the conduction limit will not change while the radiation limit will rise.
Tabletop: For a beam-stopping thick target the deposited power is fixed at I x E_beam regardless of further thickness, so the design moves entirely to the conduction side — mount the target material on a heat-sunk metal backing and the problem becomes an ordinary conduction calculation.
-
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 & tabletop applicability
perhaps the foil is damaged when there is radiation from a single spot only.
Tabletop: 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/IRML): rolling is by far the most material-conserving route to thin metal foils; vacuum evaporation reaches ultrathin elemental and thin/thick compound films but with efficiencies as low as ~1%; electroplating, casting/pressing, CVD and sputtering fill the corners. Their Table 1 (PDF 18-23) lists, element by element, which method reaches which ug/cm2 range in which backed/self-supporting form — read it before choosing a technique.
Table 1 legend: a = evaporation, b = rolling, c = electrolytic, d = casting or pressing; backing 1 = self-supporting, 2 = metal backing, 3 = thin carbonSource, quote & tabletop applicability
Rolling is by far the most conservative process with regard to material loss in preparing thin targets.
Tabletop: 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 & tabletop applicability
prevents the material from adhering to the rolls of the mill and enables a much thinner foil to be prepared
Tabletop: A jeweler's rolling mill plus shim-stock sandwich makes durable self-supporting metal targets (Table 1 shows most ductile metals reach 500-1000 ug/cm2 and up this way) — the natural route to robust backing foils and beam-stop targets.
-
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 & tabletop applicability
evaporation efficiencies of only 1% are obtained.
Tabletop: Budget isotope/material mass assuming ~1% of the charge lands on the substrate unless the geometry is engineered (tubular crucible, substrate close and directly above); crucible-evaporant chemistry (carbide formation, alloying) is chosen per material, not per convenience.
-
Characterize targets by areal density (ug/cm2 = atom count per area), never by linear thickness: microscopic voids and mixed crystal phases make any linear measurement converted through bulk density "grossly erroneous", while weight is directly proportional to the number of nuclei if stoichiometry is known (Adair & Kobisk).
areal density W [ug/cm2]; atoms/cm2 = W*N_A/M; linear h = W/rho only as estimateSource, quote & tabletop applicability
Linear measurements can lead to grossly erroneous values of atom content by virtue of included microscopic voids or a mixture of various crystal phases.
Tabletop: Yield calculations for a reaction target need atoms/cm2, which weighing gives directly; a micrometer or interference measurement of an evaporated film does not.
-
Weighing discipline (Adair & Kobisk): direct weighing reaches ~0.5% for samples above ~1 mg even in a normal lab, and 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 to 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 & tabletop applicability
In almost every case the agreement was better than +-1%.
Tabletop: A used 1-ug-precision microbalance plus the free NBS weighing protocol is a complete sub-percent target-mass QA capability; the protocol, not the balance, is what removes the drift that dominates single weighings of sub-mg samples.
-
Quartz crystal monitors are for in-situ rate and rough thickness only — calibrate them (ORNL used a vacuum microbalance; CBNM Mol made boron and uranium reference layers defined to +-0.3% that way), take the final thickness from direct weighing after removal, water-cool the crystal when the source environment exceeds ~300 C, and extend range for thick deposits with a rotating apertured wheel that samples the flux (Adair & Kobisk).
Source, quote & tabletop applicability
the ultimate measurement remains the direct mass determination of the target after it has been removed from the vacuum system.
Tabletop: Treat the crystal monitor reading as a process gauge (right range, right rate), never the certified thickness; the crystal is heat-sensitive, so radiant load from the source shifts its frequency exactly when the reading matters most.
-
Measure self-supporting film thickness by charged-particle energy loss (Adair & Kobisk): collimated alphas (241Am) through the foil, spectrum shift on a calibrated MCA, areal density = dE / stopping power. Works from a few ug/cm2 to several mg/cm2 — but published stopping-power data carry ~+-10% accuracy, which bounds the absolute result. Fission fragments (252Cf) resolve much thinner foils; beta transmission covers 40-500 mg/cm2.
W = dE / S(E), S in MeV cm2/g; alpha for ug/cm2-mg/cm2, fission fragments for ultrathin, beta absorption for 40-500 mg/cm2Source, quote & tabletop applicability
most of these data have an accuracy of ~ +-10%.
Tabletop: The one thickness method that needs no balance and works on a mounted film; a surface-barrier detector, a check-source alpha emitter, and an MCA are all standard home-lab equipment. Quote absolute thickness no tighter than the stopping-power tables allow.
-
Quick semi-quantitative gauges (Adair & Kobisk): a calibrated light densitometer reads carbon foil areal density in the 5-50 ug/cm2 range (useless above ~40-45 ug/cm2 where transmission saturates); low-geometry alpha or gamma counting assays radioactive deposits to ~+-1% with geometry factors down to 1e-7 for hot samples.
Source, quote & tabletop applicability
light intensity change is not a very useful technique for carbon films of thickness greater than 40 or 45 ug/cm2.
Tabletop: A photodiode and lamp sort carbon stripper/backing foils into thickness bins in seconds — calibrate once against weighed foils and use it as the incoming-inspection tool.
-
Map uniformity, not just mean thickness (Adair & Kobisk): scan the foil with a collimated alpha (or beta) beam position by position and draw a thickness topograph — a rolled 58Ni foil profiled this way showed max deviation +-1.5%. For radioactive deposits, scan with a small aperture and a silicon detector.
Source, quote & tabletop applicability
The uniformity of thin foils can be determined by scanning the foil with a collimated beam of alpha particles.
Tabletop: The same alpha energy-loss rig with an XY-translated collimator becomes a uniformity mapper; a single-point thickness number hides exactly the wedge or crystallite structure that ruins energy resolution (see Abele et al., this volume).
-
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 & tabletop applicability
it is equally important to know what species are present and in what concentration.
Tabletop: For a reaction-yield target the practical home-lab equivalents are material pedigree (certified purity), clean processing, and a background run on a blank backing — the backing and its contaminants (esp. carbon and oxygen) produce charged particles too.
-
Sputter from rolled isotopic foils when film properties matter (Adair & Kobisk): IRML modified a commercial sputtering system's target electrode from 12.7 cm down to 6.4 cm to accept small rolled isotope foils as sputter sources — "a very reproducible process" — trading deposition speed for material economy and reproducibility.
Source, quote & tabletop applicability
this method has proved to be a very reproducible process.
Tabletop: Shrinking the source electrode to match the available material is the general move — sputtering scales down to gram and even milligram stock gracefully, unlike melt-based methods.
-
Build the alpha source yourself (Thompson): expose an aluminum foil above an open 228Th bottle with the foil held at -300 V; recoil-ionized 220Rn plates onto the foil and decays to 212Pb (10.6 h half-life), giving alphas at 8786, 6090 and 6050 keV. ~10 h activation, ~24 h useful source life, no sealed-source procurement. Enclose the activator in a vented glove box because of the escaping radon.
228Th -> 224Ra -> 220Rn(+) collected at -300 V -> 212Pb (T1/2 = 10.64 h) -> alphas 8786 / 6090 / 6050 keVSource, quote & tabletop applicability
A large portion of the 220Rn gas is created as positive ions which are attracted by the -300 volt collecting potential
Tabletop: A thoriated source and a -300 V bias produce a fresh, essentially massless (recoil-implanted) alpha source on demand; the 2.7 MeV spread between the 212Pb lines self-calibrates the spectrometer with no external standard. Ventilation for thoron is mandatory.
-
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, then read target thickness from the channel shift of each peak with the target in place. Estimate fractional channel positions from adjacent-channel counts (peaks are Gaussian) — a 5-channel shift read to whole channels is only good to ~20%. Vacuum below 1e-4 torr, else detector-bias glow discharge can 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 & tabletop applicability
This is all the calibration which is necessary since now only energy shifts are of interest.
Tabletop: The whole rig is a surface-barrier detector, preamp, biased amp and any old 512-channel MCA — Thompson wrote it up precisely so small labs could build it; the differential (shift-only) design makes absolute gain calibration irrelevant.
-
Limits and free diagnostics of the alpha-loss method (Thompson): minimum measurable thickness ~ Tmin = 1.22*(30 + A) ug/cm2 (A = atomic number) for 10% accuracy at half-channel estimation on 512 channels; upper limit beyond 5 mg/cm2. Peak broadening beyond the no-target width flags nonuniformity; small UNSHIFTED satellite peaks flag pinholes. Composition must be known — use Bragg additivity for compounds.
Tmin = 1.22*(30 + A) ug/cm2 (10%, half-channel, 512 ch); S_compound = (1/M) * sum Ni*Ai*Si (Bragg additivity)Source, quote & tabletop applicability
They show up as small unshifted peaks in the energy spectrum.
Tabletop: One spectrum yields thickness, uniformity and pinhole count simultaneously — run it on every target before it goes into the machine and again after beam exposure to quantify damage.
-
Seed difficult condensers with a hexagonal-structure metal (Heagney & Heagney, MicroMatter): high-vapor-pressure hexagonal metals (Zn, Cd, Sb, As, Mg) stick poorly to amorphous substrates; pre-evaporating ~1 ug/cm2 of Be or Bi (both hexagonal, both mono-isotopic) from a side-by-side source — without breaking vacuum, to avoid oxidizing the seed — makes them condense uniformly with very high sticking coefficients.
seed layer ~1 ug/cm2 Be or Bi; dual boats so seed and evaporant deposit in one pump-downSource, quote & tabletop applicability
Zinc and cadmium condensed uniformly and with very high sticking coefficients.
Tabletop: The crystal-structure-matching trick generalizes — when a film refuses to stick or beads up, a nanometer-scale nucleation layer of a structurally compatible metal fixes it; good sticking also raises tolerance to substrate heating during deposition.
-
Reduce oxides in the evaporation boat with graphite (Heagney & Heagney): mix the metal oxide with spectroscopic-grade graphite powder, press to a pellet, heat in a tubular or e-beam boat — CO2 evolution on the pressure gauge tracks the reduction, and tens of mg reduce in tens of minutes while holding the chamber below 5e-5 torr. Works for Zn, Cd (which evaporate at reduction temperature), Fe, Cr.
MO_x + C -> M + CO2; chamber held < 5e-5 torr; rate limited by pumping speedSource, quote & tabletop applicability
the pressure gauge gives an indication of the rate of reduction
Tabletop: Lets a target come straight from a stable oxide powder with no separate metallurgy step, and the vacuum gauge doubles as the process monitor — no optical pyrometry needed.
-
In-situ reduction for calcium-class reactive metals (Thomas, ANL): press CaCO3 (or CaO) with a reducing agent such as Zr into a pellet, evaporate from a closed tantalum boat with heat shield and collimator at only 3.0 cm source-substrate distance — routine targets from FEW-MILLIGRAM isotope samples onto substrates as thin as 15 ug/cm2 carbon. And soften the roughing sequence: an abrupt roughing-valve opening blew every thin carbon substrate off its frame in their new commercial evaporator.
CaCO3 + heat -> CaO + CO2; 2CaO + Zr -> ZrO2 + 2Ca; closed Ta boat, 3 cm throwSource, quote & tabletop applicability
the valve opened with a POOMPF and all the carbon substrates disappeared.
Tabletop: Short-throw closed-boat geometry is how milligram quantities become usable targets (efficiency scales as 1/d^2); and every pump-down/vent of a chamber holding fragile foils needs a throttled soft-start path — the foils die from the pressure transient, not the vacuum.
-
Sputter-yield systematics (Scaife, Hanley & Purser): threshold 10-40 eV; yield rises exponentially from ~100 to ~1000 eV; nearly linear above 1 keV; maximum near 25 keV for conductors (50-60 keV dielectrics), plateau beyond. At the 20-keV working point, yields run 2-10 atoms/Ar ion (silver ~9.5, refractory metals ~2) — and yields rarely differ between materials by more than ~10x, unlike evaporation rates.
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 & tabletop applicability
At focused ion beam energies, sputter yields between 2 and 10 atoms per argon ion are typical.
Tabletop: The keV-yield plateau means any small ion gun in the 5-25 keV range is a usable deposition tool; choose Ar for economy, Kr/Xe when a 2-3x rate matters more than gas cost.
-
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 a factor of two — so refractory metals, and mixtures whose components would fractionate in a melt, deposit as readily as anything else, with no crucible contact and hence no crucible contamination.
Source, quote & tabletop applicability
the evaporation rates for these two metals differ by nine orders of magnitude, whereas their sputter yields differ by only a factor of two.
Tabletop: When the target material is refractory (B, C, W, Ta) or reacts with every crucible, sputtering is the escape hatch; a graphite source holder adds only carbon, the lowest-yield contaminant.
-
The 10-eV ejection energy is why sputtered films are tough (Scaife et al.): sputtered atoms arrive at ~10 eV versus ~0.1 eV thermal — far above the ~0.1 eV adhesion energy — producing chemisorption-grade adherence (500 A Ti on glass resisted a scissors point), in-flight substrate cleaning, localized annealing, and self-supporting films with bulk-like strength and ductility. Corollary: the cleaning defeats some release agents — Teepol is scrubbed off, NaCl and BaCl still work.
sputtered-atom energy ~10 eV (maintained above ~1 keV bombarding energy) vs ~0.1 eV thermal depositionSource, quote & tabletop applicability
Self-supported films usually display the same strength, toughness, and ductility as their bulk parent material.
Tabletop: For a target that must survive beam, handling, and mounting stress, sputter-deposited beats evaporated at equal thickness; and pick the release agent for the process — salt layers for sputtering, organics only where nothing scrubs them.
-
Sputter in high vacuum, not plasma pressure (Scaife et al.): focused-beam sputtering at 1e-6 torr keeps the sputtered atoms' mean free path at meters so they arrive with full energy; glow-discharge sputtering at 1e-3 torr (mean free path ~1 cm) thermalizes them in gas collisions, costing adhesion, strength and rate. Film purity follows too — ~100 ppm noble gas is the residue (Xe in Ta).
mean free path ~1 cm at 1e-3 torr vs ~meters at 1e-6 torrSource, quote & tabletop applicability
At 1e-3 torr, the mean free path in the vacuum chamber is about 1 cm
Tabletop: If building a small sputter rig, separate the ion source (differentially pumped duoplasmatron-class gun) from a high-vacuum deposition region rather than lighting a glow discharge in the whole chamber — the film quality difference is structural, not cosmetic.
-
Working numbers for a focused-ion-beam sputter rig (Scaife et al.): 2 mA of 20-25 keV Ar+ from a von Ardenne-type duoplasmatron through an einzel lens (beam kept under ~30% of lens diameter to dodge spherical aberration) erodes ~50 ug/sec total and deposits ~20 ug/cm2/min of Ti at 2.5 cm; usable targets from ~10 mg of source material; ~10% thickness uniformity over a 30-degree included angle statically, better with source/substrate rotation; deposition falls as 1/d^2 and the sputtered-atom lobe is slightly narrower than cosine, peaked near the source normal.
2 mA @ 20 keV Ar+ -> ~50 ug/s erosion, ~20 ug/cm2/min Ti at 2.5 cm; beam diameter <= 0.3 x einzel lens diameterSource, quote & tabletop applicability
A typical deposition rate for substrates located 2.5 cm from the sputtering source is 20 ug/cm2/min. of titanium.
Tabletop: Calibration point for sizing any home sputter-deposition scheme — mA and tens of keV, i.e. small-accelerator ion-source technology, not exotic hardware; a boron deposition run for a 100 ug/cm2 target is minutes, not days.
-
Contact evaporation for maximum recovery (Reynolds & Morgan, Liverpool/Manchester): place the substrate DIRECTLY on top of a resistance-heated tantalum tube source containing the charge, with stacked tantalum mesh discs inside acting as a multi-point source for uniformity — 200 ug of Cd isotope gave 200 ug/cm2 targets with >= 90% material recovery and ~10% uniformity over a cm2; heat to ~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 & tabletop applicability
a uniformity of 10% over an area of cm2 with a recovery of at least 90% of the material.
Tabletop: The zero-throw geometry turns the 1% efficiency of open evaporation into 90% — the method of choice when the feedstock (separated isotope, exotic compound) costs more than the labor of one-at-a-time targets.
-
Store reactive targets under inert gas cradle-to-grave (Bonetti et al., Bruyeres-le-Chatel): lithium, calcium and rare-earth foils live in dessicated-argon glove boxes from fabrication onward and SHIP in argon-filled containers; electrodeposited targets are nonuniform (thickness variations up to 100%, asymmetric) while electrosprayed ones hold ~7% — know the uniformity signature of the process before trusting a target from it.
Source, quote & tabletop applicability
The targets are sent to the users in containers filled also with dessicated argon.
Tabletop: An argon-purged jar (or wide-mouth desiccator backfilled from a weld-gas cylinder) preserves oxidizable targets for months; assume any electroplated deposit is factor-of-2 nonuniform unless mapped.
-
Vacuum storage beats atmosphere for degradable targets (Worthington, Jedlowski & Thomas, ANL): a 90-position storage wheel at < 5e-7 torr (diff-pumped, -35 to -40 C optically dense baffle against oil) with a screw-tip transfer rod and a double-valved transfer chamber moves hygroscopic or oxidizing targets evaporator-to-storage-to-beamline without ever seeing air; the transfer interlock is pumped below 0.05 torr before either valve opens, and an electronic interlock system guards against the system's one chronic accident — vacuum loss.
storage < 5e-7 torr; interlock volume < 0.05 torr before valve openingSource, quote & tabletop applicability
Some targets may be hydroscopic, while others may oxidize rapidly.
Tabletop: A miniature version — one valved transfer pot pumped by the machine's own roughing line — lets an air-sensitive target (Li, Ca, some borides) move between evaporator and chamber intact; the load-lock principle scales down to one target.
-
The parting agent, not the evaporation, can set target nonuniformity (Abele et al., TU Muenchen): parting-agent crystallites run 100-2000 A with 50-1000 A surface roughness — the same order as a 10 ug/cm2 carbon or 100 ug/cm2 gold film (~500 A) — so the film is a replica of the crystallite field "however uniform an evaporation may be". A 1-mm-aperture alpha thickness scan averages right over it; the damage appears as excess energy straggling, growing sharply with target tilt angle.
crystallite size 100-2000 A ~ film thickness; effective-thickness spread grows with 1/cos(tilt) plus crystallite-plane geometrySource, quote & tabletop applicability
however uniform an evaporation may be, the parting agent produces an inhomogeneous target.
Tabletop: If a target will sit tilted to the beam or feed a spectrometer, the release-agent choice is a resolution decision, not a convenience; standard single-point thickness QA cannot see this defect — only straggling-width measurement can.
-
Choose low-crystallite organic parting agents for resolution work (Abele et al.): among NaCl, betaine/sucrose, CsI, alanine and Teepol (= Lensodel), only Teepol — and nearly, alanine — kept measured straggling near the Vavilov (ideal-target) prediction at 30-50 degree tilt; NaCl and betaine replicas broadened it severely. Their QA method transfers whole: pass monoenergetic alphas through the finished target and compare the straggling width to Vavilov — "check the resolution of the target without using expensive beam time".
FWHM_thickness = sqrt(FWHM_exp^2 - FWHM_Vavilov^2) / stopping power (Gaussian-folding deconvolution)Source, quote & tabletop applicability
all targets should be produced with the use of Teepol as parting agent, or ... an organic parting agent with very little crystallite structure
Tabletop: Detergent-film release (Teepol-class) over salt release wherever the condensing metal tolerates it; and the alpha-straggling comparison is a complete bench-top target-quality metric using the same rig as the thickness measurement.
-
Proton targetry is forgiving; energy loss scales as the square of projectile charge (Erskine, ANL): with a proton beam even a leftover gold target gave 5.1 keV FWHM at 16 MeV (1 part in 3100) — "with a proton beam, targetry is just no problem" — because mean energy loss carries a Z_proj^2 factor (oxygen loses ~64x more than protons at equal energy) while straggling grows ~Z_proj; a 10% target nonuniformity that costs protons 1.9% in energy width costs a calcium beam 22%.
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 & tabletop applicability
With a proton beam, targetry is just no problem. One can obtain very nice high-resolution results.
Tabletop: 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; budget with the Z^2 scaling when tempted by heavier beams.
-
Backings are not free (Erskine): a carbon substrate "produces a lot of difficulty because of the contaminant reactions observed from carbon", carbon has ~2.5x gold's energy loss per ug/cm2, and reaction-site path-length compensation by tilting the target only works if the target is flat — bowing, wedge or microscopic roughness defeats it. His 48Ca best case stuck at 110 keV resolution from suspected calcium-layer nonuniformity no target change could beat.
Source, quote & tabletop applicability
using a carbon substrate produces a lot of difficulty because of the contaminant reactions observed from carbon
Tabletop: For reaction-yield measurements, run the blank-backing background and prefer a backing whose own reactions with the beam are energetically closed or distinguishable; flatness of the mounted foil matters as much as its thickness distribution.
-
Foil lifetime scales inversely with beam current DENSITY, not current (Yntema, ANL): he plots carbon stripper lifetimes as particle-uA-min per mm2 of actual beam spot (for an oscillated target, the spot size, not the swept area), against ion velocity (MeV/A); stationary unheated foils fall on a straight line in these variables. Minimum practical stripper foil ~3 ug/cm2.
lifetime metric = particle uA min / mm2 (beam-spot area); velocity variable MeV/ASource, quote & tabletop applicability
we have assumed that the foil lifetime is inversely proportional to the particle density incident on the target.
Tabletop: Current density is the damage variable — halving the spot diameter quarters foil life at fixed current; any foil-life data from the literature transfers only through uA/mm2, so measure the actual beam-spot size before predicting.
-
Heat carbon foils to ~500 C under beam (Yntema): radiative heating of a carbon foil to ~500 C under a 4 MeV Ni+ beam extended life ~40x; adding slow motion (6x effective area) made it >200x an unheated stationary foil. Pre-annealing at 1000 C before use gave NO benefit — the heat must be present during bombardment. Foils also thicken under beam from hydrocarbon cracking (suppressed in 1e-9 torr vacuum at Harwell) plus beam-induced effects; oscillation moderates the thickening.
~500 C in-beam -> ~40x life; + slow motion (6x area) -> >200x; pre-annealing at 1000 C -> no effectSource, quote & tabletop applicability
The increase in observed lifetime was about a factor of 40.
Tabletop: Radiation-damage annealing is concurrent, not a pre-treatment — a small radiant heater keeping a carbon foil dull-red-adjacent (~500 C) during operation is the cheapest 40x in stripper/target life on record; keep hydrocarbons out of the vacuum or the beam writes a thickening carbon spot on every foil.
-
Electrostatics can kill a foil instantly (Yntema): beam current flowing through a thin foil concentrates near the frame edge, and current + temperature gradients rupture foils at the holder; a charged insulator near the foil "can be blown off the frame almost instantaneously". A thin evaporated Au layer raised carbon foil life ~50% (ANL), while a thin Al layer DECREASED it substantially (Chalk River).
Source, quote & tabletop applicability
the foil can be blown off the frame almost instantaneously.
Tabletop: Ground the target frame conductively, keep charged insulators (charged windows, PTFE hardware) away from foil positions, and make the foil-to-frame electrical contact generous — the mounting, not the film, is often what fails first under beam.
-
Defocus and raster whenever the physics allows (Berry, ANL/Chicago): sweeping the beam at 1 kHz in x and y across a 25 mm2 aperture-defined area cut 5 ug/cm2 carbon foil breakage by 5-10x by making the current density uniform; a defining pre-aperture keeps beam off the foil holder ("better lifetime characteristics"); and a rotatable 23-foil carousel makes replacement cheaper than heroics — "defocus whenever possible is the moral".
1 kHz x-y electrostatic raster over 25 mm2 -> breakage / 5-10; life ~ proportional to uniformly-illuminated areaSource, quote & tabletop applicability
Defocus whenever possible is the moral to this result.
Tabletop: An internal target wants the widest beam spot the measurement tolerates, an aperture that shadows the frame, and a multi-position holder; electrostatic wobble plates at kHz are trivial hardware on a small machine and equivalent to Corwin's mechanical rotation.
-
Match the e-beam spot to the evaporant droplet (Maier-Komor, TU Muenchen): for small isotope charges (100 mg Mo = 3.5 mm droplet) the most efficient energy transfer is beam diameter = droplet diameter; a larger spot wastes power on the cooled crucible, a smaller one saturates (dense vapor above the impact point scatters the beam and burns power making secondary electrons and ions). ~2 kW reaches evaporation for such charges despite ~50% backscatter loss — Kanter/Sommerkamp data give total power absorption ~49% on a Ta sphere (PAC ~ 0.61 cos^1/2), worse for high Z.
beam spot ~ droplet diameter; power absorption ~49% (Ta sphere); backscatter loss rises with Z and with incidence angleSource, quote & tabletop applicability
the most efficient energy transfer is achieved, when the electron beam and the molten droplet have the same diameter.
Tabletop: Small-charge e-gun work is a spot-placement problem — half the beam power never enters a high-Z melt, so rated gun power overstates melt power by ~2x; don't size a gun (or a power budget) from evaporation enthalpy alone.
-
Regulate the e-gun supply or re-aim at every power change (Maier-Komor): drooping (resistance/inductance-limited) supplies sag up to 25% at full load; with magnetic deflection the spot radius goes as sqrt(voltage), so a 25-mm-radius gun's spot walks ~7 mm at full load — clean off the evaporant. Find the true spot by melting a hole in a copper foil laid in the crucible (electrostatic/permanent-magnet guns) or by maximizing crystal-monitor rate versus deflection (electromagnetic guns). Use water-cooled COPPER crucibles (W cracks, Mo gains little), cleaned of oxide, one dedicated crucible per isotope.
magnetic deflection radius ~ sqrt(V); 25% V droop -> ~7 mm spot walk at r = 25 mmSource, quote & tabletop applicability
the beam spot will shift nearly 7 mm when the power supply is fully loaded and the beam will no longer hit the evaporant.
Tabletop: 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): a parting-agent-coated substrate is an insulator — start at a very low evaporation rate so the growing layer can discharge, or sparks crack the parting film and the young target layer; ground the substrate mount so the film edge makes contact. An INSULATED mount charges toward the gun's acceleration voltage and pulls plasma ions into the film, growing hillocks and craters; coat a glass bell jar's inside with metal or it charges to the acceleration voltage too.
Source, quote & tabletop applicability
sparks will occur, destroying the parting film and the thin isotope layer by hairline cracks.
Tabletop: Grounding topology inside the evaporator is part of the recipe — the same charging physics that pits e-gun films will bite any deposition or beam system with floating fixtures near keV electrons.
-
Budget substrate heating from condensation and source radiation (Maier-Komor): condensation releases ~6e5 J/g-atom for low-vapor-pressure metals; at 10 cm throw a condensation rate of 5e-8 g/cm2 s (= 1e-2 torr source vapor pressure for a 3.5 mm droplet) keeps a 50 ug/cm2 NaCl parting layer under ~10 C/sec of heating. Radiant load depends on source temperature at equal vapor pressure — Mo radiates ~10x what Au does at 1e-2 torr — so cool the substrate or pulse the evaporation; and hold source vapor pressure below ~1e-6 torr-equivalent rates if contamination ratio matters.
condensation energy ~6e5 J/g-atom; 5e-8 g/cm2 s at 10 cm -> < ~10 C/s in 50 ug/cm2 NaCl; radiant load at fixed vapor pressure ~10x higher for Mo than AuSource, quote & tabletop applicability
the only way to avoid destruction of the targets is to cool the substrate or to periodically interupt the evaporation process
Tabletop: 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, 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 Mo boat, substrate 6 cm above, charge pressed to a tablet to stop splashing; cold-trapped system at 5e-6 torr; hold the boat at cherry red (~600-900 C) one minute to pre-heat the substrate receptive, then bright red (~1100-1450 C) to deposit; close the high-vacuum valve during the evaporation and mind sulphide toxicity on venting.
Source, quote & tabletop applicability
The cleaning process is of utmost importance and each of the following steps contributes significantly to good results.
Tabletop: Template for any compound that dissociates or splashes — pelletize the charge, chimney the boat, pre-warm the substrate with the source itself, and treat the color-temperature chart as the process instrument; valve off the diffusion pump so the compound vapor doesn't load the pump oil.
-
Expect beam-induced foil failure to be MECHANICAL, not thermal: the beam spot thickens (carbon buildup and/or mass transport toward the spot), the film tightens, radial stress lines develop, and the foil tears across the thickened spot — so a foil breaks at its thickest part, at the bombarded/unbombarded transition.
Source, quote & tabletop applicability
It has always bothered me that a film should ever break at its thickest port [sic]; (Ramsay, "Alternatives to Thin Film Carbon Foils")
Tabletop: Any thin internal target or probe foil in a proton beam fails by this stress mechanism long before bulk melting; inspect failed foils for the radial-crease signature before blaming heat.
-
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 & tabletop applicability
start with as large a beam spot as possible and slowly focus it smaller (Ramsay, "Alternatives to Thin Film Carbon Foils")
Tabletop: 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: a 2 ug/cm2 carbon film backed with 10 ug/cm2 of gold survived beam exposure that tore an identical unbacked carbon foil at the beam spot.
2 ug/cm2 C + 10 ug/cm2 Au backing survived; bare 2 ug/cm2 C toreSource, quote & tabletop applicability
two of the targets did not break (Ramsay, "Alternatives to Thin Film Carbon Foils")
Tabletop: When a self-supporting film keeps failing, evaporating a few ug/cm2 of a conductive metal onto it is a cheap fix — it adds conduction paths and mechanical tempering for negligible energy loss.
-
When forming a target compound by heating a deposit on a substrate (e.g. nitriding Ti on Ta), the reaction temperature has a two-sided window: too low leaves the reaction incomplete, too high diffuses the reactant into the substrate and smears the target thickness. For TiN on Ta the window is 750-800 C.
TiN nitriding window 750-800 C (optical pyrometer, uncorrected for emissivity)Source, quote & tabletop applicability
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")
Tabletop: Any reacted-layer target (nitride, oxide, deuteride) on a metal backing has such a window; a smeared depth profile shows up as degraded resonance width or energy resolution.
-
Hydrogen tube-furnace reduction converts most common target oxides (CuO, Fe2O3, WO3, GeO2, PbO...) to metal with modest equipment, but the combustion boat must be chemically compatible (iron in a graphite boat forms carbide), the H2 must be deoxygenated and dried, and an oil trap should guard against flashback if the vent gas is burned.
per-element reduction table (temp, reductant, boat) at PDF pp.102-103; Vycor tube to 1000 C, quartz to 1300 CSource, quote & tabletop applicability
Iron forms a carbide if a graphite boat is used (Heagney & Heagney, "Reduction Techniques for Isotopic Materials")
Tabletop: The route from purchased oxide powder to rollable or evaporable target metal; the two-page table is the reference to consult before buying any element as oxide.
-
Electrolytic reduction is the most material-conserving oxide-to-metal route for zinc and cadmium: better than 90% of the metal deposits on the cathode at 5-10 mA/cm2 from cyanide/hydroxide baths of a few ml, and the remainder is chemically recoverable.
Zn, Cd plating at 5-10 mA/cm2; bath volume 1-5 ml scaled to isotope quantitySource, quote & tabletop applicability
Usually better than 90% of the metal can be deposited on the cathode (Heagney & Heagney, "Reduction Techniques for Isotopic Materials")
Tabletop: For milligram-scale enriched material the deciding metric is recovery fraction, not speed — electrolysis beats furnace reduction whenever the metal plates well.
-
For a beam-durable deuterium target, evaporate titanium in a low-pressure D2 atmosphere (5e-3 torr, 2-3 h slow evaporation, backings at 200 C) rather than using deuterated polyethylene, which dies quickly in beam; assay the occluded deuterium by nuclear scattering, not by weight.
Ti evaporated in 5e-3 torr D2 over 2-3 h; ~2 ug/cm2 D occluded in 250-300 ug/cm2 TiSource, quote & tabletop applicability
Deuterated polyethylene could not be used because of its rapid deterioration under bombardment (Meens, "Deuterated Titanium Targets on Thin Backings")
Tabletop: The standard durable D-target chemistry for a d-beam or D(p,..) work at any current; plastic CD2 targets are for lowest-current work only.
-
When the target element is volatile or liquid, build the target from its most thermally stable compound rather than the metal or an amalgam — a sublimed HgS film tolerated ~20 particle-nA of heavy-ion beam where the amalgam target allowed ~1 particle-nA, and inhomogeneity shows 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 & tabletop applicability
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")
Tabletop: Compound-vs-element is a factor-of-20 beam-current decision, not a chemistry nicety; and the elastic-peak tail is the free in-beam diagnostic of target quality.
-
Cool a fragile target in use by conduction through its edges: connect the target edge to a chilled copper block with silver paint. A block at -80 C held a mercury-sulfide target near -50 C during bombardment.
edge conduction via silver paint; block -80 C -> target ~-50 C (~30 K rise through the joint and film)Source, quote & tabletop applicability
They are cooled from the edges by connecting to a copper block with silver paint (Maier, discussion of "Preparation of Isotopically Enriched Mercury Targets")
Tabletop: The simplest conductive-cooling geometry for a target that cannot be water-backed — a cold finger to the frame plus a conductive-paint joint; budget tens of kelvin of drop across the joint.
-
In reduction-distillation, pick a reductant of MODERATE oxygen affinity so the reaction speed is controllable by furnace temperature: tungsten powder reduces HgO smoothly at 500 C in ~10 min, while thermodynamically stronger reductants (Zr, Th) react explosively and scatter the charge.
choose reductant by oxide dissociation-pressure diagram; W + HgO controllable at 500 C, Zr/Th explosiveSource, quote & tabletop applicability
the reaction with mercury oxide runs into an explosion (Friebel et al., "Preparation of Isotopically Enriched Mercury Targets")
Tabletop: Strongest is not best in metallothermic reduction; a controllable reaction that completes in minutes beats a violent one that contaminates the product.
-
Thick (beam-stopping) targets from powder: press 300-400 mg between two polished stainless ferrotype plates at ~3 tons/in2 into a ~2-cm disc of 100-150 mg/cm2; strengthen fragile pressed discs with a few drops of dilute polyethylene-in-xylene, and glove-box the pressing for air/water-sensitive compounds.
~3 ton/in2 between polished plates -> 100-150 mg/cm2 discs; 1 mg/ml polyethylene-xylene binder wash for fragile discsSource, quote & tabletop applicability
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")
Tabletop: The thick-target recipe for activation and yield measurements where the beam must stop in the target — no evaporator needed, just a hydraulic press and polished plates.
-
Split any conductive target-holder ring when the target sits in an RF field, so the ring cannot carry induced eddy currents.
Source, quote & tabletop applicability
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")
Tabletop: 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 fixes it.
-
Weighing is a poor thickness gauge below ~10 ug/cm2 — adsorption/desorption alone contributes ~0.5 ug/cm2 of error — so use optical transmittance with a double-reflectance correction (ln(I_T/I_0) = -mu*x + ln(1-R_R)); measure thin foils at short wavelengths and thick foils at long wavelengths where they still transmit.
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 & tabletop applicability
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")
Tabletop: A bench spectrophotometer (or a single calibrated LED/photodiode pair) measures foil thickness in seconds without an accelerator; cross-cite ornl-3021 for the films this gets applied to.
-
Prevent stress failure of evaporated films by heating the substrate during deposition: film tension falls with substrate temperature, passes through zero, and can go compressive; the crossover scales with melting point (~210 C for Ni, ~100 C for Cu, ~300 C for Fe). Annealing AFTERWARD (<=400 C) does not remove the frozen-in stress.
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 & tabletop applicability
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")
Tabletop: The missing variable when evaporated foils curl, buckle or shatter on float-off; set substrate temperature at deposition time — post-baking will not save a stressed film. Complements the ORNL-3021 evaporation recipes.
-
A small bench-type hand-cranked rolling mill is sufficient for foils down to 1-5 mg/cm2 — large mills are not required; and when a small isotope quantity rolls non-uniform (thick center, thin edges, too few passes), press it between two polished cobalt-tungsten-carbide flats instead.
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 & tabletop applicability
One can roll many useful foils down to the 1 to 5 mg/cm2 region with a small bench-type manually operated mill (Perry, discussion "Rolling of Metal Targets")
Tabletop: A jeweler's mill covers the whole thick-target range a small machine needs; the carbide-flat press is the fallback when rolling wastes scarce material on edge taper.
-
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 & tabletop applicability
This can be avoided by making three to five passes at the same setting before going thinner (Perry, discussion "Rolling of Metal Targets")
Tabletop: The same-setting-passes trick (work-harden the surface before the next bite) and the electropolish-between-stages trick for oxidizing metals are the two non-obvious moves in amateur pack rolling.
-
Heating and moving a stripper/target foil multiply its life under intense beams: holding foil and frame at 450+-150 C gave ~4x lifetime, orbiting the foil at 1 rpm (beam walking around the foil) ~3x, and both together ~6x. Failure signature changes too — cold foils break suddenly and completely, heated foils tear 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 & tabletop applicability
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")
Tabletop: A small heater ring or a slow rotation stage on a target/foil holder is a cheap 3-6x life multiplier; the gradual-tear failure mode of a heated foil also gives warning instead of sudden loss.
-
Beam duty-cycling extends foil life only if the off-periods are long enough for stress relaxation: equal on/off periods of 60 s helped noticeably, 6-s periods did almost nothing.
60 s on / 60 s off effective; 6 s / 6 s ineffective (3-MeV Kr+ on 5 mg/cm2 C)Source, quote & tabletop applicability
Periods of sixty seconds have produced encouraging results while six second periods showed very little improvement in foil lifetimes (Thomas et al., "Lifetimes of Carbon Stripping Foils")
Tabletop: Relevant to any interlock or chopping scheme meant to spare a target — the relaxation time constant is tens of seconds, so second-scale chopping buys nothing.
-
Rolled foils outlast evaporated foils under intense beams because their structure is crystalline: evaporated films (substrate <700 K) are partly amorphous with many Frenkel defects, and beam-driven phonon excitation reorders those regions, wrinkling and destroying the film; in a rolled foil displacing an atom costs the full Wigner energy (10-40 eV in metals).
Source, quote & tabletop applicability
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")
Tabletop: When a target must survive sustained current, prefer rolled (or electrodeposited/annealed) material over as-evaporated film — durability is set by crystalline order, not thickness.
-
Rolling feedstock must be a clean solid bead: e-beam melt 50-500 mg portions in a water-cooled copper crucible, let the drop solidify slowly from the cooled side so impurities concentrate in a last-frozen "stalagmite", cut it off, and repeat (~10x for uranium). Avoid pressed-and-sintered powder (grain-boundary defects end rolling early) and arc melting (gas impurities: 1 ppm impurity in the arc gas is like working at 1e-3 torr).
e-beam zone refining by slow solidification + stalagmite cutting, ~10 cyclesSource, quote & tabletop applicability
The defects at the grain bounderies [sic] set an early limit during the rolling process (Kellner & Maier-Komor, "Rolling Thin Uranium Foils")
Tabletop: Explains why bought powder pressed into a pellet will not roll thin; the melt-and-decant-impurities step is what makes sub-mg/cm2 foils possible.
-
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 & tabletop applicability
We noticed that material with a thickness of 0.5 mm or below gave the best results (Kellner & Maier-Komor, "Rolling Thin Uranium Foils")
Tabletop: The foil replicates every flaw of the jacket, not the rolls — jacket steel selection is the dominant quality variable in pack rolling.
-
Pack-rolling schedule: reduce ~3-10% per pass; when the jacket has grown to about twice its size, transfer the foil to a fresh jacket; below 5-10 mg/cm2 switch to a double sandwich — a 0.1-0.2 mm vacuum-melted inner jacket inside the 0.5 mm outer — and keep the same 2x-growth rule.
3-10% reduction/pass; re-jacket at 2x elongation; double sandwich (0.1-0.2 mm inner) below 5-10 mg/cm2Source, quote & tabletop applicability
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")
Tabletop: The complete quantitative schedule for rolling any metal to sub-mg/cm2; with it they reached 800 ug/cm2 uranium and 130 ug/cm2 molybdenum with no hot rolling.
-
Anneal rolled foils between resistively-heated tantalum sheets in good vacuum for ~30 min at a temperature chosen BELOW any phase transition of the metal (uranium: below 930 K at 1e-7 torr); etch oxide first with highest-purity dilute nitric acid — an electronegative foil getters every metal impurity out of a dirty acid.
anneal ~30 min, 1e-7 torr, T below phase transition (U < 930 K)Source, quote & tabletop applicability
at a temperature below 930 K, which was chosen to prevent phase transitions (Kellner & Maier-Komor, "Rolling Thin Uranium Foils")
Tabletop: Interpass and final annealing is what keeps a work-hardened foil rollable and flat; the phase-transition ceiling matters for any allotropic metal (Ti, Fe, U), not just uranium.
-
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 & tabletop applicability
The problem was a poor vacuum of 10-5 Torr in the scattering chamber which allowed oxidation (Kellner & Maier-Komor, "Rolling Thin Uranium Foils")
Tabletop: A 1e-5-torr-class chamber actively burns reactive targets under beam — the beam spot acts like a getter pump. Budget target life against chamber pressure, and expect oxide growth in the spectrum before mechanical failure.
-
Reactive sputtering produces target films that evaporation cannot match for durability: adherent, "even, tough" nitride films with free choice of backing material, good thickness control, and purity limited only by system cleanliness — suitable for water-cooled targets under 10 uA alpha beams at 2-5 MeV.
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 & tabletop applicability
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")
Tabletop: Sputter deposition is the durable-target counterpart to the ORNL-3021 evaporation recipes — slower, but the film adheres and survives beam heating on whatever backing the cooling design wants.
-
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 & tabletop applicability
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")
Tabletop: The same cracking chemistry that contaminates sputtered films coats everything in any glow discharge backed by an untrapped oil diffusion pump — condition the discharge on a shutter before exposing the workpiece.
-
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 & tabletop applicability
the longer sputtering times required for thick targets produce higher temperatures, and higher rates (Stinson, "Nitrogen Targets Produced by Reactive Sputtering")
Tabletop: 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).
-
Protect oxidation-prone target layers as a sandwich: evaporate 0.01-0.2 mg/cm2 of carbon, titanium, nickel or gold over (and under) the active layer; layers thick enough to be their own heat sink (20-100 mg/cm2) can instead go bare onto ~2-mm copper chips.
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 & tabletop applicability
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")
Tabletop: Two transferable patterns — a tens-of-ug/cm2 cover layer buys shelf life and in-beam oxidation resistance for negligible energy loss, and a thick copper backing chip is the simplest conductive heat sink for a high-power target.
-
Refractory-metal (W) evaporation practice: spot-weld the outgassed isotope ball to a ground-flat tungsten rod pedestal in the water-cooled crucible and heat by electron bombardment from a loop filament (6 kV, 130 mA); higher evaporation rates give LESS stressed targets; and tank pressure above 4e-6 torr makes the films brittle with short shelf life. Best substrate: NaCl-coated 10-mil stainless at 400-600 F.
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 & tabletop applicability
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")
Tabletop: A cyclotron-target paper end to end; the quantified links rate-to-stress and pressure-to-brittleness carry to every evaporated self-supporting film, not just tungsten.
-
Inventory of solid-target failure modes under intense beams — and the escape hatch: beam-spot temperatures reach ~3000 C where heat conduction is poor (past most melting points), charge buildup breaks nonconductive targets electrostatically, and structural rearrangement causes strain, peeling, blistering and voids. A windowless supersonic gas jet (density knot of an underexpanded Laval nozzle) is the unbreakable alternative, tunable ~1-100 ug/cm2 by inlet pressure.
Laval-jet density knot ~5 mm long x 3 mm dia; thickness linear in inlet pressureSource, quote & tabletop applicability
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")
Tabletop: The checklist of what actually kills targets as current rises — conduction, charge relief, and structure all have to be engineered, and a gas target is the limit case when none of them suffice.
-
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 & tabletop applicability
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")
Tabletop: A vacuum-compatible tacky mounting adhesive solves the foil-jumps-off-the-frame failure of float-mounting; pairs with the ORNL-3021 float-off recipes.
-
Rollability of a brittle metal is set by parts-per-hundred-thousand purity: a few hundred ppm of almost any metal (or O, N, H) embrittles chromium; only the highest-purity reduction route (hydrogen) gives rollable material, and heat treatments at intermediate thicknesses prevent pinholes when rolling on below ~1 mg/cm2.
few-hundred-ppm impurities embrittle Cr; ductile fragments 10-15 mg; interpass anneals above 1 mg/cm2; minimum reached 700 ug/cm2Source, quote & tabletop applicability
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")
Tabletop: When a foil cracks in the mill, suspect chemistry before technique — the reduction route chosen upstream fixes the ductility available downstream.
-
Derive the gas-purity spec for hydrogen reduction from equilibrium thermodynamics, not habit: for Cr2O3 + H2 at 1400 K the equilibrium water ceiling is 540 ppm, and completing the reaction in reasonable time wants <=10 ppm — hence a palladium-diffusion purifier (<1 ppm H2O/O2) and 6 h at 1400 K.
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 & tabletop applicability
in equilibrium the maximum tolerable water content of the hydrogen atmosphere is 540 ppm (Friebel et al., "Preparation of Isotopically Enriched Chromium Targets")
Tabletop: The template calculation for judging whether tank-grade gas is good enough for any reduction or annealing atmosphere — compute the equilibrium ratio at your furnace temperature before blaming the furnace.
-
Thick carbon foils (1-8 mg/cm2) need no evaporator: settle 325-mesh GRAPHITE powder from an air suspension onto carbon-coated glass, then press at ~14 tons/in2 into a lustrous flexible film (uniformity <10%). Amorphous carbon is rejected on physics grounds — it will not bind, and its low thermal conductivity and high resistivity make it a poor accelerator target anyway.
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 & tabletop applicability
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")
Tabletop: Beam-stopping carbon (and the thermal/electrical selection argument — a target material must conduct heat and charge away) from a drugstore powder blower and a hydraulic press; developed at a cyclotron facility for cyclotron targets.
-
Ion-beam power density on a sputter target (or any small-spot bombarded surface) forces cooling: at ~10 kV and 2-4 mm focus the loading exceeds 100 W/cm2 and a low-conductivity material surface runs several hundred C — hot enough to oxidize reactive materials mid-deposition and spoil thickness reproducibility — so the material post must be cooled.
>100 W/cm2 at 10 kV, 2-4 mm spot -> surface several 100 C for low-conductivity materialSource, quote & tabletop applicability
a cooling system for the target material post is required (Baumann & Wirth, "A Heavy Ion Sputtering System with a Penning-Ion-Source")
Tabletop: 100 W/cm2 is the order of loading a mm-scale beam spot delivers at tens of uA and tens of kV — the same arithmetic that sizes cooling for beam stops, probes, and targets on a small machine.
-
For long uninterrupted deposition runs and reactive process gases, a cold-cathode Penning source beats a duoplasmatron: no filament to burn out, 165 h of stable output (0.2% stability at 0.58 mA) demonstrated, chemically resistant to O2/N2 operation, and total source power under 30 W — no cooling circuit needed.
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 & tabletop applicability
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")
Tabletop: A documented small PIG design point (geometry, discharge mode, gas flow, stability) from outside the cyclotron literature — the filament-free argument is the same one that favors PIG sources inside a cyclotron.
-
Electrodeposited metal targets are mechanically tougher in beam than evaporated ones of the same material; for platinum the workable compromise is ~250 mA/cm2 (higher current densities give spongy deposits) from a hexahydroxoplatinate bath, ~3.6 ug/cm2-min.
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 & tabletop applicability
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")
Tabletop: 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.
-
Carbon foil breakage under ion beams depends only on TOTAL integrated fluence — it is independent of foil thickness (2-22 ug/cm2) and of beam current — following tau(p-uA-min/mm2) ~ A*E^1.15 (MeV/amu) with A ~20 for Ar (larger for lighter ions, ~60 for N; smaller for heavier, ~5 for Ni/Br). Therefore make stripper/window foils as thin as mechanics allow: thinner costs nothing in life and minimizes dispersion.
tau(p-uA-min/mm2) = A * E^1.15 (MeV/amu); A ~ 20 (Ar), ~60 (N), ~5 (Ni, Br); thickness-independent over 2-22 ug/cm2Source, quote & tabletop applicability
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)
Tabletop: A fluence budget, not a current limit — halving the current doubles the time to the same death; plan foil replacement by integrated charge, and never buy life by thickening a foil.
-
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 & tabletop applicability
it was not possible to carry out accurate measurements with slides that had been coated with a soap-like parting agent (Rhoads, Stoner & Bashkin, "Calibration of Surface Densities of Metal Films by Optical Transmittance")
Tabletop: 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.
-
Kill pinholes by fixing the SUBSTRATE, and map your evaporation boat before spending isotope: an hour of argon glow discharge "levels" a commercial copper foil enough to give pinhole-free 1.8 mg/cm2 films over 100 cm2, and weighed-square thickness maps show the yield/uniformity trade — a chimney boat close-in gives maximum thickness over one small spot, a central-hole boat at 15 cm gives ~80% edge uniformity.
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 & tabletop applicability
The sputtering "leveled" the copper surface (Meens, "Vacuum Tight 208Pb Foils")
Tabletop: Pinholes replicate substrate defects, not evaporation errors; and one sacrificial natural-material run with a grid of weighed squares characterizes a boat geometry forever.
-
Load titanium with hydrogen (or deuterium/tritium) by heating to ~650 C in sub-atmospheric purified gas: outgas at 800 C in vacuum first, pass the gas through a deoxygenating cartridge AND a liquid-nitrogen trap (without the trap absorption simply fails), and meter the uptake as a pressure drop in a known volume; ~2 h absorb-and-cool per batch, 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 & tabletop applicability
The trap is essential; the gas is not absorbed otherwise (Gursky & Sherwood, "Hydriding of Titanium Cones for a Sputter-Ion Source")
Tabletop: The bench recipe for making Ti-H/Ti-D loaded pieces — hydride targets or gas reservoirs — with nothing but an RF or furnace heater, a differential gauge, and scrupulous gas drying.
-
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 & tabletop applicability
If the beam is focused to an area of about 0.2 cm2, the resulting specific energy depositions amounts to 1 kW/cm2.
Tabletop: The reference machine at -3 nA / ~150 keV deposits ~0.5 mW — any target survives. The same two-line arithmetic must be rerun at every upgrade; a 10 uA / 1 MeV machine puts 10 W into a mm-scale spot, and that is rotating-target or water-cooled-backing territory.
-
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 & tabletop applicability
The wheel thus had to be rotated at a velocity of 666 rpm (equal to 20 deg in 5 ms or during one macropulse).
Tabletop: The design move — spread the duty cycle over many target areas, and if the beam is pulsed, lock the rotation phase so no single spot sees consecutive pulses — scales to a bench wheel behind any external beamline; the 1e17-particle survival figure sets the achievable scale.
-
Interlock target rotation with the beam: a GSI rotating disc of 1.8 mg/cm^2 Au targets survived up to 1 uA of 15 MeV/u Au ions at 1333 rpm, but an identical target exposed to full beam with the drive motor switched off was destroyed — SEM showed zones of molten gold from thermal deposition. Damage manifests first as wrinkling from beam heating, then melting.
Source, quote & tabletop applicability
exposed to the full beam intensity while the disc-driving motor was already switched off
Tabletop: 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.
-
Sandwich low-melting-point target metals (Pb, Bi) between carbon layers: GSI standard practice for high-current wheel targets, e.g. C/Bi/C at 0.03/0.5/0.03 mg/cm^2, extending stability and lifetime under bombardment.
C/metal/C sandwich, typ. 0.03 / 0.5 / 0.03 mg/cm^2Source, quote & tabletop applicability
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
Tabletop: Direct recipe for any soft-metal target a small machine bombards; the carbon skins add mechanical strength, radiation cooling, and conduction paths for a few ug/cm^2 of added material.
-
Multi-layer overcoats buy target lifetime through conduction, not just chemistry: the 1983 heavy-ion discussion (led by Kobisk) recorded that metal/carbon overcoat layers enhance thermal and electrical conductivity, shunting both heat and accumulated charge to the heavy frame around the target, significantly increasing lifetime; energy accumulation showed up as local melting, detected as broadening of scattering peaks.
Source, quote & tabletop applicability
This improved energy transfer tended to significantly increase target lifetime under bombardment.
Tabletop: 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 melt detector rather than waiting for visible failure.
-
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 & tabletop applicability
it was observed to take five minutes before any significant amounts of oxygen or moisture were detected
Tabletop: Sets the realistic scale for handling windows on Li/Ca/lanthanide targets moved from evaporator to chamber in air — minutes, not hours — and shows overcoat choice is coupled to the experiment (overcoat nuclei scatter too).
-
Monitor target thickness and damage in-beam rather than trusting pre-weighing: GSI watched the elastic-scattering peak at 30 deg forward with a surface-barrier detector — FWHM measures target homogeneity, broadening flags damage — and calibrated the detectors against weighed standard targets. Per-target histories on a rotating wheel came from tagging each count with wheel position.
Source, quote & tabletop applicability
broadening of the peak indicates target changes or damages
Tabletop: A silicon detector at a fixed forward angle is cheap on any small machine; the scattering-peak-width-as-damage-gauge is the lightest possible target diagnostic and doubles as a luminosity monitor for excitation measurements.
-
When resolution does not matter, defocus: Ford (ORNL/HHIRF) class-1 experiments ran rolled 0.5-5 mg/cm^2 targets at 0.5-5 electrical uA — all the beam the target withstands — and deliberately diffused the beam spot on the target to manage heating.
Source, quote & tabletop applicability
target heating can be a problem and efforts are made to diffuse the beam on the target.
Tabletop: The zero-cost cooling knob — spot size enters the W/cm^2 arithmetic squared. For activation or yield runs on a small machine, defocus or wobble the beam before engineering any water cooling.
-
For small-quantity evaporations the failure mode is a molten ball overheating the substrate: the 1983 general-targets discussion (led by Gursky) prescribes cooling the substrate or backing it with a heat sink, and notes ~25 mg of isotope suffices if the e-beam focus is very small. Guard against evaporating the water-cooled copper hearth itself when e-beam heating tiny charges.
Source, quote & tabletop applicability
An important problem is overheating of the substrate by a large, molten ball of material.
Tabletop: Applies verbatim to boron and enriched-isotope work in a bench evaporator; the water-cooled pedestal trick (molten zone confined to the pellet top, pedestal only 3-5 cm across) is stated for induction-heated boron specifically.
-
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 & tabletop applicability
If pitting or burn-up of the copper foil substrate occurs increase cooling. if curling occurs as the deposit thickens, increase heating
Tabletop: The pitting-vs-curling pair is a complete closed-loop tuning rule for any hot deposition onto a cooled backing — stress control by temperature, readable by eye. Also note the loose clamp so the foil can contract.
-
Make thick elemental Si from enriched SiO2 by magnesium reduction in a closed crucible: 200 mg oxide + 170 mg freshly filed Mg (avoid excess Mg or Mg2Si forms), pressed into a capped Ta crucible, 1000 C for 1 h under vacuum, MgO leached 48 h in 2N HCl, product outgassed at 1000 C; overall yield ~70%, and 70-80 mg of reduced Si makes one 1 mg/cm^2 target (Hinn).
SiO2 + Mg reduction; 200 mg oxide to 170 mg Mg; ~70% yieldSource, quote & tabletop applicability
A large excess of Mg must be avoided to preclude formation of Mg2Si instead of Si.
Tabletop: The whole metallothermic-reduction pattern (reductant choice, closed crucible, acid leach of the oxide by-product) is the standard route from affordable oxide feedstock to a solid target; directly relevant if boron or silicon targets are ever made from oxide.
-
Internally stressed deposits have a shelf life: Hinn's 1 mg/cm^2 Si targets slowly curled and fractured within about two weeks (trapped impurities producing stress); targets left on their copper substrate could be recovered by re-annealing, and finished targets were stored under vacuum or argon.
Source, quote & tabletop applicability
they would slowly curl and fracture
Tabletop: Plan target fabrication against the run schedule, not the calendar — a self-supported evaporated or reduced film is a perishable. Vacuum/argon storage and use-within-weeks discipline belong in the ops checklist.
-
Slackened stripper foils live ~10x longer than taut ones: ATLAS (Pardo) mounts 2 ug/cm^2 arc-evaporated carbon on a holder whose diameter is then reduced to slacken the foil, gaining approximately an order of magnitude in lifetime (Ni beams: ~5 particle-nA-hours on target, ~1.0 particle-uA-h on the foil). ORNL (Ford) got reliable mass production of slackened foils by mounting them still wet in an airstream so they slip on the frame.
slackening ~10x foil lifetimeSource, quote & tabletop applicability
slackening gives approximately an order of magnitude increase in the foil lifetime.
Tabletop: Thermal-cycling stress, not sputtering, kills taut thin foils — the slack lets the foil move instead of tear. Any thin window, stripper, or degrader foil on a small machine should be mounted with deliberate slack (or spare stock budgeted; heavy-ion foil lifetimes ran minutes to hours).
-
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 & tabletop applicability
is expected to be only the order of 1 hr.
Tabletop: Proton beams are far gentler than 127-I, but the engineering lesson stands — anything thin in the beam needs replacement without opening the chamber. A multi-position foil/target ladder on a next machine's chamber costs little at design time and a vent-and-pump cycle every failure otherwise.
-
A cyclotron can feed stripper foils through the dee itself: the Chalk River superconducting cyclotron mounts glow-discharge (cracked ethylene) carbon foils at fixed intervals on a continuous bicycle chain that passes down the hollow coaxial-tuner conductor and into the upper dee half via the dee stem; expected foil lifetimes minutes to hours; failed foils advance to a magazine replaceable through a vacuum lock. Foils must be flat — ripples increase effective source thickness and degrade the first-orbit definition (Gallant & Dmytrenko).
Source, quote & tabletop applicability
foils must be flat since ripples increase the effective source thickness and thereby degrade the performance.
Tabletop: An existence proof that in-vacuum consumable-changers can share space with a live dee structure, and the cleanest statement in this collection that foil flatness is an orbit-quality parameter, not cosmetics — relevant to any internal-foil or internal-target scheme.
-
Glow-discharge (cracked-hydrocarbon) carbon beats arc-evaporated carbon for foil lifetime only above ~10 ug/cm^2: at 2-5 ug/cm^2 all fabrication methods gave about the same lifetime (Pardo/ATLAS); the stripper-foil discussion (Adair) found published comparisons mostly invalid because beams and current densities differed, and called for same-beam side-by-side lifetime tests.
Source, quote & tabletop applicability
no method seems superior to the arc evaporated foil.
Tabletop: Two lessons — pick fabrication method by thickness regime, and distrust any foil-lifetime claim not measured under your own beam and current density. The same skepticism applies to target-durability claims generally.
-
The saddle-field ion source is the cold path to sputtered targets: its beam carries a high fraction of energetic neutrals (sputters insulators as well as conductors), focuses to ~2 mm (small isotope quantities), and heats the evaporant only ~10 C — no damage to substrate or release agent, so substrates can sit very close for high collection efficiency; no magnetic field, electrostatic only (G. Thomas, ANL).
Source, quote & tabletop applicability
a cold filament which produces a temperature rise of the evaporant of only ~ 10 C
Tabletop: The commercial gun class (Ion Tech FAB11NS type) is bench-scale and vacuum-modest — the natural route to boron and refractory films for targetry without an e-gun; neutral-beam operation also suits insulating targets that would charge under ion-only sputtering.
-
Saddle-field sputter setup numbers (Thomas, ANL): gun at 30 degrees to the target surface and ~5 cm away (steeper angles back-sputter material into the gun); vacuum ~1e-5 Torr with high-purity argon at very low flow (chamber pressure rises only ~0.2e-5 Torr); ~2 mA at 6 kV; component alignment is critical — misalignment shorts the source; the beam is visible in the dark for alignment.
30 deg incidence, 5 cm standoff, ~1e-5 Torr, ~2 mA @ 6 kVSource, quote & tabletop applicability
the gun be at a thirty degree angle to the horizontal surface and about 5 cm from the sputter source.
Tabletop: A complete recipe card for commissioning a sputter gun in a diffusion-pumped bell jar of exactly the archive's class; the see-the-beam-in-the-dark alignment trick costs nothing.
-
Budget time, not power, for sputtered targets — deposition rates are tens of ug/cm^2 per hour: measured saddle-field rates were Au ~44, Sn ~14, W ~12.5, Ni 5-13, Fe 4-10, Si ~4 ug/cm^2/hr (Glover, Drinkwater, and ANL columns agreeing on Au). About half an hour to stabilize, then the rig runs virtually unattended for days.
Au ~44, Sn ~14, W ~12.5, Si ~4 ug/cm^2/hrSource, quote & tabletop applicability
it can be left virtually unattended overnight and usually for several days with only slight adjustments.
Tabletop: A 1 mg/cm^2 durable film is a multi-day sputter run — schedule accordingly or reserve sputtering for thin layers and adhesion coats; deposits are notably adherent, with a small implantation component.
-
Focused-ion-beam sputtering is the scarce-isotope economizer: GSI (Folger) consumed only 2.3 mg of Zr to make five 0.1 mg/cm^2 targets on carbon backings with a 1 mA, 10 kV Ar+ beam focused to ~1 mm on the cathode (Sletten-type apparatus); self-supported 0.2-0.5 mg/cm^2 rare-earth sputter layers were routine after dissolving a copper substrate.
2.3 mg Zr -> 5 targets x 0.1 mg/cm^2Source, quote & tabletop applicability
only 2.3 mg of Zr were consumed in the preparation of 5 targets of 0.1 mg/cm2
Tabletop: Sets the material-efficiency benchmark for enriched or expensive feedstock (boron isotopes included) — milligrams in, multiple targets out, versus tens of milligrams lost in an evaporation plume.
-
Stretch fragile foils flat with O-ring compression against a polished reference surface: the Argonne stretcher (Radford) clamps the foil between an O-ring and a tapered ring, then a central tube with an optically polished top lifts the foil; tightening the screws compresses the O-ring and draws the foil taut across the polished face. Near-100% success on 2-10 mg/cm^2 gold; foils stayed stretched under beam heating and after evaporating target material onto them; foil-to-foil gap verified capacitively down to ~3 um.
Source, quote & tabletop applicability
with adequate care to ensure cleanliness, high quality RDM targets and stoppers can be produced reliably and easily
Tabletop: The general mounting lesson — flatness comes from a polished reference surface plus elastomer-mediated even tension, and cleanliness of foil and surface set the achievable quality. Capacitance-vs-distance is a nonmagnetic gap gauge usable anywhere two conducting planes must be set um-close.
-
Thermally stretch polypropylene windows over a heated dome and metallize them gently: Chalk River stretched 25 um film over a Teflon-coated disc held with a deliberate radial gradient (edge 105 C, middle 115 C, center 125 C) to ~75 ug/cm^2; a 10 ug/cm^2 cellulose-nitrate undercoat raised heat resistance; then Cr 5 ug/cm^2 in two steps and Au 20 ug/cm^2 in three steps with cooling pauses — single-step evaporation ruptured the film by radiant heat (Dmytrenko et al.).
stretch 105/115/125 C; CN 10 + Cr 5 (2 steps) + Au 20 ug/cm^2 (3 steps)Source, quote & tabletop applicability
Attempts at single step evaporations to these thicknesses were unsuccessful because of rupturing of the foil due to heat damage.
Tabletop: Stretched polypropylene is the standard thin window for gas counters and low-energy vacuum isolation; the step-and-cool metallization discipline applies to coating any plastic film. Same material class as the detector windows the diagnostics literature assumes.
-
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 & tabletop applicability
any remaining traces of moisture would result in failure to produce a self-supporting target
Tabletop: The two moisture checkpoints (bake substrate before the parting agent; methanol-displace water after float-off) are cheap insurance on every float-off evaporation — the same practice ORNL-3021's thin-film procedures assume but rarely state.
-
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 (Behrndt geometry), versus 23% for a static substrate at close range; Maier (Munich) measured ~1% in practice by Au x-ray fluorescence. Static close-crucible geometry still wins on economy: 186 ug/cm^2 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 & tabletop applicability
there is a "best ratio" r/h 0.7 which generates a minimum relative thickness variation far below 1% across the target.
Tabletop: The uniformity-vs-economy trade in one number pair. GSI's rotating fixture (tilted 7 deg, 12 rpm) held +-1% on plate centers for stripper-foil carbon by the same principle — a small motorized turntable upgrades any 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 & tabletop applicability
This prevents target damage by gas out-rush.
Tabletop: Even a desiccator-scale target store benefits from the two habits — throttled first venting/roughing near fragile foils, and treating cooling-water plugging as an expected failure mode with a flow alarm rather than a surprise.
-
A solid target in a circulating (storage-ring) beam is thickness-capped by beam heating and thermal runaway: IUCF Cooler design (Lozowski) tolerates only ~1 ug/cm^2 (C) to ~1.5 ug/cm^2 (Bi) with the beam traversing ~1e6 times/s; thicker targets defeat the cooling and dump the stored beam. Proposed solid-target routes: graze the beam edge with the target edge, and use fibers/whiskers (7 um C fiber ~975 ug/cm^2, 0.5 um quartz ~80 ug/cm^2) as overcoated substrates.
max ~1-1.5 ug/cm^2 for stored-beam solid targets; C fiber 7 um ~ 975 ug/cm^2Source, quote & tabletop applicability
thermal runaway would occur and the stored beam would be lost.
Tabletop: Directly relevant to the synchrotron campaign, not the cyclotrons — any internal-target idea for a ring must respect the multiple-traversal multiplier, which turns nanoamp circulating currents into effective milliamp bombardment.
-
Chemical vapor deposition makes thick refractory films from milligram feedstock: Chalk River (Gallant) flowed dilute H2 + WF6 over an induction- or lamp-heated susceptor at ~500 C and produced good-quality tungsten films over 2 mg/cm^2 thick; only the susceptor reaches reaction temperature, so very small quantities of W, Ta, or Mo serve, and the H2 sweeps out the fluorine by-product. Flagged as nearly absent from target-lab practice at the time.
H2 + WF6 -> W film; susceptor ~500 C; films > 2 mg/cm^2Source, quote & tabletop applicability
very small quantities of metals such as tungsten, tantalum, and molybdenum can be used in miniature systems
Tabletop: The one route in the volume to thick refractory-metal targets and coatings without an e-gun or rolling mill — though fluoride chemistry demands real gas-handling respect; note the parallel to CVD boron routes if boron targetry is ever pursued.
-
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 & tabletop applicability
relatively high strengths and in some cases were virtually transparent.
Tabletop: A genuinely low-tech thick-oxide route — solution chemistry plus an oven, no vacuum plant — suited to oxide targets (including B2O3-adjacent chemistry) where elemental form is not required; loading scales with solution concentration.
-
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 & tabletop applicability
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.
Tabletop: Marginal technically for a proton machine, but present as the worked example of matching host-material physics (crystal symmetry, conductivity, heat sinking) to what the measurement needs — and as the rights-boundary marker for this volume.
-
Expect multipactor start-up failure specifically in self-excited machines where the dee IS the oscillator tank: conventional cyclotrons driven from external oscillators with their own resonant tank circuits suffer only slight difficulty, but a simple-dee-as-tank-circuit oscillator can fail to break into full oscillation at all. Diagnose the architecture before blaming the amplifier.
Source, quote & tabletop applicability
in cyclotrons using a simple dee system as the tank circuit difficulties are encountered in getting the oscillator to break into full oscillation.
Tabletop: DIRECT — this sentence names the exact configuration of the 8" machine (simple dee system as the tank circuit) and matches its documented multi-year pattern of RF amplifiers failing to bring the dee to voltage. Multipactor loading in the ~100 V band is a named, testable candidate cause for that history, distinct from amplifier inadequacy.
-
The two conventional multipactor-start cures each carry a cost: (1) bias the dee and dee stem several kV from ground (customary on FM cyclotrons) — costs HV isolation of the whole dee structure and mechanical complexity; (2) drive the oscillator strongly from an external RF source so order-100-V multipactor loading cannot stall the rise — costs a second RF source and changeover logic (some installations remove the drive automatically after start, some do not). Same pair as mddc-1045 p.12 (DC sweeping bias; tickler oscillator) — the two reports agree.
Source, quote & tabletop applicability
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.
Tabletop: The decision menu for any machine that stalls in the multipactor band: bias, drive-through, or (this report's contribution) 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 few-hundred-volt DC offset on the dee — pick by which fights the existing hardware least.
-
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 & tabletop applicability
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.
Tabletop: Transferable decision pattern: on a machine whose dee stem is grounded through the tank structure, retrofitting DC bias means rebuilding the stem insulation, while a shock starter touches nothing but a spare port. Choose the quench that is additive.
-
Third multipactor cure — impulse (shock) excitation: a small coupling loop inside the dee stem tank, fired by a capacitor discharge through an air spark gap, rings a surge of HF current into the tank walls and plate/grid circuits that shocks the dee to several hundred volts — above the multipactor band — after which the oscillator builds to full voltage unaided.
shock amplitude needed ~ several hundred volts on the dee (just above the order-100-V multipactor band); oscillator completes the rest of the buildup itselfSource, quote & tabletop applicability
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.
Tabletop: The cheapest cure in this collection for a stalled self-excited start: one loop, one capacitor, one spark gap, one HV supply — all amateur-stock parts. The key insight is that the kick need only clear the top of the loading band, not deliver operating power; everything above a few hundred volts is the oscillator's own job.
-
Sparker circuit values that worked: 500 pF total charged through 700 kilohm from a 30 kV supply into an air spark gap (about 0.2 J per spark), gap spacing adjusted for roughly two sparks per second — and ordinarily a single spark starts the oscillator.
E = C*V^2/2 = 500e-12 * (3e4)^2 / 2 ~ 0.22 J per spark; RC charge time ~ 0.35 ms, rate set by gap spacing to ~2/sSource, quote & tabletop applicability
The spark gap is adjusted so that the sparking rate is roughly two per second. Ordinarily a single spark will cause oscillation to commence.
Tabletop: Complete parts list (values on Fig.2, PDF p.8). A sub-joule impulse sufficed on a 27" machine; a smaller dee system needs proportionally less. The 30 kV supply is the only nontrivial part, and a NST or flyback-class supply covers it.
-
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 & tabletop applicability
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.
Tabletop: DIRECT automation pattern: gate the starter on (RF enabled) AND (dee pickup below threshold). The dee capacitive pickup already present for voltage monitoring is exactly the signal needed, and the same logic doubles as a stall alarm — sparks repeating at 2/s means the machine is failing to start.
-
Decouple an auxiliary coupling loop from steady-state operation by geometry: orienting the sparker loop with its plane perpendicular to the tank axis makes the RF voltage induced in it very small even at full dee voltage, so the spark circuitry neither loads the running machine nor gets destroyed by it — sparks occurring during operation cause no perceptible change.
Source, quote & tabletop applicability
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.
Tabletop: General principle for any diagnostic or starter coupling added to a resonator: choose an orientation that is null for the operating mode. The impulse still couples because the spark's broadband ring excites wall currents, not the clean mode — an inefficient coupler is acceptable precisely because the required kick is small.
-
The decay envelope of a ringing dee maps the multipactor band edges: with plate power off, spark-induced dee oscillations fall smoothly until the voltage reaches roughly 1/3 of its (few-hundred-volt) maximum, drop steeply through the loading band, then decay slowly again below it. This is an experimental confirmation that multipactor loading occupies a BOUNDED voltage window — refining mddc-1045 p.12 (discharge exists only below ~500 V extinction) with a directly observable top edge. The observation bounds the band but does not discriminate between the proposed gap and axial multipactor mechanisms, so it contradicts neither.
sharp-drop onset at ~1/3 of the ringdown maximum; loading band top ~ order 100 V hereSource, quote & tabletop applicability
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.
Tabletop: A free diagnostic: ring the dee (impulse or drive-and-release), scope the pickup envelope, and look for a kink. A visible steep-decay segment localizes the multipactor band on YOUR machine and tells you whether nominal operating voltage sits inside it — the critical question for any dee running near a few hundred volts.
-
A shock start does not depend on the oscillator tube's state: initial dee-voltage response to the sparker was unchanged with plate power on or off and filament on or off, while retuning the grid circuit changed the spark-induced amplitude severalfold — the impulse energy reaches the dee through the passive resonant system (with considerable capacitive current through the tube), not through tube gain.
Source, quote & tabletop applicability
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.
Tabletop: Two practical consequences: the shock method transfers to solid-state drivers (nothing about it is tube-specific), and every branch circuit hanging on the resonator participates in the ring — tune-dependent shock amplitude means the starter should be commissioned at the operating tune, not on the bench.
-
Impulse starting needs a healthy resonator and modest gas load — it fails when tank gas pressure is too high or the feedback (grid) loop is detuned, and after a major shutdown the outgassing must begin at the smallest-cavity (highest-frequency) tuner position for the shock to take. The ringing itself is broadband and self-tuned: ~12 Mc regardless of oscillator condition, decaying 50% in ~3 cycles.
sparker loop ring ~12 Mc on a 10-20 Mc machine, Q-equivalent ~ few (50% decay in ~3 cycles) — no tuning of the sparker needed across the bandSource, quote & tabletop applicability
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.
Tabletop: Sets expectations honestly: the shock cures the multipactor stall, not bad vacuum or a detuned feedback network. If a spark does not start the machine, the fault list is pressure, tune, or outgassing state — a diagnostic branch in itself. The low-Q broadband ring means one fixed sparker covers a whole tuning range (trivially true at fixed frequency).
-
For an add-on impulse coupler, prefer inductive over capacitive coupling to the dee when the dee chamber is crowded and RF pickup on the starter circuitry is a concern; energy-transfer efficiency was "extremely small" and still adequate, with tighter loop coupling or a tuned sparker loop available as upgrades never needed in practice.
Source, quote & tabletop applicability
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.
Tabletop: Directly usable trade note: a loop near the dee stem (outside the beam region) beats a capacitive plate facing the dee in a small chamber where every square inch by the dee is contested. Do not optimize the coupler — "works with margin" arrived at the first, deliberately inefficient geometry.
-
A passive magnetic mirror made from a 1/8"-diameter steel bearing ball inserted at the top of the arc hood reflects electrons streaming up the arc channel (mirror cone sin^2(theta_c) = B0/Bmax): a one-part, zero-power upgrade that converts a hooded-arc filament source to reflex (electron-oscillating) operation inside the cyclotron's own field.
sin^2(theta_c) = B0/Bmax (electrons outside the cone reflect; Spitzer 1956)Source, quote & tabletop applicability
a magnetic mirror built into the upper end of the arc hood by the simple insertion of a steel bearing ball 1/8" in diameter.
Tabletop: DIRECT and nearly free for any filament hooded source running in the main field: a bearing ball is stock hardware and the hood already exists. This is the halfway house between a plain filament arc and a cold-cathode PIG — same electron-reuse physics, no second cathode, no separate supply.
-
Read where arc electrons land from incandescence: before the mirror the graphite hood top glowed bright orange under electron bombardment during arc operation; after, it stayed black. Hood-glow color is a free, direct diagnostic of electron end-loss (and of mirror effectiveness) visible through any viewport.
Source, quote & tabletop applicability
the top of the graphite hood glowed a bright orange color when the arc was operating, because of the intense electron bombardment.
Tabletop: A diagnostic that costs a glance: if the chimney/hood top of a small source runs orange-hot, the arc power is exiting axially instead of ionizing gas — evidence for adding reflection (mirror or repeller) and a before/after check that it worked.
-
Reflex electron economy: with electrons oscillating between the magnetic mirror above and electrostatic repulsion from the filament structure below, the arc current required for a given hydrogen ion yield fell severalfold. Each trapped electron ionizes on many passes instead of one transit.
Source, quote & tabletop applicability
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.
Tabletop: The physics argument for reflex geometry at any scale — the same multiple-pass ionization a PIG buys with two cathodes, obtained here with one filament, its own space charge, and a ball. Severalfold less arc current means severalfold less filament drive, heat, and gas decomposition in a source the size of a thumb.
-
Filament life scales strongly with required emission: cutting the needed arc current severalfold (via reflex operation) let the filament run cooler, stretching typical 60-mil tungsten hairpin lifetimes of 15-30 hours to an intact-though-thin filament at 109 hours. Fixing electron economy is a filament-lifetime fix, not just a power fix.
lifetime 15-30 h at full emission -> >109 h severalfold-reduced emission (same 60 mil W hairpin)Source, quote & tabletop applicability
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.
Tabletop: Directly answers the standing filament-source maintenance complaint: a 3-7x life extension from a passive part is worth more per run-hour than any filament-material change. Tungsten evaporation is brutally steep in temperature, so every ampere of arc current not needed pays back in hours.
-
Mirror-assisted source behavior is geometry-sensitive and was not understood even by its inventor: the identical steel-ball mirror transplanted into a second hooded source failed outright, the only 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 & tabletop applicability
is mounted with its plane vertical, parallel to the magnetic field of the cyclotron, rather than perpendicular as in the first source.
Tabletop: An honest negative result from 1961 that still stands: the electron injection angle into the mirror (set by filament orientation relative to B) decides whether electrons are inside or outside the loss cone. Plan the mirror experiment as an A/B test with the glow diagnostic, and try filament orientation as a variable if the first try fails.
-
Shrink the hood extraction opening to cut source gas flow into the tank — 1/32" x 3/16" sufficed for protons/deuterons here and measurably lowered tank pressure — 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 & tabletop applicability
after a few days of operation, it was found to have become somewhat enlarged in the direction of ion rotation.
Tabletop: Two rules in one: (a) the chimney slit is the gas throttle — sizing it small is the cheapest pumping upgrade a small machine can get; (b) the asymmetric erosion (beam-side, along rotation) is both a wear mechanism and an inadvertent beam diagnostic showing where first-turn ions strike the hood.
-
Hooded-arc operating envelope on a 27" machine, 7-14 kG: arc currents to 2 A and arc voltages to 250 V were used, but deuterium ran on about 0.75 A at about 100 V — and pushing arc current from 1.0 to 2.0 A bought only a relatively small beam increase. Run at the knee of the yield curve, not at maximum arc.
deuterium: ~0.75 A / ~100 V sufficient; beam saturates between 1 and 2 A arc; B = 7,000-14,000 gauss (NOTE: "deuterium" is a handwritten correction over typed "hydrogen" on the page)Source, quote & tabletop applicability
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.
Tabletop: Concrete supply-sizing anchors: ~100 W of arc fed a 27" machine's proton beam. The saturation observation is the operating doctrine — beyond the knee, extra arc current buys filament wear and gas load, not beam. Find the knee on your own source and park below it.
-
Optimize the source per species rather than forcing one design: the H/D mirror source gave only ~1/10 the alpha beam of the dedicated helium source (also hooded — a tantalum button on a quartz spacer atop a tantalum-tubing hood, with a larger ~1/8" x 3/8" opening). Ionization economy, hood material, and slit size that win for one gas can lose for another.
Source, quote & tabletop applicability
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
Tabletop: Mostly a scoping warning for any future gas change: a source tuned for hydrogen is not a universal source. The tantalum-button-on-quartz construction detail is also this collection's only sketch of a helium-specific hooded source, useful if alphas are ever on the menu.
-
Keep the magnet gap length no more than about half the orbit radius if the field must be shimmed to a prescribed shape: field solutions in the gap cannot be controlled by pole-surface contouring when the gap is deeper than that. The calutron magnets set gap = 24 in. for rho = 4 ft and 13.5 in. for rho = 2 ft.
l_gap <= ~rho/2 for shimmable fieldSource, quote & tabletop applicability
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.
Tabletop: 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.
-
Derive the allowable field gradient from the allowable bowing of the flux lines, not the other way around: for a line bowing x over half-gap h, x = (h^2/2)(1/H)(dH/dx) (from curl H = 0 at the midplane). Powell's worked case — 0.5 mm allowable bow over a 250-mm path with h = 125 mm — gives a maximum edge-ward gradient of 0.16 per cent per inch.
x = (h^2/2) * (1/H) * (dH/dx); calutron limit 0.0016/inSource, quote & tabletop applicability
is the maximum allowable space rate of change of the magnetic field in a direction toward the edge of a gap.
Tabletop: The general move — translate a beam-geometry tolerance into a measurable dH/dx budget via the curl-free midplane relation — is machine-independent and gives a field-map pass/fail number before any tracking is run.
-
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 & tabletop applicability
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
Tabletop: Same arithmetic every H-frame designer runs today (corroborates the ampere-turn sizing in Wouters and Zickler's CAS magnet notes); the 85-95% efficiency band is a sanity check on any FEMM excitation result for an unsaturated return frame.
-
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/1e5)^2 * (mean turn in.)^2 (Cu); J = 486*sqrt(P/W_c)Source, quote & tabletop applicability
the product of the power and weight of a coil conductor depends on the ampere turns and the mean diameter of the coil.
Tabletop: 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.
-
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 & tabletop applicability
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
Tabletop: Brackets the usual 1.5-2.5 A/mm^2 air-cooled small-magnet guidance from the modern side (Zickler/Tanabe territory) with 1940s operating experience; a passively cooled tabletop coil should sit at or below the bus-bar figure.
-
Assume a coil space factor (copper volume / coil-container volume) of ~0.5 for purpose-wound oil-cooled coils at preliminary design; expect 0.30-0.37 when forced to use whatever conductor stock is available rather than sizes designed for the job.
space factor ~ 0.5 designed; 0.30-0.37 with off-the-shelf conductorSource, quote & tabletop applicability
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.
Tabletop: Amateur coils are almost always wound from available magnet wire — budget the pessimistic 0.3-0.4 space factor, not the textbook 0.5, when sizing the coil window.
-
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 & tabletop applicability
both the first cost and the power cost of a magnet increase almost proportionately with an increase in beam radius.
Tabletop: 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.
-
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 & tabletop applicability
The forces tending to separate the halves are surprisingly large and if overlooked can be disastrous.
Tabletop: Directly relevant to removable pole caps and bolt-on shim plates on a small H-frame — the retention hardware must react a lateral load, not only the axial pull normally computed from B^2/2mu0.
-
Working force formulas (English units): pull between pole faces F[lb] = (kG)^2 x area[in^2] / 1.735; force on a conductor F[lb] = kG x amp x length[in] / 1750. Conductor hot-spot check for strip losing heat from two edges: Delta-T[C] (center to edge) = 0.0094e-6 x (width, in.)^2 x (J, A/in^2)^2 for copper — this sets the maximum strip width.
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 & tabletop applicability
Force between pole faces (lb) = 1/1.735 X (kilogauss)^2 X area (sq in.)
Tabletop: 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.
-
Order of design operations for an iron magnet: (1) fix gap size, field, and uniformity from beam requirements; (2) choose the magnet topology by iron economy — adjacent gaps can share return yokes, and as gap count grows the structure approaches a solenoid with constant steel, copper, and power per gap; (3) keep the driving coils as close to the air gaps as possible to limit field spreading and bowing; (4) rough out Cu/Fe/power; (5) settle details on a scale model.
Source, quote & tabletop applicability
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.
Tabletop: 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.
-
For absolute field intensity with an induction coil, only full 180-degree flips count: partial throws are acceptable for relative and bucking measurements but not for absolutes, because the flipped flux change is exactly 2*B*A only at 180 degrees. Full-scale magnet magnetization curves were taken exclusively by flip coil for this reason.
delta-phi(180-deg flip) = 2*B*A_effSource, quote & tabletop applicability
In accurate determinations of the absolute magnetic field intensity, only angular throws of 180 deg are considered satisfactory.
Tabletop: 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 an integrator, provided the flip is a true reversal.
-
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 & tabletop applicability
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.
Tabletop: Transfers verbatim to any ADC/integrator field mapper — calibrate at deflections spanning the readings, with the same input impedance, rather than trusting one scale factor.
-
Build the calibration chain on geometry: a single-layer solenoid coil wound on an accurately machined cylinder has effective area pi*D^2*N/4 good to at least 0.1 per cent when wire diameter << cylinder diameter — a primary area standard any shop can make. Calibrate random-wound working coils against it (rotate-to-null comparison, A = S*sin-theta), or in a long solenoid with a tapped bucking secondary (mutual-inductance formula good to 0.05 per cent).
A_eff = pi*D^2*N/4 (single layer, mean D center-of-wire to center-of-wire)Source, quote & tabletop applicability
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.
Tabletop: A machined-spool primary standard plus a fluxgate-free comparison puts sub-0.5% absolute field capability in a home lab; it is the piece that turns a flip coil from a relative into an absolute instrument.
-
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 & tabletop applicability
The value of X is 0.35 per cent, which is verified in practice.
Tabletop: Sets the realistic error floor for coil-and-integrator absolute field measurement; a Hall probe certified to 0.1% is genuinely better than the classical chain, but only if its own calibration is traceable.
-
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 (tilt or shunt) until excitation on/off gives zero net deflection. Supply drift then enters only the measured field DIFFERENCES — a 1 per cent current wobble costs 1 per cent of the (small) nonuniformity, i.e. ~1e-4 of the field for a 1 per cent contour.
series-bucked pair; error ~ (dI/I) x (delta-H/H), not (dI/I)Source, quote & tabletop applicability
A 1 per cent change in the exciting current produces an error of only 1 per cent in the changes in the magnetic field.
Tabletop: The classical answer to shimming with a wandering surplus supply — map relative structure differentially and pin the absolute scale with occasional flips; a modern two-channel Hall differential measurement inherits the same immunity.
-
Match the probe to the field structure: sample the field at a point, not an average — the model-survey coils were 0.20 in. diameter x 0.15 in. high (2000 turns of No. 46, ~350 turn-cm^2) so that 0.5 in. resolution on the full-scale magnet (1/32 in. on the 1/16 model) was preserved, and coil placement errors were held below 1/32 in. Verify by repeat runs that the finite coil size does not degrade the map.
probe dimension << field-structure scale / model scale factorSource, quote & tabletop applicability
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.
Tabletop: The active-area rule for Hall mapping a shim edge: a 1-2 mm sensor is marginal where the gradient scale is a few mm (pole edge, shim step); position repeatability of the mapper jig belongs in the same error budget as the sensor.
-
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 & tabletop applicability
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.
Tabletop: Maps directly onto modern integrator front-ends — put the gain in the coil (turns), keep the electronics gain low, and treat offset/drift correction as part of every run, not a once-per-day calibration.
-
Two low-tech field-shape tools worth keeping: (a) iron filings photograph the stray-field direction map, with slightly-magnetic stainless-steel filings filling in near sharp iron corners where iron filings migrate to the pole; print the pattern directly onto sensitized (blueprint) paper laid under the filings for an immediate permanent record, then take magnitudes with a coil at points on the printed pattern. (b) A mercury-arc discharge tube aligned with the field collapses its glow onto the field line, giving line-shape deviation measurable with a cathetometer.
Source, quote & tabletop applicability
stainless-steel filings (being slightly magnetic) sprinkled in this area will arrange themselves along the lines of force without accumulation.
Tabletop: Zero-cost qualitative diagnostics for a home lab — a filing map locates stray-field lobes and leakage paths before any probe survey, and the discharge-follows-field trick is a natural cross-check in a machine that already runs a plasma source.
-
Turn beam-physics tolerances into go/no-go field acceptance tests before measuring: the plant translated "focal pattern within 0.5 mass unit" into (a) an integral criterion — measured integral of h_z dx along the beam arc (30 series-connected coils on the orbit arc) must match theory within 3 cm of galvanometer deflection — and (b) template numbers laid over source-region data sheets (0.2%/in along the arc, 0.1%/in axially). Field quality became a pass/fail reading, not a judgment call.
acceptance = |integral h_z dx (meas) - (theory)| < deflection criterion; gradient templates 0.2%/in and 0.1%/inSource, quote & tabletop applicability
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.
Tabletop: The discipline transfers whole: derive numeric field-map acceptance bands from orbit tolerance (phase-slip or centering budget) beforehand, so a survey ends in pass/fail per region instead of open-ended interpretation. Orbit-integral quantities beat point values when the beam only feels the integral.
-
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 & tabletop applicability
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.
Tabletop: 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.
-
Match model scale to question precision: 1/16 scale answered every production design question (excitation, end effects, forces, flux allocation, stray field), but for the finest field-uniformity contour maps the team deferred to the 1/8-scale model of the same pole geometry as inherently more accurate. Bigger model only where the question demands it.
Source, quote & tabletop applicability
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.
Tabletop: The mesh-refinement decision in physical form — coarse resolution for excitation/force/leakage questions, fine resolution only for the ppm-level uniformity region; spending fine-model effort on questions the coarse model already answers is waste in either medium.
-
The standard model-test suite, in reporting form: (1) saturation curve H_g vs NI/l_g; (2) efficiency vs NI/l_g; (3) leakage coefficient at various points (directly applicable to full scale); (4) uniformity contour maps of (H-H_g)/H_g on normalized pole coordinates; (5) stray-field map. Plus, in practice: gap-to-gap comparison, flux audit of every iron member, and magnetic forces. This is the complete characterization a predictive model owes the design.
report H_g(NI/l_g), eta(NI/l_g), L(x), (H-Hg)/Hg contour map, stray mapSource, quote & tabletop applicability
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
Tabletop: A ready-made deliverables checklist for a simulation campaign on a new magnet — a FEMM study that produces these five plots plus a member-by-member flux audit has done what the 1944 model program did, in the same order.
-
Track efficiency (gap mmf / total mmf) at TWO field levels as the saturation health check: the revised Alpha II model measured 95.6 +/- 2.0 per cent at 4600 Oe and 95.4 +/- 2.0 per cent at 3400 Oe — equality within error at both excitations demonstrated the iron was nowhere near saturation and the design 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 field levelsSource, quote & tabletop applicability
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.
Tabletop: A two-point excitation scan (measured or simulated) separating "efficiency constant" from "efficiency dropping" localizes saturation onset without any interior probe — directly usable on an H-frame by comparing measured B vs I against the linear NI prediction at two currents.
-
Audit the flux through EVERY iron member with wound loops and a ballistic integrator: loop-flux differences divided by enclosed-area differences give local leakage flux components (horizontal and vertical separately, by choosing loop pairs); dividing member flux by member steel area gives its working induction. Alpha II verdicts: core steel 12,000 G comfortable; core rim 17,460 G too high (fixed by the thicker full-scale rim, ~15,000 G, mu ~ 550); yokes at 10,000-15,000 G "good"; deliberately sacrificial cooling-tank walls saturated at ~30,000 G.
B_member = (phi_loop difference)/(A_steel); leakage component = d-phi/d-A between loop pairsSource, quote & tabletop applicability
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.
Tabletop: 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.
-
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 & tabletop applicability
the corresponding permeability would drop to 118, which is dangerously low. In certain localized regions it might even be lower.
Tabletop: Gives this collection a quantitative "too far": mu ~ 100-150 at the working point is the failure territory, and the audit must use the actual steel''s curve — the same reason a FEMM model of an H-frame is only as good as the 1010/1018 B-H table fed to it.
-
Correct model predictions for known model/prototype differences, with signs stated: the team measured permeability of BOTH the model steel and the full-scale steel (full-scale better -> full-scale performs slightly better), and tallied deliberate geometry differences (model rim proportionally 1 in. thinner -> model worse; model coil-tank iron 0.5 in. thicker -> model worse). Every known discrepancy got a direction, so the prediction became a bound, not a guess.
Source, quote & tabletop applicability
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.
Tabletop: The sign-audit habit transfers to simulation directly — list every model-vs-hardware difference (B-H table provenance, fillets, packing factor, gaps at joints) with the direction it biases the prediction, so measured-vs-predicted discrepancies arrive pre-explained.
-
Find end-cell compensation empirically by two-point linear extrapolation: end coils adjacent to a yoke theoretically need 50 per cent of a full coil (each gap shared by two coils), but yoke reluctance leaves end gaps low. Alpha II (revised): 50% turns -> end field 4.0% low; 57.7% -> 0.73% low; extrapolated optimum 59%. Other magnets landed at 61.5% and 55%, and XBX at 66-2/3% taps — so BUILD IN TAPS and settle the ratio by measurement.
measure end-gap deficit at two end-coil turn ratios; extrapolate linearly to zero deficitSource, quote & tabletop applicability
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.
Tabletop: The general pattern — a boundary cell needs measured, adjustable over-excitation (or shimming), and a two-point measurement plus linear extrapolation converges in one iteration — applies to any edge-compensation knob: outer-radius shim thickness, trim turns near a yoke window, or a correction-coil ampere-turn setting.
-
If flux leaves the pole structure at higher density than the gap average, spread it before it crosses any tolerance gap: the Alpha II cellular core emitted flux from 50%-steel at twice the average density, which would have doubled both the mmf across the core-to-tank tolerance gap and the wall force; a thin steel faceplate over the core face equalized the flux before the gap. (Full-scale analog: stacked H-beam core inserts forming a continuous plane.)
without spreader, gap mmf and local force scale with B_local^2/B_avg^2 concentrationSource, quote & tabletop applicability
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.
Tabletop: 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 — a modest face sheet decouples interior steel economies from gap-field quality.
-
Convert the model into a force ledger before detailing structure: combine magnetic wall pressures with atmospheric pressure on vacuum walls (Alpha II: 171 t magnetic out, 116 t atmosphere in, 96 t internal field in -> net figures per wall); remember force goes as the average of H^2, so averaging H first understates it; then publish safe-envelope numbers for the structure (200 t core-tank max, 30 t unbalanced, 175 t/side track tension, 350 t on end yokes, 20 t tank-ejection allowance).
F ~ integral H^2 dA (use mean of squares); tabulate per-member envelope with marginSource, quote & tabletop applicability
the forces calculated on the basis of the average over the entire region will be lower than the true force.
Tabletop: 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).
-
Gap-spacing tolerance for field quality between a pole structure and an inserted wall (Nelson-Frankel-Richardson criterion): keep the separation large enough that the MAXIMUM separation never exceeds twice the minimum separation. Fractional tolerance on a parasitic gap, not absolute flatness, is what the field cares about.
s_max <= 2 * s_min over the parasitic gapSource, quote & tabletop applicability
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.
Tabletop: Governs any shim pack, pole-cap seat, or chamber-lid-under-pole arrangement: a deliberately larger uniform standoff can beat a smaller irregular one, because +/-50% of a big gap passes where +/-50% of a tiny gap is unmachinable.
-
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 & tabletop applicability
The magnetic performance of the track is better than predicted from the model experiment.
Tabletop: The historical calibration point for any predict-then-verify magnet pipeline: a faithful scaled model (same-steel/same-B then; validated FEM now) lands within a few per cent on global quantities and errs conservative when the prototype''s iron is better than the model''s — but the trust was EARNED by one full validation campaign, not assumed.
-
After the first article validates the prediction chain, degrade acceptance testing to mechanical metrology: once track 1's 71 tanks all passed magnetic tests and shim-position measurements were shown sufficient to guarantee the field, track 6 was accepted on a dimensional check of shim positions alone, with magnetic spot checks only for special questions (end-tank asymmetry).
Source, quote & tabletop applicability
the excellent results obtained in testing track 1 showed that a dimensional check of the shim positions was entirely adequate.
Tabletop: The economic payoff of validation: once field-vs-geometry is established (by model/simulation plus one measured article), later shim changes can be accepted on caliper and indicator readings, reserving full field maps for genuinely new configurations.
-
Expect field CORRECTION to be trial and error, and budget for it: the 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 the team concluded the only feasible correction method for out-of-criteria fields was iterative cut-and-try.
Source, quote & tabletop applicability
It would appear that the only feasible method of making corrections when the necessity arises is by trial and error.
Tabletop: A 1944 warning that survives every FEMM run: analysis predicts the as-built field well but predicts CHANGES to an as-built field only if the change is modeled exactly as executed. Plan shimming as measure-cut-measure iterations, and keep shim stock adjustable.
-
Members held in place by field symmetry are in unstable equilibrium — anchor them: plant tanks crept as much as 2.5 in. out of their gaps over days of energized operation. The ejection force follows from reluctance-minimization energy accounting (flux-energy density H^2/8pi times the volume swept per unit displacement gave 9.71 tons maximum; tests bracketed the actual force between 4.53 and 9.71 tons), and it GROWS as the member moves out, until wall saturation reverses it.
F = d/dx [ (H^2/8pi) * V_field(x) ] ; force increases with displacement from symmetrySource, quote & tabletop applicability
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.
Tabletop: 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 invisible at the symmetric position and largest just when the part has already started to walk.
-
Cheap full-scale field techniques that earned their keep: compass-and-drawing-board flux plots (5/8-in. compass, 1/4-in. cross-section paper) traced field-line shape with error under 1/8 in. and repeat-trace checks under 1/16 in.; switchboard ammeters were calibrated against a potentiometer across the current shunt (magnetization curves were 2%-accurate, limited by the ammeter); and unregulated excitation was tolerated per-tank by correcting all readings to a reference field on the assumption that field SHAPE is invariant for small level changes.
Source, quote & tabletop applicability
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.
Tabletop: Three habits for a home lab: repeat-trace to certify a mapping method, calibrate the current METER (it is usually the accuracy floor of a B-vs-I curve), and normalize survey data to a monitor reading so supply drift cancels out of shape maps.
-
Copy a proven machine when one exists at your scale: the UW 60-inch followed the Berkeley Crocker cyclotron from a complete set of plans, followed "closely on the magnet design," plus sustained advice from the originating lab — and reached assembled-ready- for-test in three years. Original design effort was reserved for subsystems where the plans were silent (shims, controls, oscillator details).
Source, quote & tabletop applicability
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.
Tabletop: The same strategy that built the reference machine from the Rutgers/Houghton lineage. For any new machine, start from the closest documented working design (this corpus) and spend novelty only where the precedent is silent.
-
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 & tabletop applicability
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.
Tabletop: Any tabletop proton/deuteron machine sits far inside the fixed- frequency regime — phase slip there is set by field shaping and dee voltage, not relativity, so FM hardware is never the fix for small-machine beam loss.
-
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 & tabletop applicability
It is designed so as to take maximum advantage of naturally occurring shielding of a small ravine.
Tabletop: Physics transfers even if the scale does not: mass is mass, and cheap mass (earth berms, water tanks, basement corners) is legitimate neutron/gamma shielding for a D-D-capable machine. Spec detail: PDF p.128.
-
Specify magnet-core steel chemistry in the purchase order and verify it yourself: UW specified C 0.15 / Mn 0.5 / P 0.04 / S 0.045 / Si 0.2 per cent maximum (Table A), then machined a Rowland ring from forged steel of the same heat and took a full magnetization curve by ballistic galvanometer, because "the control of the magnetic properties in the manufacture of steel is rather uncertain." Gap induction predicted from that curve by elementary magnetic-circuit theory was later verified by direct measurement.
Specified max: C 0.15%, Mn 0.5%, P 0.04%, S 0.045%, Si 0.2%Source, quote & tabletop applicability
Apparently the control of the magnetic properties in the manufacture of steel is rather uncertain.
Tabletop: 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.
-
State the field-shape requirement as two separable specs before shimming: (1) the median-plane radial dependence must follow a defined falling law, and (2) inside the exit radius the field must be accurately symmetric about both the axis and the median plane. UW then attacked them as separate campaigns (radial shims; azimuthal correction; median-surface survey).
Source, quote & tabletop applicability
(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
Tabletop: 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.
-
A scale-model magnet is a close call — list the reasons before building one. UW's five advantages of the 1/12 model: cheap/fast shim iteration (especially if special alloys needing heat treatment were tried), work proceeds before the full magnet is done, no interference with other construction, convenient minor measurements, and future re-studies while the cyclotron operates. The two difficulties: spatial resolution of field measurement, and coil heat (current density scales as 1/L, heat per unit volume as its square). Verdict after the fact: "advantages and disadvantages ... were fairly closely balanced" — partly because part geometry constrained shim options more than expected.
Scaling at constant B: J ~ 1/L; heat/volume ~ J^2 ~ 1/L^2Source, quote & tabletop applicability
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.
Tabletop: 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).
-
If you do build a model magnet, pour it from the same heat as the full core and make it a precise replica: UW's 1/12 model used Midvale forgings "poured from the same heat and it can be assumed magnetic properties are identical," a precise replica except bolts and carrying lugs (227 lb), with cover plates made from scraps of the actual cover plate stock.
Source, quote & tabletop applicability
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.
Tabletop: The transferable rule is identity of 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, not a library curve for its nominal grade.
-
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 & tabletop applicability
the supporting structure for the coils failed, presumably under the magnetic forces. The coils became distorted and short circuits developed.
Tabletop: 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, and remember the yoke-steel trick — outer return-path steel raises gap field without touching pole-gap geometry.
-
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 by a lead screw — flipped simultaneously through equal angles. Cancelling most of the EMF permits high sensitivity on the DIFFERENCE and "eliminates the importance of many instrumental imperfections ... such as drifting of the exciting current, inaccurate flipping, inconstancy of the fluxmeter, and temperature effects"; it even made close regulation of the magnet current unnecessary (a hand rheostat sufficed). One reduced-sensitivity reading with the fixed coil alone establishes the percentage scale.
Source, quote & tabletop applicability
drifting of the exciting current, inaccurate flipping, inconstancy of the fluxmeter, and temperature effects
Tabletop: DIRECT — the differential trick ports to modern probes; two matched Hall/NMR channels read as a difference kill supply drift and thermal drift, the dominant error sources in a garage field survey. Same scheme reused on the full magnet with 28-turn, 0.607-cm-mean-radius coils (PDF p.30).
-
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 & tabletop applicability
at the exit radius the parameter n = - (r/B)(dB/dr) shall have the value 0.4.
Tabletop: DIRECT physics — the n = 0.4 exit target and monotonic ~1% interior droop are the same numbers this collection's Wouters and Livingston rules give, here as an as-built spec that produced a working field. A FEMM shim study should adopt criteria (1)-(5) as its objective function.
-
Check a max-performance shim against reduced-field operation before accepting it: UW's highest-exit-momentum shim demanded more dee voltage than could be promised AND produced a minimum in the radial dependence when the exciting current was reduced ("an objectionable feature"). The adopted compromise 3 in x 1/2 in shim with 25-in exit radius keeps a usable shape only over 13,900-15,000 gauss, with exit droop 1.2%-2.2% of center — i.e., a shim design is valid over a FIELD RANGE, not at a point.
Source, quote & tabletop applicability
with this shim design a reduction of the exciting current produced a minimum in the radial dependence, which is an objectionable feature.
Tabletop: 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.
-
Magnetic force on chamber walls inside the gap can dwarf atmospheric load — size the structure for it: UW's model study found the pull on the (mild steel) vacuum-tank cover plates exceeded 35 tons against 24 tons of atmospheric force. The same model incidentally measured stray field at the oscillator tube location, which sized the tube's magnetic shielding box.
UW 60-inch: magnetic pull on covers > 35 tons vs atmospheric 24 tonsSource, quote & tabletop applicability
the results indicated a force greater than 35 tons for the cyclotron magnet. For comparison the force of atmospheric pressure is 24 tons.
Tabletop: Any ferromagnetic chamber lid or pole-integrated cover on a tabletop machine sees magnetic clamping comparable to or exceeding vacuum load — check both cases (energized/de-energized) for deflection, and expect assembly/disassembly forces. Stray field at the RF tube/amplifier is likewise a real design input for a compact machine.
-
Verify the model's prediction on the full magnet before committing to shims: UW measured the unshimmed full-scale radial dependence first, found "close agreement" with the model, and only then cut cyclotron shims to the model design — after which "the predicted radial dependence was verified and the results were considered satisfactory." Prediction, cross-check, commit.
Source, quote & tabletop applicability
showed that the model data could be used as a basis of prediction with confidence.
Tabletop: 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.
-
Central spikes: a cone-topped cylinder at the magnet center (UW: 1.5-in radius, 1/4-in cylinder + 1/4-in cone height, essentially filling the available axial space) produces "a sharp increase in the induction at the center of gap without producing a minimum anywhere in the radial dependence" — adopted after University of California reported a remarkable beam-current increase on the 184-inch from such spikes. Even undersized spikes (largest possible was still below optimum) were judged worth installing.
Source, quote & tabletop applicability
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.
Tabletop: A central field bump gives axial focusing in the first turns, where small machines lose most of their beam. A machined center button is one of the cheapest beam-current experiments available to the reference machine or a next machine — the no-minimum constraint is the part that takes care.
-
Expect azimuthal asymmetry from a definite checklist of construction features, not from mystery: UW's list — (1) unsymmetric core (yoke) shape, (2) small asymmetric steel details: bolts securing cover-plate sections, screws holding the copper liners, the gap where a shim is relieved for water lines, (3) accidental asymmetries in construction and placing of the coils, (4) non-uniformities in the steel. Every item is a design decision someone made.
Source, quote & tabletop applicability
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 accomodate water lines
Tabletop: DIRECT — an H-frame yoke is item (1) by construction. Keep fasteners, liner screws, and cooling-line reliefs symmetric in the pole region, or place them where the survey says the beam doesn't care.
-
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 & tabletop applicability
this correction was made the criterion for final adjustment rather than reference to mechanical measurements.
Tabletop: DIRECT — thousandths of pole tilt are visible in a tabletop field survey and in beam behavior. Shim the measured field, not the dial indicator; calibrate shim sensitivity from the first iteration and extrapolate; and expect a floor because every local correction spreads.
-
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 & tabletop applicability
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.
Tabletop: Sets a realistic bar — a carefully shimmed iron magnet holds azimuthal variation to ~a few parts in 10^4 over the working radii, and the spec that matters is at ~80% radius, not at the pole edge.
-
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 and vertical scale, the whole rig raised by screws until the field lay parallel to a reference direction taken at the (very uniform) gap center. Verdict: max departure 0.5 in from the geometric midplane, accepted without direct correction; the later azimuthal shimming was symmetric about the midplane so it could not disturb the median surface.
Source, quote & tabletop applicability
an azimuthally symmetric field may still have a dish-shaped median surface.
Tabletop: DIRECT physics: a displaced/dished magnetic median plane steers the circulating beam into a dee lid at small gap heights. A tabletop analog of the dip needle (or vertical probe-pair difference) belongs in the survey plan; and keep deliberate shimming mirror-symmetric about the midplane unless correcting the median surface is the goal. Needle details PDF p.44, map Fig. 3.13 p.45.
-
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 & tabletop applicability
Aluminum was chosen over stainless steel because of its short half-life property.
Tabletop: DIRECT for any machine that will make neutrons: aluminum's activation products die in hours-days while stainless (Co-60 from cobalt traces) lives for years. Choose the beam-facing metal for the machine you hope it becomes, and TIG aluminum is proven UHV-adequate practice from 1951.
-
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 & tabletop applicability
Double gaskets with a pump-out space between the two gaskets are used wherever possible for making seals at the joints in the system.
Tabletop: 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 on any joint that gets opened often; the 1951 materials list maps to modern Buna-N/Viton.
-
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 & tabletop applicability
Initial testing of the system disclosed two leaks in welds, both of which were in stainless to mild steel joints.
Tabletop: DIRECT — stainless-to-mild transitions (and any dissimilar pair) crack and porosity-leak preferentially; put them where they can be reached for repair, or design them out with transition flanges and gaskets.
-
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 & tabletop applicability
Installation of the copper tank liners, R. F. loops and loop insulators approximately tripled the interior surface area
Tabletop: DIRECT: every liner, loop and insulator added to a chamber is outgassing area — expect the base pressure to track it. And a $20 variac experiment (heater power vs measured speed) is how to find a surplus diffusion pump's real optimum, exactly as done here.
-
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 & tabletop applicability
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.
Tabletop: The construction vocabulary (EHC copper skin, silver-soldered cooling, silver-plated RF joints, high-pressure sliding contacts) is exactly what a 5-13 kV LDMOS-driven dee upgrade needs; split-for-repair is cheap foresight at any scale. Same contact-pressure concern as the nyo-9683/ornl-2648 sliding-contact rules.
-
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 & tabletop applicability
the filament may be replaced without breaking the vacuum of the tank proper.
Tabletop: The reference machine's filament-change downtime is this exact problem, solved in 1951: a small gate-valved source lock plus an external sylphon/bellows positioner turns a half-day vent cycle into a minutes-long swap and adds live source alignment — high payoff on any filament-eating small machine. (The shuttered viewport is a free detail worth stealing.)
-
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 & tabletop applicability
upon considering the approximations necessarily made in this type of analysis, the figure of 150 kw maximum r-f power was selected.
Tabletop: 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/(2R_shunt)), then buy the amplifier with a 2-3x factor for the terms the lumped model misses. The Koeth Rutgers dee-voltage note is the same math on an 8-12 inch machine.
-
A two-dee system has two near-degenerate modes a few percent apart — design the oscillator coupling to select the push-pull one: in the zero mode the dees swing in phase (no accelerating gap voltage); in the pi mode they swing opposite and gap voltage doubles. UW chose a SELF-EXCITED grounded-grid oscillator with the plate loop coupled into one dee stem and the filament (cathode) loop into the other specifically because that topology "should be easiest to assure oscillation at the proper frequency with the dees operating 180 degrees out of phase" — mode selection built into the feedback path itself.
Source, quote & tabletop applicability
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.
Tabletop: For a one-dee-plus-dummy machine the mode problem collapses, but the principle stands for any driven system — verify which resonance the amplifier is locking to (a network analyzer sweep distinguishes the modes), because the wrong one accelerates nothing. Also this collection's second explicit SELF-EXCITED architecture choice (see ucrl-9435 rule on the self-excited-vs-MOPA tension).
-
Plan the multipactor climb-through at design time: UW knew "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 in a small self-excited "booster" oscillator, NOT coupled through the dee system, powerful enough to "raise the dee voltage up to a point where electron oscillations can no longer take place." The booster (a converted BC-677 radar transmitter, ~2 kW) is driven by a small oscillator at HALF the cyclotron frequency feeding it as a frequency-doubling power amplifier — so when the main oscillator takes over, its energy cannot couple back into the booster chain.
Source, quote & tabletop applicability
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.
Tabletop: The corpus's driven-start cure (mddc-1045 tickler; nyo-9359's catalog) as a 1951 DESIGN feature rather than a retrofit — including the elegant half-frequency/doubler isolation trick so the starter needs no 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 ~100-V multipactor band without foldback/protection tripping.
-
Model the RF system at quarter scale (4x frequency) before building it: UW's quarter-scale model of the entire resonant system validated the calculated line lengths ("sufficiently accurate") and needed only minor adjustments; measured model Q ~3500 with no special joint precautions — about half the full-scale expectation, as scaling predicts (Q ~ sqrt(scale) at fixed geometry). Calculated equivalent-circuit constants were treated as guides, with the report noting it is "sometimes desirable" to add capacitance at the tube in parallel with the interelectrode capacitance to make a practical stub line.
Source, quote & tabletop applicability
there are many uncertainties in the exact determination of the constants of the equivalent circuit ... the calculated values ... serve well as a guide
Tabletop: 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).
-
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 & tabletop applicability
the plate is operated at d-c ground potential so that no insulation is required in the water lines.
Tabletop: Solid-state amps moot the HV plumbing, but two transferable doctrines survive — pick the grounding scheme that keeps coolant out of the HV problem, and use source impedance (here transformer reactance) as passive inrush protection instead of active circuitry where a component's own rating allows it.
-
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 & tabletop applicability
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.
Tabletop: The capacitive-paddle dee voltmeter is the same instrument Koeth calibrated on the Rutgers 12-inch and the missing calibration on the reference machine's "~800 V nominal" — a soldered paddle + defined-gap probe + diode peak detector, calibrated once against a real HV probe, converts dee voltage from folklore to data. The saturable- reactor trick survives as the Hall-effect/isolated-shunt principle: never bring an HV node to the meter.
-
It is legitimate to delete a protective subsystem when a cheaper pair of provisions covers its function — but record the reasoning: 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 tube conditioning. Supply: 3-phase full-wave 869-B mercury-vapor bridge, induction-regulator tap control, 2-19 kV at up to 15 A.
Source, quote & tabletop applicability
On the basis of cost it was decided to omit this refinement.
Tabletop: The decision pattern (name the deleted protection, name the two things standing in for it, keep a commissioning-only resistor in the drawer) is directly reusable; contrast ucrl-9435, where the 88-inch — with 20x the stored energy — bought the full hard-tube-modulator protection instead. Scale decides.
-
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 & tabletop applicability
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.
Tabletop: DIRECT blueprint for a tabletop control panel or PLC: interlock- chain-ordered start, ready-light-with-reason indication (the diagnostic half most amateur panels omit), RF-enable as the terminal permissive, and a cooling run-on timer. Complements the ad-755510 interlock rules with the wiring-bookkeeping practice that keeps the system maintainable. Details pp.99, 107.
-
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 & tabletop applicability
Machining work will begin after the oscillator is operating and an internal beam produced.
Tabletop: The corpus's commissioning-order lesson (internal beam -> then extraction) stated as an explicit 1951 schedule decision. For a next machine, budget the probe and its lock as first-beam hardware and hold extraction hardware at the drawing stage until the field and RF are proven.
-
Deflector design choices from the UW study: shorten from 90 to 70 degrees (starting 60 degrees beyond the dee gap) for mechanical stability of the control mechanism; keep the deflector plate at RF GROUND and use the RF field between plate and grounded dee edge for deflection, supplementing with DC only when dee voltage runs below ~120 kV; phase analysis sets a floor — at least 80 kV dee-to-ground RF so ions "do not enter the region of decelerating phase at any time within the dees" (with ~34 kV of DC then needed); channel width remotely variable (1/4 to 1 in, 60 kV / 20 mA supply), widen for flux or narrow to a constant 0.90 cm for energy selectivity — expected spread ~1.5 MeV about 21 MeV, with the useful-intensity core ~1 MeV.
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 & tabletop applicability
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.
Tabletop: The RF-ground deflector-plate trick (steal the existing dee field, add DC only as a supplement) and the adjustable-channel flux-vs-resolution trade are scale-free ideas for any future extraction study on a next machine; the phase-floor analysis is the kind of computation this collection's deflector cluster (nyo-9360 etc.) expects before metal is cut.
-
Measure extracted beam power by direct charge collection, not calorimetry, when you have the choice: UW considered deducing beam power from target cooling-water temperature rise but preferred the insulated-probe current measurement — "the direct measurement is preferable since for appreciable water flow the temperature difference is very small" and harder to read accurately.
Source, quote & tabletop applicability
the direct measurement is preferable since for appreciable water flow the temperature difference is very small.
Tabletop: At nA-uA tabletop currents calorimetry is hopeless (uW-mW against watts of RF pickup) — the Faraday cup + electrometer choice the reference machine already made is the 1951 conclusion too. Calorimetry earns its place only at tens of watts of beam.
-
Construction cost structure of a university-built 60-inch, 1948-1951 (to April 15, 1951): total ~$642,000 excluding university overhead and staff salaries — buildings $225,000; machine materials and supplies $201,500; UW payroll $14,000; ONR contract $150,000; AEC contract $51,500. Buildings alone exceeded the machine's materials — and most machine labor was donated/institutional (Navy-supplied machine tools, supplier technical assistance "too numerous to mention").
Buildings $225k > machine materials $201.5k; visible payroll only $14k of $642kSource, quote & tabletop applicability
Total expenditures to date from all sources, excluding University of Washington overhead and staff salaries, has been $642,000.
Tabletop: Same cost anatomy the plan's budgeting already assumes: facility and infrastructure rival the machine, and the labor line is invisible because it is donated — the honest comparison for an educational-accelerator business is materials PLUS the labor a customer cannot donate. Corroborates the ornl-3540 cost-structure rules from the construction side.
-
Cyclotron RF differs from industrial RF in exactly three ways — design for all three from day one: (a) the resonator is a SPARKING load that delivers large energy into the electronics within each spark; (b) multipactoring, "common in the field of particle accelerators, rarely occurs in other industrial applications"; (c) large power must be tuned continuously over a wide frequency band. (a) drives protective circuitry and tube ruggedness; (b) drives start-up provisions; (c) intensifies parasitic and harmonic problems.
Source, quote & tabletop applicability
(b) the multipactoring problem, common in the field of particle accelerators, rarely occurs in other industrial applications
Tabletop: The checklist for adapting ANY industrial/ham RF gear (including an LDMOS pallet) 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).
-
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 band onset ~150 V-class gap voltage (secondary-emission threshold ~150 eV); resonance when transit time = T_rf/2Source, quote & tabletop applicability
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.
Tabletop: DIRECT — the ~100-150 V band is exactly where a small machine's dee voltage must pass on every start. Completes this collection's cure set with the DC SWEEP variant: mddc-1045 (bias + tickler), nyo-9359 (impulse), ucrl-64 (volume reduction + bias), aecu-1951 (booster drive-through). Same author lineage as ucrl-3153/3187.
-
Bake in a new dee system by letting it spark — by the hundred thousand: "This conditioning process is usually referred to as baking in the dee. 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." Each spark's energy (~4.5 J stored in the 88-inch resonator) vaporizes the whisker or inclusion that initiated it — sparking is the conditioning mechanism, not merely a failure mode.
Conditioning scale: ~10^5-10^6 sparks; stored energy 4.5 J (88-inch resonator)Source, quote & tabletop applicability
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.
Tabletop: DIRECT for the 5-13 kV dee upgrade: plan a conditioning campaign (auto-recycle protection makes it unattended) rather than interpreting early sparking as failure. A tabletop resonator stores millijoules, so conditioning is gentle — the count, not the violence, does the work. Corroborates the ornl-2648/nyo-9683 conditioning rules and quantifies them.
-
Every dee spark is a system-wide transient: the spark's discontinuity propagates through the RF system and "often causes a spark to occur within the oscillator tube," which can then divert the full dc supply as a power arc. So protection is layered by speed — at Berkeley: vacuum switches in the 3-phase 16.6-kV ac feed open in ~10 ms (installed so an ignitron crowbar COULD be added); a Federal D-50 hard-tube modulator in the dc line opens within ~10 us of a fault, and doubles as the dee-voltage regulator (removing rectifier ripple, ion-source noise, and beam-loading changes, to 0.1%); the dc anode cable is terminated in its characteristic impedance at the supply end so the protection transients themselves cannot ring; RC surge networks sit across the rectifier transformer and dc output.
Protection ladder: hard-tube series switch ~10 us; ac vacuum switches ~10 ms; (alternative: ignitron crowbar)Source, quote & tabletop applicability
In this service it will open the anode circuit within 10 usec of a fault.
Tabletop: The modern translation is exact: LDMOS drain supplies want a fast electronic disconnect (the hard-tube modulator's descendant), a slower breaker layer, snubbers, and a matched/terminated dc feed. The dual-use insight — the series regulator IS the fast protection switch — carries straight into a solid-state dee supply. Cross-check ornl-2403's protection chapter; Smith's is the self-excited counterpart.
-
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 — "In this type of system the resonator is the frequency-determining element of the system; hence it is called a self-excited oscillator" — and buys back MOPA's advantages piecewise: frequency accuracy via a servo trimmer + AFC to 10 ppm, amplitude stability via the hard-tube modulator regulating dee voltage to 0.1%, and mode/phase integrity by designing anode and grid circuits as very-high-SWR lines whose voltage phase is 0 or pi everywhere, so the grid stays 180 degrees out of phase with the anode across the whole 5.3-16.5 Mc band (price: <1% line loss). Goodman's ornl-2403 argues the MOPA route (external stable master oscillator + power amplifier) for control; Berkeley (this paper, ucrl-3153/3187) and UW (aecu-1951) chose self-excitation for guaranteed oscillation on the wanted mode with automatic frequency tracking of the resonator. BOTH are proven; the choice turns on whether your hard problem is control (MOPA) or startup/tracking (self-excited).
Source, quote & tabletop applicability
In this type of system the resonator is the frequency-determining element of the system; hence it is called a self-excited oscillator.
Tabletop: 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.
-
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 & tabletop applicability
At the maximum particle energy, the beam requires 60 kw of power.
Tabletop: The four-line budget is the right form at any scale — a tabletop version is watts of copper loss, ~zero stray-ion, uW of beam, and a misc line that is mostly coupling/radiation. The named "stray-ion loss at the center" term is a reminder that source gas load steals RF power — one more reason the reference machine's beam and RF problems interlock.
-
Kill parasitics on paper first: compute/measure the higher modes of the anode and grid circuits and ADJUST CIRCUIT ELEMENTS so that no mode coincides with a class-C plate-current harmonic anywhere in the tuning range. Harmonic content falls roughly as 1/n, so only the low harmonics (2nd, 3rd) can excite a mode destructively; the 88-inch verified mode placement on a quarter-scale RF model and reports the consequences of getting it wrong — destructive voltages at the grid vacuum insulator and reduced fundamental output.
Design constraint: f_mode(k) != n * f_osc for n = 2, 3 over the whole tuning range (harmonic amplitude ~ 1/n)Source, quote & tabletop applicability
The circuit elements of the rf system were adjusted so that the first two higher modes would not be excited by an oscillator harmonic.
Tabletop: DIRECT for a fixed-frequency machine: sweep the dee system to a few hundred MHz on a VNA, list the modes, and check none sits at 2f or 3f of the drive — if one does, detune it with a strap or stub BEFORE blaming the amplifier for instability. Same mode-vs-harmonic discipline as the msucp-9 and ornl-2648 lines.
-
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 & tabletop applicability
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.
Tabletop: The solid-state translation: LDMOS gates tolerate NO spark energy — the joule-absorbing ruggedness must move into the coupling network (series blocking, clamping, circulator/isolator) because it no longer lives inside the active device. Budget those parts as the modern "shield tees."
-
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 & tabletop applicability
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
Tabletop: DIRECT and cheap: a comparator on (dee pickup voltage vs forward power) with a ~1 s drop-and-retry turns dee sparks from session-enders into log entries, and is precisely the automation a conditioning campaign needs. The ratio form matters — absolute thresholds miss arcs that still draw full power.
-
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 & tabletop applicability
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.
Tabletop: A protection spec you cannot derive from electronics alone — the dwell time is chosen so each spark finishes cleaning the spot that caused it. For a tabletop supply: let a dee spark burn ~1 ms before the drop-and-retry, but trip amplifier-device faults as fast as the electronics allow. Two speeds, two purposes.
-
A cyclotron resonator is automatically its own RF shield — exploit it and mind the boundary: "the problem of stray rf radiation common to all industrial rf applications is automatically relieved somewhat by the fact that the resonator has to be vacuum-tight, automatically making it rf-tight," with the tube and external electronics seeing only relatively low RF. The 88-inch measured stray radiation under 10 uV/m at one mile — meeting FCC-class expectations by construction, with leakage dominated by whatever penetrates the vacuum wall (loops, probes, windows, lines).
Source, quote & tabletop applicability
the resonator has to be vacuum-tight, automatically making it rf-tight.
Tabletop: DIRECT and comforting for a residential machine: a metal chamber dee system radiates almost nothing — EMI escapes via feedthroughs, viewports and the amplifier side, so gasket those and shield the drive chain and the neighbors' radios stay quiet. (The same reasoning applies to viewport mesh in the fusor literature.)
-
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, grid bias -700 V from a 500-ohm grid resistance, driving power 3 kW, RF plate swing 14 kV peak / 130 A peak, RF grid voltage 2 kV peak, power output 319 kW — i.e., ~85% plate efficiency class-C, power gain ~100, and grid dissipation three orders below output. Any proposed oscillator/amplifier chain whose numbers sit far from such ratios deserves suspicion.
6949 max: 15 kV x 25 A in -> 319 kW out (~85% eff); drive 3 kW (gain ~100); bias -700 V @ 1.4 A gridSource, quote & tabletop applicability
Maximum operating conditions for the RCA 6949 for the 88-in. cyclotron
Tabletop: The ratio discipline transfers: a healthy class-C/E chain shows 70-90% final efficiency and 15-20 dB final-stage gain whether it is 319 kW of tube or 500 W of LDMOS — efficiency far below that in the reference machine's or a next machine's amplifier means mistuning, parasitics, or multipactor loading, not "small machines are just lossy."