Design Guide › level 2
Cyclotron design rules, level 2: first-order design
619 of the guide’s 1878 rules sit at level 2: first-order design — sizes the subsystems of any machine.
The level ranks how early and how universally a rule binds a cyclotron design — breadth,
never weight. It is not permission to skip a rule whose trigger a machine has, and safety
rules are never skippable on level alone; how the levels were assigned and audited is on
the methodology page. Each rule keeps its
formula where the source gives one, a verbatim quote, a page-level citation, and a stable
identifier (dg-NNNN) that resolves here, on its
subsystem page, and on the
all-in-one guide. Where an editorial note says “the
reference machine”, its parameters are on the
guide’s front page.
This level’s rules by subsystem — each link opens just that subset, in the all-in-one guide’s filters: Magnet (234) · RF (138) · Beam dynamics (134) · Dee (82) · Fabrication (77) · Ion source (68) · Coils (64) · Vacuum (63) · Safety (55) · Materials (36) · Cyclotron general (35) · Modeling (33) · Vacuum chamber (32) · Extraction (30) · Project management (27) · Beam measurement (26) · Shielding (20) · Detectors (14) · Targets (11) · Physics theory (9) · Seals (8) · Pedagogy (7) · RF matching (4) · Controls & instrumentation (2). A rule carrying several tags is counted under each; a subsystem’s complete rule set, across all levels, is on its own page in the subsystem directory. To add a search term or a second subsystem, open this level in the all-in-one guide with filters, which carries every rule and filters in the browser.
Verify before use. Every rule here is a source extract in the vocabulary of the editorial methodology — faithful to its cited page, not an independently validated engineering requirement. Re-read any rule that drives a real design decision at the cited page before committing metal, money, or high voltage to it. The editorial note under each quote is this site’s extrapolation to a tabletop machine, not something the source said: an editor’s judgement, audited for overreach, never a citation.
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Shape the field to fall smoothly with radius by a total of 3 to 4 percent (small machines with relatively high dee voltage and few turns) or ~2 percent (medium 15-20 MeV machines) from center to the exit radius - the quoted historical totals.
total radial field decrease: 3-4% (small cyclotrons), ~2% (15-20 MeV), ~1% (very large)Source quote & editorial note
the total decrease below the value of the central field out to the exit slit is about 2 per cent. The radial decrease can be larger (3 to 4 per cent) in small machines in which D voltage is relatively high.
Livingston & Blewett, Particle Accelerators (1962) — p. 161
Editorial note, tabletop extrapolation: The reference machine is the small, few-turn case the quote names, and the census machines converged on the same few-percent smooth droop (dg-702). Aim for a smooth 3-4%-class fall-off shaped against the machine's own n(r) requirement (dg-003), with the number as the historical anchor rather than the spec.
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MIT's measured weak-focusing profile: n(r) rises roughly linearly from 0 at center to ~0.02 where fringing begins, then rapidly to ~0.4 at the exit-slit radius and 1.0 just beyond; they placed the septum just inside the maximum-energy radius.
MIT: n = 0 -> 0.02 at r = 0.8*R_pole, 0.40 at exit slit (18.75 in), 1.0 at 19.25 inSource quote & editorial note
The n value rises almost linearly from zero at the center to 0.02 at 15 in. (where fringing effects start), then increases rapidly to 0.40 at 18.75 in. (exit-slit location) and to 1.0 at 19.25 in.
Livingston & Blewett, Particle Accelerators (1962) — p. 161-183
Editorial note, tabletop extrapolation: One documented profile, useful as a shape target rather than a scaling law: fringe onset and width depend on gap-to-pole ratio, edge shape and shims, so map n(r) on the actual 8-in poles (FEMM, then measurement) and place extraction where the MEASURED n has climbed toward ~0.4 - before the n = 1 radial-stability edge.
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Taper the poles so flux density stays roughly constant along their length; a designed 18 kG gap field needs a pole base about 24 percent larger in diameter to stay under ~20 kG in the iron.
42-in pole face at 18 kG -> ~52-in base; keep B_iron < ~20 kG (saturation)Source quote & editorial note
For a designed flux density of 18 kilogauss in the gap of a 42-in. cyclotron ... the pole base would have to be about 52 in. in diameter to keep flux density in the base of the pole below the practical limit.
Livingston & Blewett, Particle Accelerators (1962) — p. 193
Editorial note, tabletop extrapolation: At 5.9 kG straight cylindrical poles are fine on the reference machine; taper starts paying when the LOCAL flux in the pole approaches the steel's knee - a FEMM check, not a gap-field threshold. The source's worked case is the calibration: an 18 kG gap wanted a base about 24% larger in diameter.
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Size the magnet gap around 1/8 of pole diameter when energy matters (5-6 in gaps on 42-in poles, 8-9 in on 60-in); excitation power grows roughly as gap length squared and a wider gap loses usable radius to fringing.
g/D_pole ~ 0.12-0.14; magnet power ~ g^2Source quote & editorial note
the longer the magnet gap the larger is the power required for excitation, varying approximately with the square of gap length ... use of 5- to 6-in. gaps for 42-in. poles and 8- to 9-in. gaps for 60-in. poles.
Livingston & Blewett, Particle Accelerators (1962) — p. 194
Editorial note, tabletop extrapolation: On 8-in poles the historical ratio suggests a ~1-inch-class gap as a starting point - at tabletop scale the RF structure, chamber walls and fringe-vs-radius scaling often force it larger, so treat the ratio as the iron-economy pull in a trade the other subsystems get votes in (dg-163). Every extra gap costs amp-turns (power ~ g^2) and usable radius.
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Regulate magnet current to better than 1 part in 1000 (sense a series standard resistor against a voltage reference and feed back); a drifting field detunes resonance before anything else does.
dI/I < 1e-3Source quote & editorial note
The magnet field must be accurately regulated to maintain a steady beam ... A constant-current regulator is needed, capable of reducing fluctuations to better than 1/1000.
Livingston & Blewett, Particle Accelerators (1962) — p. 194
Editorial note, tabletop extrapolation: A modern current-regulated supply can meet this - verify ripple AND thermal drift on the actual unit: 0.1% of 5.9 kG is 6 G, a shift of the same order as deliberate shim corrections, so supply drift competes with the shim budget (and with RF detuning) for the resonance.
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The gap field follows B = mu0*Ni/g while the iron is well below saturation; at higher excitation the observed field falls short of the ideal - Livingston & Blewett's example delivered 0.73 of the prediction at 18 kilogauss - as iron reluctance and leakage grow.
B = K*mu0*Ni/g; K -> 1 at low excitation, measured 0.73 at 18 kG on their magnet; 10 kG across a 10 cm gap: 7.95e4 A-turns idealSource quote & editorial note
To produce a field B of 1 weber/m2 (10 kilogauss) in a gap of 10 cm length, the number of ampere-turns required is 7.95 x 10^4 ... At 18 kilogauss ... the observed value of B is 0.73 of that predicted.
Livingston & Blewett, Particle Accelerators (1962) — p. 258-260
Editorial note, tabletop extrapolation: At the reference machine's 5.9 kG the ideal formula is a good first estimate (~1.7e4 ampere-turns across its 3.6 cm gap) before iron reluctance and leakage add their share - FEMM closes that gap. Field headroom is cheap while the iron stays unsaturated and expensive after; where the knee sits is a property of the specific circuit, not a universal 10 kG line.
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Expect the usable field to end about half a gap-length inside the pole edge - the quoted offsets: 0.6g without shims, 0.45g with the chosen ring-shaped shims (what threshold defines 'usable', and the high-field behavior, are the book's context: scan re-read queued).
R_useful ~= R_pole - (0.45 to 0.6)*g; boundary moves inward at high B due to pole-corner saturationSource quote & editorial note
the edge of the usable region is inside the pole boundaries by about one-half the gap length ... Without shims the useful region was inside the pole edge by 0.6g; with the chosen ring-shaped shims it was inside by 0.45g.
Livingston & Blewett, Particle Accelerators (1962) — p. 260
Editorial note, tabletop extrapolation: With its 1.42-in gap on 8-in poles the builder loses ~0.85 in of radius to fringing; shrinking the gap or adding ring shims recovers usable radius.
Cited in: Cyclotron Magnet Design
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Shrinking the pole gap raises the field at fixed excitation: the source expected reducing the gap from 3.8 cm to 1.3 cm to lift the same magnet from ~0.49 T to ~0.75 T - well short of the ideal inverse-gap prediction (~1.4 T), because leakage, iron reluctance, and (here) the permanent magnets' operating point all move with the gap; energy gain is quadratic in B, so gap reductions still pay twice.
ideal B ~ 1/g at fixed MMF is an upper bound (the source's own numbers deliver ~55% of it); T_final ~ B^2Source quote & editorial note
we will reduce the air gap between the poles of the magnet to 1.3 cm thereby increasing the magnetic field to roughly 0.75 T.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 22
Editorial note, tabletop extrapolation: The cheapest field upgrade for a next machine is gap reduction - thinner chamber lids, pole pieces reaching into the chamber - before any coil or steel changes. Model the actual gain in FEMM rather than assuming 1/g.
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Expect the 1%-uniform region of a flat-pole magnet to end well inside the pole radius - the measured case: 0.493 T uniform to 1% out to 6.19 cm on 7.6 cm radius poles, about 80% - and note the quoted geometry: their RF electrode at 7.14 cm CONTAINED the full uniform region, keeping acceleration inside it.
r_uniform(1%) ~ 0.8 * r_poleSource quote & editorial note
The magnetic field is uniform at 0.493 T, to within one percent, out to a radius of 6.19 cm... The RF electrode radius is 7.14 cm containing the full uniform region.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 22-23
Editorial note, tabletop extrapolation: Suggests planning the reference machine's usable beam radius around ~80% of the 8-in pole (~3.2 in) unless shims extend the flat region - with the machine's own field map as the arbiter (dg-098, dg-638).
Cited in: Cyclotron Magnet Design
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Characterize a repurposed electromagnet from its field-versus-gap curve before designing around it: the Varian V-3900 NMR magnet gives 2.7 T at a 1.25-inch gap, which at a 7.5 cm usable extraction radius yields E = q^2*B^2*r^2/(2m) ~ 1.96 MeV protons (the thesis's figure - usable radius, not the full 8 cm pole radius, goes in the formula).
KE = q^2*B^2*r^2/(2m); 2.7 T, r=0.075 m -> 1.96 MeVSource quote & editorial note
the magnet generates 2.7 T of magnetic field with a 1.25 inch pole separation... capable of accelerating protons to a maximum kinetic energy of 1.96 MeV
Editorial note, tabletop extrapolation: The surplus-NMR-magnet route to MeV energies: small radius is fully compensated by high B (energy ~ B^2*r^2), so a 6-inch 2.7 T machine beats a 12-inch 1 T machine.
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Plan roughly 20 kW of DC coil power - water-cooled hollow copper tubing on a 2-ton mild-steel core, 33-inch-diameter coils, poles tapered from 12-inch stems to 10-inch faces, 17,000 gauss - as the Iowa State 1.5 MeV undergraduate cyclotron's magnet budget. [2026-09-06 re-read note: the paper gives no pole-gap figure anywhere - its only gap dimensions are the dee gap (1.5 cm) and dee height (2.4 cm), and Figure 5 is explicitly not to scale.]
20 kW dc into water-cooled hollow-copper coils; 33 in coil diameter; 2-ton mild-steel core (Iowa State 1.5 MeV machine)Source quote & editorial note
The magnet consists of coils of hollow copper tubing wound on a two-ton core of mild steel. ... capable of producing a very uniform 17,000 gauss field ... tapered from 12-inch pole stems to 10-inch pole faces.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. PDF 7 (printed 479) carries the quoted 20 kW sentence; the magnet paragraph is on PDF 5 (printed 477) and Table 1 on PDF 9 (printed 481)
Editorial note, tabletop extrapolation: Sets the scale of the jump from the reference machine's 0.59 T solid-tubing magnet toward a 1.5-1.7 T machine: at multi-kilowatt dissipation, hollow conductor with water flow is the usual regime (dg-092). The exact power for a next machine depends on its actual gap, field and copper budget - the magnet-power calculator sizes it, this precedent scales it.
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A workable student-cyclotron design point for ~1.5 MeV protons: 10-inch pole faces, 17,000 gauss, 25.68 MHz RF, 10-14 kV dee-to-dee at 2 kW RF, giving 2 uA of beam (about 1.3e13 protons/s).
10 in poles, 1.7 T, 25.68 MHz, Vdee 10-14 kV, 2 kW RF, 2 uA, 1.5 MeVSource quote & editorial note
Size: 10-inch pole diameter ... Dee voltage: 10,000 to 14,000 volts dee-to-dee; R.F. power: 2,000 watts; R.F. frequency: 25.68 megacycles ... Magnetic field strength: 17,000 gauss
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 9
Editorial note, tabletop extrapolation: The closest historical analogue to a next machine's target: same pole diameter as the reference machine, and the ~3x field buys the ~10x energy (E ~ B^2*r^2 at fixed radius). The ~10x dee voltage buys turn count, phase margin and beam survival at that field - not the energy ceiling itself.
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Regulate magnet current, not field, with a precision shunt feeding a difference amplifier against a voltage reference: this system held 17,000 gauss to +/-4 gauss (2.4e-4) - the stability that machine ran at.
+/-4 G on 17,000 G = 2.4e-4 stabilitySource quote & editorial note
This regulation system is capable of holding the 17,000 gauss field to within +/-4 gauss of its nominal value.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 9
Editorial note, tabletop extrapolation: A concrete precedent for a home magnet supply: a few parts in 1e4 is achievable with a shunt, op-amp and pass bank. What a given machine NEEDS follows from its turn count and phase budget (dg-273); this figure is the documented professional practice, not the requirement.
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Use low-carbon soft iron for all flux-path parts: the ANL forgings ran C 0.12%, Si 0.17%, P 0.014%, S 0.024%, Mn 0.39% - the low-carbon end of the steel range is the standard magnet choice, with carbon the most-watched impurity.
C ~ 0.12% (low-carbon steel, 1010-1020 class or better)Source quote & editorial note
The magnet yoke, poles and tips, acceleration chamber lids, and shims are of soft iron forgings with the impurity analysis as follows: Carbon 0.12%...
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 11
Editorial note, tabletop extrapolation: A concrete spec to hand a supplier: 1010/1018-class low-carbon steel serves for a next machine's yoke stock; for pole tips avoid high-carbon or unknown scrap - and remember silicon and processing also move the curve, which is what measuring your own stock settles (dg-1330).
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Size the yoke return-path (arm) cross-section larger than the pole so the arms run below pole flux density and never saturate first: the source increased arm area by 25% and quotes the arm flux density as 1.2 T against the 1.6 T maximum (nominally 1.6/1.25 = 1.28 T - their 1.2 T is rounded or carries extra margin).
A_arm > A_pole; source: +25% area, quoted arm density 1.2 T vs 1.6 T pole (exact ratio 1/1.25 = 0.80)Source quote & editorial note
the arms of the yoke carry a 25% smaller flux density than the maximum: only 1.2 T. This is achieved by increasing their cross-sectional area by 25%.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 29
Editorial note, tabletop extrapolation: A ready sizing pattern for a next machine's H-frame: make every return-path section 25-33% larger in area than the pole face (33% if the goal is a genuine 25% density reduction), and check the narrowest section - that is the one that saturates first (dg-037).
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Expect and accept roughly 4-5% total field droop from center to full dee radius (1.64 T -> 1.57 T at 6 in) in a weak-focusing design; verify with a magnetostatic code like Poisson Superfish.
dB ~ 0.08 T droop over 6 in radius at 1.6 T (~5%)Source quote & editorial note
at a dee radius of 6'' the field is 1.57 T, a .08 T drop off from 1.64 T directly at the center.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 31
Editorial note, tabletop extrapolation: One machine's by-design droop as a sanity anchor: a few percent total is the common class (dg-702's census clustering). What YOUR field may droop is set by the phase-slip budget and the n(r) requirement - verify with Poisson/FEMM against those, not against 5%.
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Size the coil from NI = B*g/mu0 as the first cut: 1.6 T across their 2.13-in gap computes to ~69 kA-turns, and they built 720 turns at 110 A (~79 kA-turns) - roughly 15% above the ideal figure, margin that real iron reluctance and leakage consume.
NI = B*g/mu0 (ideal gap-only first cut); their example: 68.9 kA-turns ideal, 79.2 kA-turns builtSource quote & editorial note
we used the basic equation for an electromagnet... we decided a 2.13'' gap a reasonable size... we then concluded that we needed 720 turns to reach 1.6T.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 32
Editorial note, tabletop extrapolation: The same sizing equation the reference machine's magnet obeys (its 538 turns are that build's own number, not this source's). The gap-only formula is the floor; the source's ~15% surplus is a realistic allowance for what it omits, and FEMM confirms the actual requirement (dg-016).
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Use the permeance (magnetic Ohm's law) method for permanent-magnet circuits: judiciously divide external space into standard flux paths and sum permeances - total flux estimates come out within ~2% of computation, though local flux density may only be good to ~30%.
Phi = F * P_total; total-flux accuracy ~2%, local B ~30%Source quote & editorial note
agreement to within less than two percent. In contrast, calculations of the flux density at Point G yield 0.39 T for the analogue method and 0.30 T for the computer
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 10-11
Editorial note, tabletop extrapolation: If a next machine uses NdFeB anywhere (source magnets, the PM cyclotron study), the permeance method sizes gap flux without FEA - trusted for totals and not point fields, per the source's own one-circuit comparison (2% total-flux vs 30% local). Check the final design in FEA regardless.
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Open (non-enclosed) permanent-magnet field sources can be made when the required gap field is less than about half the material remanence - the source's feasibility condition for axially finite cavities. Above that, flux confinement (cladding, a closed yoke) or an optimized geometry (Halbach-class arrays) is what buys more.
B_gap (simple open source) <~ Br/2 - a sufficient-condition screen, not a hard ceilingSource quote & editorial note
If the required fields are less than about half the remanence, open compact sources for fields in axially finite cavities can be made
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 33
Editorial note, tabletop extrapolation: Quick feasibility screen: with Br ~ 1.3 T NdFeB, a simple open PM assembly reaches 0.6 T-class gap fields - marginal at the reference machine's field. Beyond it the answer is confinement or Halbach-class geometry, not impossibility.
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Prefer rare-earth magnets (NdFeB, Br/B0c ~ 1.05, near-linear demagnetization) over alnico: an REPM has one circuit-independent mmf, while an alnico's operating point walks down minor loops whenever the gap is widened or the magnet removed, permanently losing strength.
Source quote & editorial note
no unique mmf can be assigned to a conventional permanent magnet... the magnet mmf will always be that corresponding to the lowest point on the demagnetization curve reached
Leupold & Potenziani, A Permanent Magnet Circuit Design Primer — ARL-TR-946 (1996) — p. 8-10
Editorial note, tabletop extrapolation: Practical warning with the mechanism stated right: an alnico circuit loses strength when opening the gap drives it to a NEW lowest point on its demagnetization curve - the first excursion does the damage; repeating the same excursion mostly retraces the established minor loop - but every deeper excursion (magnet fully removed, steel tools across the gap) ratchets it further down. NdFeB's near-linear curve tolerates gap changes reversibly.
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For a permanent-magnet cyclotron the required PM material volume depends only on particle energy, gap height and PM working point - not on pole radius or average field - via the energy-product relation (required volume scales as (Bg*R)^2 at fixed gap), with the PM working hardest at its maximum-energy-product point.
Bg^2 ~ mu0*Bm*|Hm|*Vm/Vg (ideal); optimum working point: Bm = Br/2 and mu0*|Hm| = Br/2 on a linear demagnetization lineSource quote & editorial note
required volume of PM material depends only on particle energy, magnet gap and PM working point and doesn't depend on pole radius or average magnetic field value.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 1
Editorial note, tabletop extrapolation: Scaling law that makes a permanent-magnet follow-on build thinkable: at ~1 MeV and a 2 cm gap the required NdFeB volume is a few percent of the 1 ton needed for 10 MeV.
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Take average field as high as iron saturation allows to minimize magnet size, then split it into strong hills and weak valleys for focusing: 1.4 T average from 2.3 T hills and 0.5 T valleys in a classical 4-sector, 45-degree geometry.
<B> 1.4 T = 2.3 T hill / 0.5 T valley, 4 sectors of 45 deg, PM magnetization 1.23 T, pole dia 750 mm for 10 MeVSource quote & editorial note
To minimize weight and size of magnet system the average magnetic field value has to be high, limited by iron saturation ... average magnetic field value was chosen as 1.4 T provided of 2.3 T and 0.5 T of hill and valley region fields
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 1
Editorial note, tabletop extrapolation: A worked AVF datapoint, not a scaling law: hill/valley ratio, sector count and sector angle set flutter and tunes in a geometry-dependent way, so an 8-12 inch pole set re-derives them (FEMM plus a tune calculation) rather than copying 4.6:1 and 45 degrees. What does transfer is the design order: average field as high as iron saturation allows, then focusing from the hill/valley split - iron, not coil power, is the ceiling on a PM machine.
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Choose the hill gap from beam intensity requirements and let the valley gap follow at about 5x that: 20 mm hill gap with a 100 mm valley gap for a 10 MeV PET cyclotron.
hill gap 20 mm, valley gap 100 mm (5:1)Source quote & editorial note
As hill gap providing enough beam intensity was chosen as 20 mm and then corresponding valley gap is 100 mm.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 1
Editorial note, tabletop extrapolation: One worked ratio for a first AVF pole-tip sketch: hill gap from beam-aperture needs, valley several times deeper - re-derived for the actual field contrast and the RF/pumping geometry rather than copied. A deep valley is indeed where an amateur's Dee and pumping naturally live.
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Expect analytic/3-D calculations of average field to run a few per cent optimistic: measurement came out 5% below calculation, and the fix was reducing the valley gap from 100 mm to 70 mm while still fitting the RF cavity.
calculated <B> 5% above measured; valley gap 100 mm -> 70 mm to recover design fieldSource quote & editorial note
disagreement with calculation was found as the calculation average field value is 5 % higher than measured one ... the valley gap height was reduced from 100 mm to 70 mm
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 2
Editorial note, tabletop extrapolation: Design in adjustability - a gap or shim you can still reduce after measuring - because model-to-measurement discrepancies at the percent scale happen in either direction (this source's ran 5% optimistic). Adjustability is cheap before assembly and expensive after.
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For permanent-magnet designs, allow for a gap-field temperature coefficient of about -0.07%/degC - measured on the source machine and judged acceptable there for normal cyclotron work.
dB/B ~ -0.07%/degC (measured, PM machine)Source quote & editorial note
The temperature coefficient of gap magnetic field was measured as about -0.07%/0C. Such coefficient is acceptable for normal work of cyclotron.
Antokhin et al., Magnet System for PET Cyclotron Based on Permanent Magnets (2006) — p. 2
Editorial note, tabletop extrapolation: A PM cyclotron in an unheated garage will drift off resonance with the seasons: from the quoted coefficient, a 10 degC swing is a 0.7% field change - orders of magnitude larger than the stability regulated professional machines hold (the dg-027 machine held +/-2.4 parts in 10^4).
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Dipole excitation per gap is NI = B*g/mu0, valid when iron path reluctance lambda/mu is negligible versus the gap; the exact form B_air = mu0*NI/(g + lambda/mu) shows when iron nearing saturation starts stealing amp-turns.
B_air = mu0*NI/(g + lambda/mu) ~ mu0*NI/gSource quote & editorial note
Bair = mu0 NI / (g + lambda/mu); ... Approximation ignoring iron reluctance (lambda/mu << g): NI = B g /mu0
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 25
Editorial note, tabletop extrapolation: The correction term is one contributor that bends the excitation curve at high current: comparing measured B-vs-I against the lumped formula flags when the iron starts stealing amp-turns - attributing the bend among saturation, leakage and fringing then belongs to FEMM, which the lumped model cannot do.
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Choose yoke topology by trade-off, per the lecture's comparison: C-core gives easy access but needs pole shims and is less rigid; H-core is symmetric and rigid but still shimmed; window-frame - the quoted row - has high field quality, no pole shim, symmetry and rigidity, at the price of major access problems (the C/H rows are the same slide set: scan re-read queued).
Source quote & editorial note
'Window Frame' Advantages: High quality field; No pole shim; Symmetric & rigid; Disadvantages: Major access problems.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 29, 31
Editorial note, tabletop extrapolation: Confirms the reference machine's H-frame as the right middle choice for a cyclotron (needs chamber access on both sides), with shimming accepted as part of the deal.
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Estimate magnet stored energy as U = B^2/(2*mu0) * (gap volume) and coil inductance as L_coil = 2U/I^2; the ramping voltage needed is V ~ B0*N*a*L/dt with L the magnet length (the source's own symbol), so turn count N is the only free knob for matching a power supply once field, gap, and ramp time are fixed.
U = B^2/(2*mu0)*V_gap; L_coil = 2U/I^2; V = B0*N*a*L/dt + I*R (a = pole width, L = magnet length)Source quote & editorial note
Given the field = B0, pole width = a, Magnet Length = L and ramp time dt, the only design option available for changing the voltage is the number of turns, N.
Editorial note, tabletop extrapolation: Quick check on a next machine's supply matching: stored energy in a 10-inch, 1 T, 5 cm gap magnet is about 1 kJ from the gap alone (B^2/(2*mu0) x volume; fringe fields add more), and turn count trades current for voltage against whatever surplus supply the builder finds.
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Use the free, LANL-maintained POISSON/PANDIRA/AUTOMESH/WFSPLOT chain for 2-D magnet cross-sections - the lecture's tour: AUTOMESH builds the mesh from a text file, POISSON relaxes the vector potential (PANDIRA for permanent-magnet and anisotropic problems), WFSPLOT draws geometry and equipotentials (component details per the lecture: scan re-read queued).
workflow: .am text file -> AUTOMESH -> Tape35 -> POISSON or PANDIRA -> WFSPLOT / OUTPOISource quote & editorial note
It is a public access code (it's free), maintained under contract with DOE by Los Alamos National Accelerator Laboratory (LANL) personnel.
Editorial note, tabletop extrapolation: Free tooling that runs on a PC, in the same code family the Houghton-line theses used (dg-142) - the standard amateur path to pole-profile design alongside FEMM.
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Compute dipole excitation as NI = B*h/mu0 divided by an efficiency of about 0.98 - a well-designed iron yoke eats only ~2% of the MMF.
NI = B0*h/(mu0*eta), eta ~ 0.98Source quote & editorial note
efficiency ~ 0.98 For magnets with well designed yokes.
Tanabe, Iron Dominated Electromagnets, Lecture 6: Excitation, Coil Design, System Design and Water Flow (2005) — p. 4-6, 12
Editorial note, tabletop extrapolation: Lets the builder size a next machine's amp-turns by hand before any FEA - with the ~2% read correctly: it is the yoke's MMF consumption in a well-designed magnet, not the accuracy of the estimate. Saturation, the real B-H curve, leakage and geometry can move the answer by far more than 2%, which is what the FEMM pass is for.
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For a DC magnet with a simple flat pole contour, a solid machined core is appropriate; choose laminations only for time-varying fields or when magnet-to-magnet reproducibility across a family matters (lamination economics: ~$50k die set, ~$1/lamination, 2-4 man-days stacking per core).
die set ~50 k$; ~$1/lamination; 2-4 man-days/core assemblySource quote & editorial note
Solid iron yokes are often used in simple, flat pole contour magnets.
Editorial note, tabletop extrapolation: Settles the default for a next machine: a one-off DC cyclotron magnet is normally solid steel - the source's 'often used' practice - because lamination tooling only pays across a production family. Laminations re-enter if the design ramps or regulates fast enough for eddy currents to matter (dg-089).
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Iron B-H properties vary with chemistry from heat to heat, carbon dominating - the quote; the lecture's practical corollaries (variation with position in the pour and rolling direction; ordering non-oriented steel; same-heat purchasing) accompany it in its discussion (scan re-read queued).
Source quote & editorial note
The BH characteristics of iron are variable and depend on the chemistry of the iron (dominated by the Carbon content, which is highly variable from heat to heat).
Editorial note, tabletop extrapolation: Practical purchasing rule: buy a next machine's pole and yoke stock as one lot from one heat where possible - and treat mixed-source top/bottom iron as a candidate cause if the median plane comes out asymmetric (a dg-138-class symptom).
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Choose the pole gap as a compromise: a small gap cuts the ampere-turns and lets orbits run close to the pole edge, while a large gap buys space for ion source, probes, and easier vacuum pumping at the price of field and power.
Source quote & editorial note
small gap: reduced number of At of coils, pole radius reduced, orbits close to outer edge; large gap: large space: injection, extraction, probes, easier vacuum pumping
Zaremba, Magnets for Cyclotrons (2005) — p. 22
Editorial note, tabletop extrapolation: Frames the central tradeoff for a next machine: shrinking the gap raises B at fixed ampere-turns while the iron stays unsaturated (dg-021's measured case shows the ideal 1/g is an upper bound) - and everything (dee aperture, ion source, probes) must still fit and pump through the smaller gap.
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Before freezing magnet geometry, check the design against every subsystem it must host: RF system, vacuum pumping, ion source/injection, extraction or internal target, and diagnostic probes.
Source quote & editorial note
Cyclotron magnet design should always consider interaction with subsystems: RF system, vacuum pumping, ion source or injection system, extraction system or internal target, diagnostic probes.
Zaremba, Magnets for Cyclotrons (2005) — p. 3, 45
Editorial note, tabletop extrapolation: A magnet that works but leaves no port for the probe or the pump is a classic amateur trap - exactly what this five-item checklist exists to prevent; run it on every layout iteration for a next machine.
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Do first-pass cyclotron magnet numbers analytically with the lecture's formula set: average field <B> = alpha*B_hill + (1-alpha)*B_valley (alpha = pole azimuthal fraction), flutter F = alpha(1-alpha)(B_hill-B_valley)^2/<B>^2, total flux Phi = B_hill*S_poles (a hard-edge estimate that neglects the valley contribution), NI from Ampere's law, and coil cooling dT(C) = 60*P(kW)/(4.19*N(l/min)).
dT(C) = 60*P(kW)/(4.19*N(l/min)); F = alpha(1-alpha)(Bh-Bv)^2/<B>^2Source quote & editorial note
coil cooling estimation: dT(C) = 60*P(kW)/(4.19*N(l/min))
Zaremba, Magnets for Cyclotrons (2005) — p. 30-32
Editorial note, tabletop extrapolation: The cooling formula is immediately usable: a next machine's 5 kW coil at 4 L/min runs ~18 C water rise; the flutter formulas matter only if the builder adds sector (AVF) pole faces.
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If using sectored (AVF) poles, a hill fraction k = 0.5 gives best RF efficiency (most valley room for dees); increase toward k ~ 0.67 (60-degree hills) only to shrink machine diameter, and design to a vertical tune around nu_z ~ 0.2.
k = hill angle/period; k=0.5 best for RF, IBA chose k=0.67, nu_z ~ 0.2Source quote & editorial note
For best RF efficiency, k=0.5 BUT to decrease machine dimensions k >0.5 (more hill, thus more field) CHOICE : k=0.67 (60 deg hills)... CHOICE : nu_z = 0.2
Zaremba, Magnets for Cyclotrons (2005) — p. 32-33
Editorial note, tabletop extrapolation: If a next machine goes AVF to escape the weak-focusing energy ceiling, IBA's documented choices are a starting point, not proven tabletop values: k between 0.5 (best RF room) and 0.67 (compactness), and a modest vertical-tune target like their nu_z = 0.2 - each re-derived for the actual geometry, since a 60-degree hill only gives k = 0.67 in their sector periodicity, and sector count and valley usage carry their own trades.
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Follow the iterative magnet design loop: rough model, hand calculations, 2-D field code, then 3-D field code - and a good 3-D model agreed with measurement to better than 3% in the source's experience.
3-D calculation vs measurement < 3%Source quote & editorial note
calculation results and measurements differ less than 3 percent
Zaremba, Magnets for Cyclotrons (2005) — p. 4, 35
Editorial note, tabletop extrapolation: The reference machine's Poisson/FEMM workflow is the professional one. Treat ~3% as the achievable-agreement benchmark rather than a diagnostic razor: a larger mismatch means something is wrong - model geometry or BH data, but equally possibly Hall-probe calibration, positioning, excitation error, or remanence - so check the measurement chain alongside the model before rebuilding either.
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Build the aperture budget as: good field region + vacuum chamber wall (0.3-2 mm) + installation/alignment margin (0-5 mm), with the paper allowing a further 5-10 mm within the good field region for closed-orbit distortion.
aperture = GFR + chamber wall (0.3-2 mm) + margin (0-5 mm); GFR includes 5-10 mm closed-orbit allowanceSource quote & editorial note
The total required aperture size is the sum of the good field region, the vacuum chamber thickness (0.3-2 mm) and a margin for installation and alignment (0-5 mm).
Editorial note, tabletop extrapolation: Explains why the pole gap exceeds the chamber's internal height by several millimetres once walls and margins stack - sum the budget's terms in a consistent full-gap or half-gap convention rather than quoting a round figure, since mixing conventions double-counts the allowances.
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Compute the required excitation directly from the gap: NI per pole = B*h/(2*eta*mu0), with efficiency eta typically 99% for a well-designed iron circuit - pole area does not enter the ideal term - and the source's own warning kept: the equation is approximate, neglecting fringe fields and iron saturation.
NI_per_pole = B*h/(2*eta*mu0); eta ~ 0.99; mu0 = 4*pi*1e-7Source quote & editorial note
where h is the magnet gap height in [m] ... eta is the efficiency (typically 99%), mu_0 is the permeability of free space ... Note that Eq. (5) is only approximate and neglects fringe fields and iron saturation.
Editorial note, tabletop extrapolation: First-cut sizing for a next machine: at a 2 cm gap and 1.0 T, ~8000 A-turns per pole sets conductor and current-density scale before any FEMM run - the floor that FEMM then corrects for fringe and saturation.
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Size the iron so flux density in the yoke stays below 1.5 T and yoke reluctance stays a small fraction (about 1%) of gap reluctance - with areas in the comparison, R_iron/R_gap = [lambda/(mu_r*A_iron)] / [h/A_gap] - and circuit efficiency exceeds 99% in the source's practice.
B_iron < 1.5 T; lambda/(mu_r*A_iron) << h/A_gap (the source's length-only form assumes comparable areas); eta > 99% when both holdSource quote & editorial note
It is good practice to keep the iron yoke reluctance smaller than a few per cent of air reluctance ... such that the magnetic flux in the iron remains smaller than 1.5 T ... the efficiency is better than 99%.
Editorial note, tabletop extrapolation: The single most useful yoke-sizing rule for an H-frame homebuilt magnet: pick return-leg area with margin beyond flux/1.5 T - equality puts the iron AT the 1.5 T line, not under it - and verify the narrowest return section in FEMM, because that section sets the circuit's behavior.
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Approximate the magnetic (effective) length as l_mag = l_iron + 2*h*k with k between 0.3 and 0.6 - and, per the quote, a precise k comes only from measurement or numerical calculation; the lecture's qualitative guidance on when k shrinks (narrow poles, saturation, close coil heads) accompanies the formula (scan re-read queued).
l_mag = l_iron + 2 h k, k = 0.3-0.6Source quote & editorial note
l_mag = l_iron + 2hk ... Typical values of k are between 0.3 and 0.6. A precise determination of k is only possible with measurements or numerical calculations.
Editorial note, tabletop extrapolation: Quantifies the fringe-field bulge at the pole edge - the region where a tabletop cyclotron's outermost orbits actually live.
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Estimate the total flux the return yoke must carry as Phi = B_gap * (w + 2h) * l_mag, where w is pole width and h the gap - i.e. add one gap-height of stray flux on each side of the pole.
Phi ~= B_gap (w + 2h) l_magSource quote & editorial note
Total flux in the return yoke is Phi = integral B da ~= B_gap (w + 2h) l_mag ... where h is the gap height and w the pole width.
Editorial note, tabletop extrapolation: For an 8-inch pole with a 1-inch gap this says design the yoke for ~25% more flux than the naive pole-area estimate.
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Estimate stored energy (hence inductance L = 2U/I^2 and supply voltage) for a simple gap magnet as U = B^2/(2mu0) * (V_gap + 2*V_coil/6 + V_yoke/mu_r).
U_magnet = B^2/(2 mu0)*(V_gap + 2*V_coil/6 + V_yoke/mu_r); energy-equivalent L = 2U/I^2 (valid for a near-linear circuit - near saturation the ramp voltage follows d(flux linkage)/dt, not this L); V_tot = R*I + L*dI/dtSource quote & editorial note
U_magnet = U_gap + 2 U_coil + U_yoke = B^2/(2 mu_0) (V_gap + 2 V_coil/6 + (1/mu_r) V_yoke)
Editorial note, tabletop extrapolation: Tells you the inductance scale and therefore how fast a bench supply can ramp the magnet and how big the flyback/dump protection must be (dg-218) - computing the protection against the worst-case inductance across the operating range, not the single linear figure.
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Choose magnet topology by field quality, per the lecture: the window-frame design provides a very homogeneous field even without shims (the quote), while a dipole C-magnet TYPICALLY produces a ~0.1% gradient across the pole with even harmonics; the lecture's H/C weight and shim comparisons sit alongside (scan re-read queued).
C-magnet: ~0.1% gradient across pole vs central field, harmonics n = 2,4,6Source quote & editorial note
Typically, the dipole produces a gradient across the pole of 0.1% with respect to the central field ... the window-frame design provides a very homogenous field quality even without shims.
Editorial note, tabletop extrapolation: Validates the reference machine's H-frame choice for a cyclotron (two-fold symmetry, lighter than a C) and warns that shimming will still be needed.
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For yoke steel use cold-rolled non-grain-oriented electro-steel (EN 10106) with sheet 0.3-1.5 mm, coercivity Hc < 65 A/m (spread < +/-10 A/m); solid yokes are unsuited to fast cycling - eddy currents lag and heat them, though slow ramps are fine - and, if used, all parts should come from the same melt for reproducibility.
sheet 0.3-1.5 mm; density 7.60-7.85 kg/dm3; Hc < 65 A/m; dHc < +/-10 A/m; resistivity 0.16-0.61 uOhm*mSource quote & editorial note
Sheet thickness 0.3 <= t <= 1.5 mm ... Coercivity Hc < 65 A/m ... Coercivity spread dHc < +/- 10 A/m
Editorial note, tabletop extrapolation: For a DC cyclotron magnet solid mild steel is fine, but this gives the numeric target for 'good' steel and explains why scrap-plate yokes vary.
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Estimate the mean turn length as l_avg = pole perimeter + 8 x (clearance between pole and coil) + 4 x coil width - the quoted formula; the lecture's sanity band 2.5*l_iron < l_avg < 3*l_iron (l_iron the iron core length) is its companion check for racetrack geometry (scan re-read queued).
l_avg = pole perimeter + 8*clearance + 4*coil width; 2.5 l_iron < l_avg < 3 l_ironSource quote & editorial note
l_avg = pole perimeter + 8 x clearance between pole and coil + 4 x coil width
Editorial note, tabletop extrapolation: Gives copper length, hence resistance and power, straight off a sketch - exactly what a garage builder needs before ordering tubing.
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Pick current density from the cooling method and coil geometry: at most 1 A/mm^2 for voluminous coils almost entirely enclosed in the yoke, up to ~2 A/mm^2 only for small thin well-exposed air-cooled coils, and up to ~10 A/mm^2 as the typical upper end for direct water-cooled hollow conductor - higher is possible but at the cost of reliability.
air (bulky, enclosed): j <= 1 A/mm^2; air (small, thin): j < 2 A/mm^2; water-cooled: j up to ~10 A/mm^2 (typical upper end)Source quote & editorial note
the maximum current density for voluminous coils which are almost entirely enclosed in the magnet yoke should not exceed 1 A/mm2 ... The current density in direct water-cooled coils can be typically as high as 10 A/mm2.
Zickler, Basic Design and Engineering of Normal-Conducting, Iron-Dominated Electromagnets — arXiv:1103.1119 (2010) — p. 28-29, 31
Editorial note, tabletop extrapolation: The reference machine's 538-turn solid copper tubing coils sit in the air-cooled regime; unless they qualify as small and thin enough to shed heat (the source's 2 A/mm^2 case), the quoted limit for enclosed coils is 1 A/mm^2 - going higher means hollow conductor with water flow.
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Design water cooling to keep coolant velocity turbulent but below 5 m/s (Re > 4000), coil surface below 60 C, and water temperature rise <= 30 C from a 30 C inlet, with 0.1-1.0 MPa (1-10 bar) available pressure drop.
u_avg <= 5 m/s; Re > 4000; dT <= 30 C; T_surface < 60 C; dp = 0.1-1.0 MPaSource quote & editorial note
The velocity of the cooling medium ... should be sufficiently high to guarantee a turbulent flow but low enough (u_avg <= 5 m/s) to avoid erosion and vibration. A maximum permitted temperature of less than 60 C on the coil surfaces was found to be good practice.
Editorial note, tabletop extrapolation: Hard numbers for a home chilled-water loop as DESIGN limits, not damage cliffs: hold velocity under ~5 m/s (erosion and vibration risk grow beyond it), coil surfaces under 60 C (insulation aging accelerates with temperature), and note the arithmetic - a 30 C inlet plus 30 C rise means up to 60 C outlet water, consistent with the surface limit but tight in a hot garage: derate for your ambient.
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Use the closed-form water-cooling recipe in the source's units throughout: flow Q[l/s] = 2.388e-4 * P/dT, temperature rise dT = 3.04e-7 * P/(u_avg d^2), and required bore d = 5.59e-3 * (P/(dT*Kw))^0.368 * (l/dp)^0.21, with Kw as defined in the source.
Q = 2.388e-4 P/dT; dT = 3.04e-7 P/(u d^2); d = 5.59e-3 (P/(dT Kw))^0.368 (l/dp)^0.21; u_avg = 0.3926 d^0.714 (dp/l)^0.57 - coefficient-based, unit-specific: convert every input to the source's units before useSource quote & editorial note
Q_water = 2.388 x 10^-4 P/dT ... d = 5.59 x 10^-3 (P/(dT Kw))^0.368 (l/dp)^0.21
Editorial note, tabletop extrapolation: Lets the builder compute the hollow-conductor bore and pump requirement for a next machine's 5-20 kW magnet with a spreadsheet, no CFD - provided every input is converted to the source's units first: a bar-for-pascal slip in the pressure drop moves the bore answer far more than the recipe's real margin.
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Compute dipole excitation as NI = B*h/(eta*mu0) with magnet efficiency eta ~= 98% for a well-designed unsaturated yoke (the iron path costs only ~1-2% extra ampere-turns when mu_iron >= 1000 and L_iron <= 10h).
NI_dipole = B*h/(eta*mu0), eta ~ 0.98Source quote & editorial note
NI_dipole = Bh/(eta*mu0), where the magnet efficiency, eta... The magnet efficiency for a well designed yoke is eta >= 98%.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 116-117, 129
Editorial note, tabletop extrapolation: One-line check of the reference machine's 538 turns: at 0.59 T and its gap the formula predicts the required current within a couple percent if the H-frame iron is unsaturated. A measured efficiency well below the formula's ~98% says the model is missing something - saturation, leakage, a parasitic joint gap, or a wrong effective-gap value - and FEMM sorts out which.
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Choose low-carbon magnet steel (the 1010 class, carbon near or below 0.10%); its BH curve becomes highly nonlinear above B ~ 1.5 T and shows fully saturated behavior by B ~ 2.0 T - incremental permeability falling toward mu0 while B still creeps up with H - so keep working iron flux density below ~1.5 T for linear, reproducible excitation.
1010-class steel: nonlinear B >= 1.5 T; fully saturated behavior B >= 2.0 T (incremental mu -> mu0; B does not stop rising)Source quote & editorial note
The BH relationship becomes highly nonlinear at B >= 1.5 Tesla and the material exhibits fully saturated behavior at B >= 2.0 Tesla.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 249-251
Editorial note, tabletop extrapolation: Sets the iron budget for the next machine: yoke and pole cross-sections should be sized so flux density stays under ~1.5 T anywhere on the return path, and pole-tip fields much above 1.8 T are not worth chasing with iron.
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Assume the fringe field extends about one half-gap h beyond the steel pole edge of a dipole (h/2 for a quadrupole of pole radius h); the pole steel therefore ends about one half-gap inside where the field effectively ends.
L_fringe ~ h (dipole), ~h/2 (quad), ~h/3 (sextupole)Source quote & editorial note
A general rule of thumb is that the length of the fringe field beyond the edge of the steel pole tip is = h, = h/2, or = h/3, for the dipole, quadrupole or sextupole
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 252-253
Editorial note, tabletop extrapolation: Tells the builder where usable field really stops on an 8-inch pole: the fringe extends about one half-gap BEYOND the steel edge before dying away, while the flat, usable region ends somewhat inside the pole radius as the falloff begins. Map B(r) (FEMM, then Hall probe) to place the maximum stable orbit; the h rule sizes how much radial real estate the fringe transition consumes.
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Size dipole pole width by adding pole overhang beyond the good-field region: for an optimized (edge-bumped) pole, overhang a = h*(-0.14*ln(dB/B) - 0.25); for a flat unoptimized pole, a = h*(-0.36*ln(dB/B) - 0.90), where h is the half gap.
x=a/h; optimized: dB/B=(1/100)exp[-7.17(x-0.39)]; unoptimized: dB/B=(1/100)exp[-2.77(x-0.75)]Source quote & editorial note
The canonical expressions... are used to estimate the amount of pole overhang required to achieve a desired field quality... for both unoptimized and optimized pole contours.
Editorial note, tabletop extrapolation: Directly sizes how much of the reference machine's 8-12 inch pole diameter is usable good field; e.g. for dB/B=1e-3 an unoptimized pole needs ~1.6 half-gaps of extra pole beyond the outermost useful orbit.
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Plain radial-sector pole tips fared worst in the Rutgers 12-inch mapping campaign: the steepest average-field falloff with radius - unusable in their assessment - while spiral sectors compromised between usable average field and roughly triple the weak-focusing axial tune.
weak focusing: flattest <B>(r); radial sector: largest falloff (unusable); spiral sector: intermediate, ~3x weak-focus nu_z at small radiiSource quote & editorial note
the radial sector poletips have the greatest average falloff - so great that it amounts to be an unusable field. The spiral sector AVF field is a compromise between the two.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 10
Editorial note, tabletop extrapolation: Direct guidance for a next machine's pole-tip upgrade at the 8-12 inch scale, as a measured comparison among these candidates rather than a ban: radial-sector AVF machines exist, but making one work takes sector-angle and profile design these candidates did not carry. Also warns that narrow spiral vanes saturate at large radius - the measured field fell below simulation there.
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Screen candidate pole-tip designs with two numbers from the 2-D map - average field vs radius (isochronism) and axial tune from nu_z^2 = n + F^2*N^2/(N^2-1), the straight-sector smooth approximation - and reserve full phase-space tracking for the final one or two contenders.
nu_z^2 ~= n + F^2*N^2/(N^2-1) (smooth approximation, straight sectors; spiral sectors add a (1+2tan^2 xi) factor; check the flutter definition in use before substituting)Source quote & editorial note
this analysis approach can be used to quickly assess a field during design, relegating the laborious task of phase space mapping and determining the limits of stability to the few the final contenders.
Koeth & Krutzler, Field Mapping in Cyclotron Magnets (2015) — p. 10-11
Editorial note, tabletop extrapolation: A cheap, quantitative design filter that works from measured maps of a home-built magnet, no orbit code required.
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First-order coil sizing: producing 1 T across a 2 cm gap requires ~16 kA-turns (e.g. 160 turns at 100 A); for a given supply and winding, gap field is inversely proportional to pole spacing.
NI = B*g/mu0; 1 T x 0.02 m -> 1.6e4 A-turnsSource quote & editorial note
production of a field of 1 T in a gap with a 0.02 m spacing requires 16-kA turns (160 turns of wire if a 100-A supply is available).
Humphries, Principles of Charged Particle Acceleration (1986) — p. 111
Editorial note, tabletop extrapolation: Numerically the builder's own worked example: 538 turns at ~30 A across the reference machine's 1.42-in (3.6 cm) gap predicts ~0.56 T from the ideal gap formula - an upper bound, because real iron reluctance and leakage only subtract from it. The measured shortfall from ideal maps those losses; FEMM attributes them.
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Magnetic fringe fields extend beyond a gap a distance comparable to the gap width (the quote's scale length); the same Laplace-equation scaling governs electrode pairs, which is why deflector designs terminate their field with a septum rather than letting it leak into the last orbits.
fringe extent ~ gap width gSource quote & editorial note
The vertical field magnitude decreases away from the magnet over a scale length comparable to the gap width.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 140, 526
Editorial note, tabletop extrapolation: Rule of thumb for a next machine's layout: expect roughly one gap-height of field transition at the pole edge - how much of it is actually unusable depends on the field tolerance, so map it (dg-098) - and shield any deflector with a grounded septum as designed practice.
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The lecture's scaling argument: final energy goes as T ~ K*Q^2/A with K = (e*B*rho)^2/(2*m0), so at fixed energy the extraction radius falls as 1/B - and, under geometric similarity, iron volume as 1/B^3 (their example: r_extraction 2.28 m at 1 T vs 0.76 m at 3 T, a 1/27 volume ratio).
K_B = (e*B*rho)^2/(2*m0); radius ~ 1/B at fixed energy; volume ~ 1/B^3 under geometric similaritySource quote & editorial note
Almost (but not quite) spherical: Efficient cyclotron magnetic circuits include more iron laterally than axially
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 48-50
Editorial note, tabletop extrapolation: The B^2 energy leverage argues for raising a next machine's field before enlarging poles: doubling B quadruples energy at fixed radius. The 1/B^3 mass saving holds only while the whole magnet scales geometrically - gap included - and the iron's own saturation (dg-096) caps how far the argument runs.
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Choose the ISM frequency 13.56 MHz (B = 0.889 T for protons) to drive the dee from commercial RF generators - the source machine's reason for its tuning - typically 50-ohm hardware through a matching network.
f = qB/(2*pi*m): 13.56 MHz protons -> B = 0.889 T; 50-ohm source -> matching network -> high-Z deeSource quote & editorial note
The cyclotron circuit was originally tuned to a frequency of 13.56 MHz due to the requirements of the commercial RF generator in use ... a magnetic field of 0.889 Tesla is required.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 10-11
Editorial note, tabletop extrapolation: Directly actionable option for a next machine: targeting ~0.89 T instead of 0.59 T puts the machine on the 13.56 MHz ISM band, where used generators, amplifiers and matchboxes are plentiful. Legality rides on emissions containment rather than the band label (dg-1373's verification), and the match must still be designed for the dee's actual impedance (dg-287).
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Shape pole faces (spherical slice or edge 'lump') to produce a few-percent radial field decrease - a flat 'magnetic capacitor' gap gives n = 0 and no vertical restoring force, so some deliberate contouring is required; the source works the example of a ~3% edge fall-off on a 6-in-radius pole via a best-fit sphere of rho ~ 21.8 in (about a 32-degree slice).
for 3% edge fall-off on 6-in-radius pole: best-fit sphere rho ~ 21.8 in (slice ~32 deg); B_z = B_0*(r0/r)^n, restoring force needs 0 < n < 1Source quote & editorial note
A radially decreasing field can be described as Bz = B0(r0/r)^n for n >= 0, where n = 0 implies a uniform field and n > 0 implies a restoring force.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 7-9
Editorial note, tabletop extrapolation: Exactly the reference machine's problem class and size: machine a gentle crown or stepped 'lump' into the 8-inch poles (or shim equivalently), aiming for the few-percent center-to-edge fall-off of the source's worked case - and verify the result against the mapped n(r) (dg-003, dg-561) rather than the geometric recipe, since the actual profile depends on gap and permeability.
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Compute magnet excitation from NI = 2.02 x B(gauss) x gap(inches) - the ideal air-gap MMF in historical units (NI = B*g/mu0).
NI (ampere-turns) = 2.02 x gauss x inches of gapSource quote & editorial note
Ampere-Turns = 2.02 x gauss x inches gap
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Editorial note, tabletop extrapolation: Directly applicable: 5900 G across a 2-inch gap needs ~24,000 ampere-turns as the ideal floor, with iron reluctance and leakage added on top (dg-016, dg-036). Leakage multiplies the FLUX the iron must carry - that sizes the yoke - not the gap MMF this formula computes.
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Design pole and coil fastenings for the magnetic forces: pole-face attraction is (kilogauss)^2 x (area in in^2)/1.735 pounds, and conductor force is kG x amps x inches/1750 pounds.
F_pole(lb) = kG^2 x in^2 / 1.735; F_cond(lb) = kG x A x in / 1750Source quote & editorial note
Lbs. force on conductor = 1/1750 x kilogauss x amperes x inches length; Lbs. force between pole faces = 1/1.735 (kilogauss)^2 x (inches^2 area)
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Editorial note, tabletop extrapolation: Directly applicable: at 5.9 kG on 50 in^2 poles that is ~1000 lb of attraction a next machine's bolts and spacers must carry.
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Wouters' recommendation: run the magnet iron near saturation for most economical performance, with most soft irons beginning to saturate near 16 kilogauss and some usable to 21 kG.
B_sat(soft iron) ~ 16 kG; upper limit ~21 kGSource quote & editorial note
most soft irons begin saturating in the vicinity of 16 kilogauss, though some may be operated as high as 21 kilogauss
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 2
Editorial note, tabletop extrapolation: Directly applicable - with the right variable: the binding number is the LOCAL flux density in the narrowest iron section, which leakage, joints and corners push above the gap figure (dg-037). The reference machine's 5.9 kG gap field leaves apparent margin; how much field a next machine can add before the iron dominates is a FEMM answer, not a factor read from the gap value.
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Size the yoke/coil for leakage flux by multiplying the gap flux by a factor set by the gap-height/gap-diameter ratio: 1/2 gives 2.0, 1/4 gives 1.5, 1/10 gives 1.2 (small cyclotrons live in the 1.5-1.2 region).
leakage multiplier: h/D=1/2 -> 2.0; 1/4 -> 1.5; 1/10 -> 1.2Source quote & editorial note
Ratio Gap Height/Gap Diameter ... Multiplying Factor: 1/2 -> 2; 1/4 -> 1.5; 1/10 -> 1.2, region of small cyclotrons
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 2
Editorial note, tabletop extrapolation: Directly applicable sizing rule: for an 8-inch pole with ~1.5-2 inch gap (h/D ~ 1/4), design coils and yoke for ~1.5x the gap flux.
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Make the pole-core length and the pole-core-to-return-yoke distance at least twice, preferably three times, the gap height.
L_core >= 2-3 x h_gap; core-to-yoke spacing >= 2-3 x h_gapSource quote & editorial note
the length of the pole cores and the distance from pole cores to return yokes is at least twice and preferably three times the gap height
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable to a next machine's H-frame: coil space often pushes the frame toward compliance anyway - check it explicitly whenever the frame is shortened, rather than assuming the coils did the enforcing.
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Bias saturation away from the return path by giving the yoke at least 25 per cent more total cross-sectional area than the cores - the source's margin.
A_yoke >= 1.25 x A_coreSource quote & editorial note
the return yoke must accordingly be designed so that its total cross sectional area is a good deal greater than that of the cores, say, at least 25 percent greater
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable: for 8-inch (50 in^2) cores, provide at least ~63 in^2 of total yoke steel around the flux return - and still check the narrowest local section, corner and joint (dg-037, dg-132): the area margin lowers AVERAGE density, while local constrictions can saturate first regardless.
-
Machine yoke-to-yoke and yoke-to-core contact surfaces flush to eliminate parasitic air gaps in the magnetic circuit.
Source quote & editorial note
It is important that the contact surfaces between yoke pieces and between yoke and pole cores be flush to eliminate additional air gaps
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable: any unintended air gap adds straight onto the magnetic circuit's gap budget - 0.003 in against a 1.5-in main gap is 0.2%, small but real; the same error across tight pole-cap joints is proportionally worse. Machine flush because it is cheap at build time and unfixable after assembly.
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Make vacuum-chamber top and bottom thin, circular steel plates - the quoted design, chosen to decrease the magnetic gap as much as possible - and make the side wall non-magnetic (brass, per the source) so field is not bypassed around the gap.
Source quote & editorial note
top and bottom of the vacuum chamber should be thin, circular steel plates ... to decrease the magnetic gap as much as possible. To prevent field bypassing, the tank wall must be non-magnetic, preferably brass
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 5
Editorial note, tabletop extrapolation: Directly applicable chamber architecture for a small machine; every millimeter of chamber wall inside the gap costs ampere-turns.
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Size the return yoke cross-section larger than the pole so yoke flux density drops below pole-tip field (Cyclotron Kids: 1.6 T on 14-inch poles reduced to 1.2 T in the yoke), keeping the return path out of saturation with scrap steel.
A_yoke/A_pole >= B_pole/B_yoke_target (1.6 T -> 1.2 T)Source quote & editorial note
Increased cross section reduces flux through yoke to 1.2T
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 8
Editorial note, tabletop extrapolation: Area-ratio thinking for welding a next machine's frame from surplus plate: size the yoke so its flux density lands comfortably below the knee of the ACTUAL steel's BH curve - surplus plate is rarely certified, so measure or assume conservatively - and check per-limb: flux splits between return limbs, and the narrowest section, corner or weld is what saturates first, not the gross ratio.
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Machine a slight taper on the pole faces so the field decreases with radius, providing the weak-focusing (restoring) Lorentz force on the beam - design it in the field code before cutting steel.
Source quote & editorial note
Slight taper on pole applies a corrective Lorenz force to the beam. Made with freeware! Poisson Superfish
Baumgartner & Heuer, The Cyclotron Kids 14-Inch Accelerator (2010) — p. 8
Editorial note, tabletop extrapolation: The documented amateur approach at the reference machine's scale - Cyclotron Kids here, with the pole-shaping rules (dg-119, dg-152) carrying the design math: put the field index into the pole profile deliberately, designed in the field code before cutting steel, rather than relying on accidental fringing.
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The deck's account: a 300 keV-class proton cyclotron project with a stated under-$1000 budget — 'Wanted 300keV protons, had <$1000 budget' — reached base pressure 0.01 mTorr, 1.6 kVpp on the dees at ~400 W peak RF, on a C-frame yoke of welded 5x5-inch soft-steel bar with meehanite pole pieces face-milled to a field-index profile. [2026-09-06 erratum, scan re-read: the deck states 300 keV as a goal and $1000 as a spending ceiling; it never states completion, an achieved beam energy, or a final cost — the earlier 'completed for under $1000' converted an aspiration into an achievement. The engineering figures are verified on the slides; the source is a slide deck, not an article.]
goal 300 keV on <$1000 budget; verified engineering: 0.01 mTorr base, 1.6 kVpp dee, ~400 W pk, machined field-index pole profileSource quote & editorial note
Polepieces of meehanite steel facemilled to a profile that gave appropriate field index... 1.6kVpp on Ds, 400Wpk. Base pressure 0.01mTorr
Niell, Effective Scientific Equipment Procurement Strategies: Building on a Budget (2010) — p. 11-17
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: the engineering menu at the reference machine's energy class — modest dee voltage (1-2 kVpp), 1e-5 torr, a machined pole profile, not heroic RF or UHV — is what the deck describes pursuing below ~300 keV. It documents the approach, not a completed machine: the existence-proof framing is withdrawn, and the census carries the documented Niell beam record separately.
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Keep the n = 0.2 contour out of the region the beam occupies: n = 0.2 is the coupled Walkinshaw resonance (2*nu_z = nu_r), and a weak-focusing machine whose ions spend many turns near it transfers radial oscillation into vertical growth wherever a coupling perturbation - field asymmetry, misalignment - drives it; real machines usually have one.
n = -(r/B)(dB/dr) < 0.2 for r < r_max; unmodified Houghton magnet reached n = 0.2 at r = 5.9 cm vs 7.8 cm Dee radiusSource quote & editorial note
the field index value n=0.2 must not occur inside the maximum ion orbit radius to avoid coupled resonances
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 2, 39
Editorial note, tabletop extrapolation: One necessary check for weak-focusing pole shaping on a 100 keV-1 MeV tabletop machine, and computable from a measured B(r) curve - necessary, not sufficient: axial focusing margin (n > 0), radial stability (n < 1), phase slip, aperture and orbit clearance all still have to be verified against the actual B(r). Where the contour cannot be pushed out to the final radius (dg-152), the design question becomes how few turns the beam spends near it, not whether the machine can work at all.
Cited in: Beam Dynamics: An Interactive Laboratory
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Make Bz decrease with radius so that the field has a restoring radial component off the median plane: weak axial focusing comes from a negative dBz/dr, and Morrow's thesis describes achieving it with a linearly decreasing Bz. The criterion that matters is the field index n = -(r/B)(dB/dr) staying in its stable range (dg-145, dg-136), not linearity of B(r) as such - constant n means B proportional to r^-n, not a straight line. [Corrected 2026-08-23: earlier text told the builder to judge every shim by the linearity of B(r) and stated Br = C*z; the sign is Br ~ z*dBz/dr (negative for a falling field) and linearity is one field shape that focuses, not the acceptance test.]
Near the median plane (curl B = 0): Br ~ z * dBz/dr. Axial focusing needs dBz/dr < 0, i.e. n = -(r/B)(dB/dr) > 0; stability 0 < n < 1, with n = 0.2 the Walkinshaw resonanceSource quote & editorial note
weak magnetic focusing can be achieved by producing a magnetic field in which Bz linearly decreases.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 26-27
Editorial note, tabletop extrapolation: For a shimming attempt on the reference machine's 8-inch poles the plottable acceptance test is n(r) from the measured B(r), by finite differences, kept inside its stable range over the whole used radius - not a straight-line fit to B(r). A field profile that passes that test still has to be checked for isochronism and phase slip (dg-1328), the n = 0.2 contour (dg-136, dg-152) and radial stability; "no orbit code needed" was an overreach, though a simple n(r) plot does reject a bad shim before any tracking is run.
Cited in: Beam Dynamics: An Interactive Laboratory
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Use the Poisson Superfish (free, 2-D magnet cross-section) plus SIMION 8.1 (commercial ion tracking) workflow to evaluate magnet modifications before cutting steel; the thesis includes the geometry files and the PSF-to-SIMION conversion recipe.
PSF model: pole face 150 mm, pole gap 39 mm, coil current 70 A, half-plane sliceSource quote & editorial note
Pole face: 150mm, Pole gap: 39mm, Current: 70A ;NOTE: this is a slice down the middle of the magnet
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 60-68
Editorial note, tabletop extrapolation: Low-cost simulation path for a hobbyist - Superfish is free, SIMION is paid but widespread, and FEMM plus the playbook's Python tracker is the all-free equivalent; the appendix geometry file is a working starting template for an 8-15 cm pole magnet.
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Budget cooling water across subsystems explicitly - the Houghton thesis's own bookkeeping: the 15 cm magnet wanted 6.1 L/min at 70 A, but the chiller could spare only 3.0 L/min after the diffusion pump's 0.8, capping operation at 50 A / 1.1 T. The source attributes the field limit to both cooling and the power supply ('the maximum field is limited by available water cooling and the power supply'); the thesis's own arithmetic makes cooling the binding constraint at 70 A.
GMW 3473-70: 70 A needs 6.1 L/min; chiller 3.8 L/min total -> limited to 50 A, 1.1 T at 3.85 cm gapSource quote & editorial note
A Haskris H-4057 water chiller, capable of 3.8 L/min (1.0 gpm) ... Since the diffusion pump requires at least 0.8 L/min, the maximum that can be supplied to the magnet is 3.0 L/min ... the magnet requires 6.1 L/min
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. PDF p.36 = printed p.36 (Loucks thesis Sec. 3.2 Magnet); the cited '35-36' range is correct, all figures are on 36
Editorial note, tabletop extrapolation: Do the L/min bookkeeping for the whole next machine (magnet + diffusion/turbo + RF amp) before buying a chiller; the cooling loop is a first-class design constraint, not an afterthought.
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A 1.2 T tabletop cyclotron design point: 15 cm flat pole faces with the chamber in place giving a 3.81 cm pole-tip separation, 1.28 T at 70 A, water cooled at 18 C and 0.8 gallon/min at 50 A.
15 cm poles, gap 3.81 cm, 1.28 T at 70 A (1.16 T at 50 A); cooling 18 C water at 0.8 gpmSource quote & editorial note
With the chamber in place, the separation between the pole tips is 3.81 cm, giving a maximum magnetic field of 1.28 T at 70 A ... requiring 18 C water flowing at 0.8 gallons per minute (at 50A)
Editorial note, tabletop extrapolation: A purchasable-magnet benchmark almost exactly at the reference machine's scale. The 0.8 gpm is a flow figure, not a chiller spec: size the chiller from coil dissipation and allowable temperature rise (P = flow x heat capacity x dT - the magnet-power calculator's territory), with the flow number as the plumbing constraint it is.
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A proven parameter set at exactly the reference machine's scale: 12 in poles, 4 in gap with removable 1 in pole tips, 1.2 T max, single 5 in radius dee with 0.9 in aperture, 2-30 MHz RF at up to 1.5 kW giving ~10 kV dee, 1e-5 Torr operating pressure.
12 in poles / 4 in gap / 1.2 T / 5 in dee / 0.9 in aperture / 1.5 kW -> ~10 kV dee / 1e-5 TorrSource quote & editorial note
12 inch diameter poles pieces forming a 4-inch gap to which upper and lower pole tips up to 1-inch thick can be easily attached and removed. ... all capable of producing a maximum central axial field, Bz(r=0), of 1.2 Tesla ... a single 5-inch radius DEE with a 0.9 inch vertical aperture and a matching dummy DEE. The Radio Frequency (RF) supply is tunable from 2 to 30 MHz with adjustable power up to 1.5 kW ... capable of achieving a peak DEE voltages on the order of 10 kV ... the 2-inch tall, 13-inch diameter cyclotron vacuum chamber's operating pressure of 1E-5 Torr.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: A complete cross-check machine for a next machine's sizing; note the removable-pole-tip trick that lets one magnet host many field profiles.
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Make pole tips removable, swappable inserts - up to 1 inch thick per the quote, with the source machine keeping four sets - so field-shaping and AVF experiments proceed without rebuilding the magnet.
Source quote & editorial note
upper and lower pole tips up to 1-inch thick can be easily attached and removed - we currently have four sets of pole tips.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: Probably the single best architecture decision the builder can copy: swap-on tips let a next machine iterate field profiles cheaply - with the caveat that a sector-tip (AVF) conversion is still re-checked against return-path saturation and coil clearances (dg-045).
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Shape the weak-focusing pole taper so the field index reaches n = 0.2 only at the final ion radius: the n = 0.2 point is the nu_r = 2*nu_z coupling resonance, where dwelling ions grow axially as far as the driving perturbation and dwell time allow - the aperture is what catches them when they do.
n(r) = -(r/Bz)(dBz/dr); require n < 0.2 for all r < r_finalSource quote & editorial note
if n = 0.2 is to be avoided (vx=2vz), then the rate at which the vertical field decreases must be moderated such that n=0.2 occurs at the final ion radius.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 3
Editorial note, tabletop extrapolation: The quantitative pole-taper design rule for a next machine: map n(r) from the field profile and keep 0 < n < 0.2 out to full beam radius.
Cited in: Beam Dynamics: An Interactive Laboratory
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For AVF/hybrid pole designs, use the tune formulas nu_z^2 = -k + F(1+tan^2 xi) and nu_r^2 = 1 + k (k = average field index, F = flutter, xi = spiral edge angle) and keep both tunes away from integer and rational-fraction resonances.
nu_z^2 = -k + F(1+tan^2(xi)); nu_r^2 = 1+kSource quote & editorial note
The axial tune... can be summarized by: vz2 = -k + F(1+tan2xi) and the radial tune is written as: vr2 = 1+k
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 6
Editorial note, tabletop extrapolation: If a next machine gets sector pole tips (allowing a rising average field), these two lines are the first-order SCREEN - in the source's conventions: check the sign convention for k and the flutter definition before substituting (dg-156's lesson) - with resonance avoidance and then tracking completing the design.
Cited in: Beam Dynamics: An Interactive Laboratory
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Compute both tunes from the same four quantities - field index n, flutter F, sector number N and spiral angle xi - using nu_z^2 = n + (N^2/(N^2-1))*F*(1+2tan^2 xi) with F = (<B^2>-<B>^2)/<B>^2 as the source defines it, and the matching radial expression.
nu_z^2 = n + (N^2/(N^2-1)) * F * (1 + 2 tan^2 xi); F = (<B^2> - <B>^2)/<B>^2 (the source's flutter - many texts call this quantity F^2; check the convention before substituting); n = -(r/B) dB/drSource quote & editorial note
F = ((<B^2> - <B>^2)/<B>^2) is called the flutter and represents the hill to valley field difference
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 25-26
Editorial note, tabletop extrapolation: The complete design equation set for an AVF follow-on build; every term is measurable from a 2-D Hall-probe map of the built magnet.
Cited in: Beam Dynamics: An Interactive Laboratory
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Spiral the poles rather than relying on edge focusing alone when flutter is small: edge focusing from a radial sector gives one focusing and one defocusing edge per hill, whereas a spiral angle multiplies the flutter term by (1+2tan^2 xi) at both edges.
focusing enhancement factor (1 + 2 tan^2 xi); at xi = 45 deg the flutter term triplesSource quote & editorial note
N large: high maximum energy, F small and quasi circular orbits -> spiral compulsory
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 26, 28
Editorial note, tabletop extrapolation: Explains when the extra machining pain of spiral tips pays: when flutter is small and orbits quasi-circular - the quoted regime, where 'spiral compulsory'. Whether an 8-12 inch N = 4 design wants spiral or more hill/valley contrast is a computed comparison (the (1+2tan^2 xi) factor against achievable flutter), not a default.
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Use N >= 3 sectors in any AVF design: the perturbative radial-tune expression breaks down at N = 2 (its resonant denominator vanishes - the pi stop-band boundary behind the quote's 'N must be larger than 2'), and each N carries an energy ceiling T = (N/2 - 1)*E0 - about 469 MeV for N = 3 and 938 MeV for N = 4 protons.
nu_r^2 = 1 - n + (N^2/(N^2-1))(3/(N^2-4)) F^2 (1+2tan^2 xi); T_max = (N/2 - 1) E0Source quote & editorial note
It implies that N must be larger than 2 (lower limit of the pi stop-band) and there is an energy limit for every N value T = (N/2 - 1)E0
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 27-28
Editorial note, tabletop extrapolation: Rules out 2-sector 'butterfly' pole tips that look easy to machine; N=3 or 4 is the practical amateur choice and neither limits sub-MeV protons.
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With constant gaps B(r) falls naturally with radius and the larger the gap the faster it falls, while coil-dominated field rises with radius but only matters once the iron saturates - use that pairing to get the profile you want.
Source quote & editorial note
Constant gaps : B(r) naturally decreasing. The larger the gap, the stronger the decrease ... Coil field : B(r) naturally increasing. Important only when iron becomes saturated
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 32
Editorial note, tabletop extrapolation: Explains the positive field index (n > 0 in the site's n = -(r/B)dB/dr convention) that a flat-pole tabletop magnet already has from its natural falloff - and why a bigger gap gives more weak focusing but less field.
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Reach for the iron before the copper when shaping a warm magnet's field: trim coils increase the gap and are 'very weak except in superconducting machines' - and even then, model before implementing (both quoted); iron shaping carries the flip side the lecture tabulates - effective and cheap but non-linear and fixed once cut (comparison rows: scan re-read queued).
Source quote & editorial note
Trim coils increase the gap ... Very weak except in superconducting machines ... Model it before implementing it to avoid unexpected effects
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 33, 47
Editorial note, tabletop extrapolation: Settles the shim-vs-trim-coil question for a small warm magnet the way the Houghton thesis found empirically: iron wins for the main profile. A weak trim coil can still earn a place for fine, reversible adjustment where the gap budget allows one.
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Choose yoke stock by construction method - the quoted row: laminations are limited to about 300 mm stack thickness (200 mm usual) with good, slightly anisotropic magnetic and mechanical properties; the lecture's casting and forging rows carry their own trades (scan re-read queued).
laminated stack thickness: 300 mm max, 200 mm usualSource quote & editorial note
Laminated: Limited thickness : 300 mm max, usual 200 mm. Good magnetic and mechanical properties. Slight anisotropy.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 57
Editorial note, tabletop extrapolation: For an amateur the practical read is: mild-steel plate stock is fine for a DC magnet; note the anisotropy if you stack plate for pole tips.
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Trade pole gap deliberately: a small gap needs fewer ampere-turns and allows a smaller pole radius - which pushes the orbits close to the outer edge, leaves no room for probes, injection and pumping, and is very sensitive to errors (vertical losses); a large gap eases vacuum, injection, extraction and diagnostics at the cost of field.
Source quote & editorial note
small gap: reduced number of At of coils, pole radius reduced, orbits close to outer edge, no space, very sensitive to errors : vertical losses. large gap: large space: injection, extraction, probes, easier vacuum pumping, lower field
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 65
Editorial note, tabletop extrapolation: Frames the central decision for a next machine (the reference machine's chamber must fit in the gap) with the actual list of consequences on both sides.
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Follow the lecture's design order - step 0: squeeze the requirements; step 1: starting numbers by hand calculation; step 2: 2-D global model; step 3: 3-D global model; step 4: 2-D cuts for detailed local objects - preferring 2-D calculations wherever they serve.
step0 requirements -> step1 hand calculation -> step2 2D global -> step3 3D global -> step4 2D radial cutsSource quote & editorial note
step0: Squeeze requirements and extract juice; step1: Get starting numbers from hand calculation; step2: 2d global model; step3: 3d global model; step4: 2d cuts for detailed local objects ... 2d calculations must be preferred.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 68
Editorial note, tabletop extrapolation: A workflow a solo builder can actually execute, and it puts pencil-and-paper (Zickler-style) sizing ahead of any software.
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In a hill/valley magnet the average field at large radius is <B> = k*B_hill + (1-k)*B_valley with stacking factor k = N*theta_hill/360 (the source's k = hill-angle/90 is its four-sector case); RF efficiency prefers k = 0.5, compactness pushes k up - C235 chose k = 0.67 (60-degree hills).
<B> = k*B_hill + (1-k)*B_valley; k = N*theta_hill/360 (source's /90 form = four sectors); C235: k = 0.67Source quote & editorial note
For best RF efficiency, k=0.5 BUT to decrease machine dimensions k >0.5 (more hill, thus more field) CHOICE : k=0.67 (60 deg hills)
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 69
Editorial note, tabletop extrapolation: The arithmetic to go from a required <B> to hill/valley fields and sector angle - first-order and reusable at any scale, with fringe and gradient effects refining it in the field code.
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The source's design sequence: choose a target axial tune (their CHOICE: nu_z = 0.2), which then fixes the spiral angle once n, N and F are known; keeping flutter and spiral modest leaves room for a stronger field gradient.
CHOICE nu_z = 0.2; spiral angle xi then determined by nu_z^2 = n + (N^2/(N^2-1))F^2(1+2tan^2 xi)Source quote & editorial note
CHOICE : nu_z = 0.2. Flutter and spiral not too large. Field gradient can be strong. Spiral angle of pole completely determined since n, N, F and nu_z are known
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 69
Editorial note, tabletop extrapolation: Gives a numeric focusing target to design toward instead of 'as much focusing as possible'. On a classical weak-focusing machine at the reference machine's energies, nu_z = 0.2 means n = 0.04 - modest and achievable from pole-face falloff. The caveat belongs to AVF designs: there the isochronous average field RISES with radius (vertically defocusing on its own), and the flutter/spiral term must supply the whole tune, which is exactly why the source treats nu_z as a choice that determines the spiral angle.
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Field in the gap of an iron-dominated magnet is B = mu0*n*I/h - proportional to total ampere-turns, inversely proportional to gap, and independent of pole area; so minimize the reluctance of the iron path so the ampere-turns are spent on the gap.
B = mu0 n I / h (h = gap height)Source quote & editorial note
the field B = mu0 nI/h is proportional to the total current in the solenoid, is inversely proportional to the magnetic gap and is independent on the pole surface, a rather counter-intuitive fact to most people.
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 70-71
Editorial note, tabletop extrapolation: The core sizing identity for a home magnet, in its regime (unsaturated iron, h the total effective gap): field follows ampere-turns over gap, and bigger poles alone buy nothing. Shaving the gap buys field at the price of chamber, dee and beam clearance (dg-163's trade) - cheap, not free.
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Remember permeability is a strong function of induction: it starts low (initial mu_r 50-150 for these materials), peaks at intermediate induction (maximum mu_r ~1000 for 0.9%-carbon steel against ~5000 for 99.8% iron), and falls toward 1 as saturation sets in - use low-carbon steel or better for yokes.
steel 0.9% C: mu_init 50, mu_max 1000; iron 99.8%: mu_init 150, mu_max 5000; iron 99.95%: mu_max 200,000Source quote & editorial note
Steel (0.9% C) 50 / 1000; Iron (99.8%) 150 / 5000; Iron (99.95%) 10,000 / 200,000
Beeckman, Cyclotron Magnets — ECPM37 lecture, Groningen (2009) — p. 72-73
Editorial note, tabletop extrapolation: Concrete reason to buy A36/1018 low-carbon plate rather than whatever scrap steel is on hand for an H-frame yoke.
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Give the average field a gentle radial decrease for axial focusing - the 86-inch used about 1% per 13 inches of radius (0.08%/inch) out to 20 inches, roughly 1.5% integrated, with azimuthal variation shimmed below 0.2%.
dB/B ~ -1%/13 in over the main region (~1.5% integrated to 20 in); azimuthal ripple < 0.2%Source quote & editorial note
The radial decrease in field strength is at a rate of one percent in 13 inches out to a radius of 20 inches ... These shims reduce azimuthal variations to less than 0.2%.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 15, 35
Editorial note, tabletop extrapolation: The fractional pattern transfers, not the inches: a smooth, monotonic few-percent center-to-edge fall-off with azimuthal ripple shimmed to the few-per-mille level is what the 86-inch exemplifies. The right numbers for an 8-inch pole come from its own n(r) stability requirement (dg-003, dg-119), not from this machine's profile.
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Choose accessibility-driven machine orientation early: the 86-inch's U-shaped magnet 'gives direct access to the top of the vacuum chamber and permits the use of an overhead crane for transferring the assembled dee system' - the quoted rationale.
Source quote & editorial note
The U-shape of the magnet gives direct access to the top of the vacuum chamber and permits the use of an overhead crane for transferring the assembled dee system.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 7, 9
Editorial note, tabletop extrapolation: The principle (design the yoke around how you will service the chamber, not vice versa) is directly applicable to a next machine's H-frame layout.
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Design the magnet structure for magnetic forces, which dwarf vacuum loads (ORIC: 1,055,000 lb magnetic vs 60,000 lb vacuum), and machine mating pole/yoke surfaces flat and parallel within 0.005 inch at ~125 microinch finish.
mating surfaces: plane and parallel within +/-0.005 in TIR; 125 uin finishSource quote & editorial note
a magnetic load of 1,055,000 lb and a vacuum load of 60,000 lb could be expected ... mating surfaces of pole bases and yoke pieces to be planes within 0.005 in. T.I.R.
Editorial note, tabletop extrapolation: Direct transfer of the tolerancing practice: face-grind a next machine's pole and yoke mating surfaces and check with a dial indicator. Do not transfer the load ratio: at ORIC's scale the magnetic load dwarfed the vacuum load, but magnetic pressure is B^2/(2*mu0) - at 0.5 T about one atmosphere - so on a tabletop machine the two loads are comparable and the structure must carry both.
-
Use plain low-carbon steel for cyclotron iron - the ORIC forgings ran ~0.11% C with low Si/Ni, per the report's check analysis of the delivered forgings ('well within our specifications'; the written specification itself was metallurgical and procedural - open-hearth killed steel, both pole bases from a single heat, forged alike - with no numeric composition) - and a conventional closed yoke; ORIC's pole-base to yoke cross-section ratio was 1:1.
steel ~0.11% C; A_pole_base : A_yoke ~ 1:1 (closed yoke)Source quote & editorial note
The finished magnet forgings satisfactorily met these specifications. The chemical check analysis of the steel, well within our specifications, was: C 0.110, Mn 0.330, P 0.010, S 0.030, Si 0.015, Ni 0.060
Livingston & Howard (eds.), The Oak Ridge Relativistic Isochronous Cyclotron — ORNL-2648, OSTI 4275955 (1958) — p. PDF 118 (printed -113-) for the chemistry; PDF 119 (printed -114-) for the quoted yoke sentence
Editorial note, tabletop extrapolation: Directly applicable: 1010/1018-class steel is the right iron for a next machine. On yoke sizing, the documented corridor runs from ORIC's 1:1 (pole BASE to yoke) to the +25-33% (pole FACE to return path) of dg-032 - the compared sections differ between sources, so pick one convention, apply it consistently, and check the narrowest section (dg-037).
-
Prove magnet field designs on a scale model before cutting full-size iron: ORIC used ~1/8-scale models with a rotating-coil fluxmeter on a 1/4-inch measurement grid, achieving ~0.6% RMS point accuracy.
1/8-scale model; grid 1/4 in; error budget: recorder 0.2%, position 0.4%, current regulation 0.3% -> 0.6% RMSSource quote & editorial note
Approximately 1/8-scale model magnets were energized ... A complete grid of points 1/4 in. apart is thus obtained over the entire model.
Editorial note, tabletop extrapolation: Inverted for the builder: their whole magnet is model-sized, so a dense XY Hall-probe map - grid pitch chosen from the field structure you need to resolve - is the equivalent discipline, with an error budget drawn up for YOUR instrument chain (Hall calibration, angular alignment, temperature drift, positioning, current regulation) the way ORIC drew up theirs.
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When choosing dee voltage, remember it trades against gap size: more volts require a larger breakdown clearance and thus magnet hill gap, so 'some compromise must be reached' - ORIC's compromise landed at 100 kV (their reasoning: scan re-read queued).
V_dee up -> turns down, but gap (breakdown clearance) up -> compromiseSource quote & editorial note
Increasing the dee voltage, however, requires increasing the required voltage breakdown gap and thus the magnet hill gap, so that some compromise must be reached.
Editorial note, tabletop extrapolation: The coupled optimization transfers: pick a next machine's dee voltage and magnet gap together, since dee clearance ultimately costs ampere-turns and field.
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Design beam extraction simultaneously with the magnet from the start, so the deflection scheme is built into the machine instead of being retrofitted against a finished field.
Source quote & editorial note
the design of the beam deflection system will be worked out simultaneously with the design of the magnet ... all the problems which arise from trying to obtain deflected beams after the machine is built would be avoided.
Editorial note, tabletop extrapolation: Directly applicable lesson for a next machine: if an extracted beam is ever wanted, reserve the azimuthal slot, field-edge profile, and feedthrough ports now, even if the deflector comes later.
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For coil power, dissipation is inversely proportional to conductor volume, so choose power first and volume follows; keep packing ratio above 0.5 and size cooling water as q(gpm) = 6.82 x U(kW) / dT(degF).
P = rho*(NI)^2*l_turn^2/V_Cu (V_Cu = copper volume; with gross coil volume multiply the denominator by packing factor f); packing ratio > 0.5; q(gpm) = 6.82*U(kW)/dT(degF)Source quote & editorial note
power varies inversely with volume of conductor, so to a first approximation it can be chosen at will ... a well-designed coil will have a 'packing ratio' greater than 0.5.
Livingston & Blewett, Particle Accelerators (1962) — p. 273-277
Editorial note, tabletop extrapolation: If a next machine's coils run hot, more copper is a fix on equal footing with more cooling: doubling conductor volume halves dissipation at the same ampere-turns - paid for in coil size, weight and winding-window space.
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Size the cooling plant with about 3x margin over normal load (ANL: 1000 kW capacity vs ~300 kW normal operating load).
plant capacity ~ 3x normal heat loadSource quote & editorial note
The circulating pumps and heat exchanger are sized to handle a 1000-kw heat load, with the normal operating load being about 300 kw.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 6
Editorial note, tabletop extrapolation: For a next machine dissipating 1-5 kW, real margin over normal load is what makes long runs boring - ANL carried about 3x; pick your own factor from duty cycle, ambient conditions and fouling allowance rather than copying the ratio.
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The source's water-cooled 1/4 in x 1/4 in hollow square copper conductor, properly cooled, safely carried about 120 A; they designed the magnet to run at 110 A for margin.
source rating: ~120 A when properly cooled; operated at 110 ASource quote & editorial note
When properly cooled, our 1/4''x1/4'' hollow copper conductor can safely carry up to 120A. Allowing a margin of safety, we designed our magnet to operate at 110A.
Heuer & Baumgartner, Design of a 2 MeV Cyclotron (2009) — p. 32
Editorial note, tabletop extrapolation: A conductor rating like this is conditional on the cooling that produced it - wall thickness, bore, flow, inlet temperature - so treat it as one documented data point for hollow-conductor coils, not a transferable ampacity. Rate a next machine's conductor from its own cooling calculation; the coil-geometry and magnet-power calculators cover the resistive side.
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Pick the number of turns N to match the power supply once NI is fixed by the field requirement: large-N/low-I gives cheap thin cables but higher voltage, small-N/high-I gives low voltage, better copper packing and bulky connections - and N also drags resistance, inductance, stored energy and cooling geometry along, so the supply match is the starting constraint, not the only one.
NI fixed; N chosen from supply V/I window (Diamond dipole example: 40 turns, 1500 A, 500 V circuit)Source quote & editorial note
The value of number of turns (N) is chosen to match power supply and interconnection impedances.
Marks, Conventional Magnets for Accelerators — CAS lecture (2004) — p. 35-36
Editorial note, tabletop extrapolation: The reference machine's 538 turns were set by its supply; for a next machine, pick the surplus supply first and wind N = NI_required/I_supply - then check voltage compliance, inductance (and its dump-path consequences, dg-218) and cooling before committing.
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Power-distribution cables are generally limited to a current density of about 1.5-2 A/mm^2 - the source's benchmark for what conductors carry without engineered cooling.
j (power cables) < 1.5-2 A/mm^2 (source's general figure)Source quote & editorial note
Power distribution cables... are generally limited to a current density of <1.5 to 2 Amps/mm2.
Editorial note, tabletop extrapolation: An orientation point, not a coil rating: magnet coils differ from distribution cables in bundling, enclosure and heat path. The coil-specific limits are dg-092's - voluminous enclosed coils are held to 1 A/mm^2, and water cooling is what opens the range upward.
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Choose water-cooled coil current density near the canonical j = 10 A/mm^2 (economic optimum in worked example was flatter, ~4 A/mm^2; the higher value trades operating cost for smaller, cheaper coils).
j_design ~ 10 A/mm^2 water-cooled (economic optimum ~4 A/mm^2)Source quote & editorial note
the optimum is flat and appears to be j=4 Amps/mm2. However, a higher design value (the canonical j=10 Amps/mm2 value) is generally chosen.
Editorial note, tabletop extrapolation: For a home machine the source's trade often runs toward the low end: hand-wound coils and metered power favor the ~4 A/mm^2 economic optimum, and the reference machine's tubing coil runs lower still. Window space and magnet size push the other way - which is why the canonical 10 exists - so do the two-line cost comparison for your own copper and power prices.
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Water temperature rise through a coil is dT(C) = 3.8*P(kW)/q(gpm); design for <10 C rise, and never exceed ~30 C rise (with 20 C inlet) if you want long potted-coil life.
dT[C] = 3.8*P[kW]/q[gpm] - standard water heat-capacity arithmetic in US units, not from the quote; quoted targets: < 10 C desirable, < 30 C maximum (20 C inlet) for long potted-coil lifeSource quote & editorial note
Desirable temperature rise... < 10 deg. C. Maximum allowable temperature rise (assuming 20 deg. C. input water) < 30 deg. C for long potted coil life.
Editorial note, tabletop extrapolation: One-line flow-rate calculator: a 1 kW coil on a next machine needs ~0.4 gpm for a 10 C rise.
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Wind each water circuit from one continuous length of conductor - no splices buried in the potting (the quoted requirements) - with the lecture's companion QA practices: a chip-free winding area, and a pre-winding ball test blowing a ball of <= 80% of the cooling-hole diameter through the passage (per its coil-quality pages: scan re-read queued).
ball diameter <= 0.8 * cooling-hole diameterSource quote & editorial note
A single water circuit in a coil assembly should be wound from a single continuous length of conductor. Splices 'buried' within the potted insulation should not be allowed.
Editorial note, tabletop extrapolation: For a next machine wound from copper refrigeration tubing: buy one continuous coil per water circuit, keep the shop swarf away from the winding, and verify the bore is clear before the tubing is buried in the stack.
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Dimension the coil pack with cross-section A = N*I/(j*fc), an aspect ratio (height:width) between 1:1 and 1:2, and a packing factor fc of 0.6-0.8.
A = b*c = N*I/(j*fc) - the standard winding-window equation, correct with fc as the conductor-area fraction (not from the quote); quoted ranges: c:b between 1:1 and 1:2, fc = 0.6-0.8Source quote & editorial note
An aspect ratio of c:b between 1:1 and 1:2 should be chosen, and the packing factor fc somewhere between 0.6 and 0.8.
Editorial note, tabletop extrapolation: Turns the amp-turn number into an actual coil window size before you buy tubing or start winding.
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Split coils into more parallel water circuits before enlarging the pump: pressure drop scales as 1/Kw^3 (doubling the number of circuits cuts dp by a factor of 8) and as 1/d^5 in channel diameter.
dp ~ 1/Kw^3; dp ~ 1/d^5Source quote & editorial note
This implies that for a given flow, the pressure drop is reduced by a factor of eight by doubling the number of cooling circuits.
Editorial note, tabletop extrapolation: Explains why splitting a big coil into 2 or 4 hydraulic circuits lets a garage chiller pump do the job - under the model's conditions: total flow and total conductor length fixed, circuits dividing both equally; then pressure drop falls as the cube of the circuit count. Confirm the friction regime still holds after the split.
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Convectively cooled power-distribution cables are limited to j <= 1.5 A/mm^2 - the source's figure for that service.
j_air <= 1.5 A/mm^2Source quote & editorial note
power distribution cables are convectively cooled and are limited to <= 1.5 Amps/mm2
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. 128-129
Editorial note, tabletop extrapolation: For the reference machine's circuit: any leg - bus, jumper, lead - running above ~1.5 A/mm^2 without an engineered cooling path will run warm, so size leads generously. Above the line the options are any real cooling: water, forced air, conductive sinking, or intermittent duty with temperature monitoring (dg-220).
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Use the source's normally-good current density j = 10 A/mm^2 for water-cooled magnet coils and a packing fraction of ~0.5 for small conductors; the lecture's first-pass sizing also takes average turn length ~3x the magnet core length.
j = 10 A/mm^2 (water-cooled); f ~ 0.5; l_ave ~ 3*L_magSource quote & editorial note
Normally, a good value for the current density is j = 10 Amps/mm2 for water cooled coils... The value of the packing fraction is typically f ~ 0.5 for small conductors.
Editorial note, tabletop extrapolation: Lets the builder size a next machine's coil cross-section on one sheet of paper: gross winding area ~ NI/(j*f) = NI/5 mm^2 for water-cooled copper - a first pass the thermal calculation then confirms, and the 10 A/mm^2 presumes genuine water cooling (dg-092's geometry conditions).
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Design coil water circuits for turbulent flow (the lecture's Re >= 4000 criterion) but keep flow velocity <= 4 m/s to avoid vibration and erosion of the copper passage, and hold coil temperature rise dT <= 30 C to protect epoxy insulation - the lecture tightens toward ~15 C where field stability matters.
Re >= 4000; v <= 4 m/s; dT <= 30 C (15 C for stability)Source quote & editorial note
Flow velocity should be high enough so that the flow is fully turbulent, Re ≳ 4000... For synchrotron radiation accelerators where beam stability depends on temperature stability, ∆T ≲ 15°C.
Tanabe, Iron Dominated Electromagnets: Design, Fabrication, Assembly and Measurements — SLAC-R-754 (2005) — p. PDF pp. 134-135 = printed pp. 134-135 (chapter section 'Coil Cooling'), as cited
Editorial note, tabletop extrapolation: Direct water-cooling design window for a next machine's hollow-conductor coil; also warns that a lazy laminar-flow circuit cools far worse than the handbook film coefficient suggests.
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Estimate the coil power-weight tradeoff with kW x tons = 0.118 x (mega-ampere-turns)^2 x (mean turn length in inches)^2 for copper: the product of dissipation and weight is fixed by NI and geometry, so more copper always buys less heat.
kW x tons(Cu) = 0.118 x (MA-turns)^2 x (mean turn length in inches)^2 - the squared length follows from P*M ~ (NI)^2*l^2 and matches the 0.118 coefficient; the quoted line's missing exponent is likely transcription (scan re-read queued)Source quote & editorial note
Kilowatt-Tons = (0.118)Cu (Mega-ampere turns)^2 (inches mean turn length)
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 13
Editorial note, tabletop extrapolation: Directly applicable trade study tool: the product of coil dissipation and coil weight is fixed by NI and geometry, so more copper always buys less heat.
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Wind coils to an approximately rectangular (square-ish) cross section around the poles; a coil that is too flat or too tall intercepts more leakage flux and wastes turns.
Source quote & editorial note
The coils should be wound so that they occupy approximately a rectangular cross section around the poles ... Either too flat or too tall a coil intercepts more leakage flux and thus wastes turns.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable guidance for a next machine's coil geometry.
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Limit close-wound naturally air-cooled coils to 750 A/in^2 of conductor continuously, 1000 A/in^2 for intermittent runs.
J <= 750 A/in^2 (1.16 A/mm^2) continuous, air-cooled; <= 1000 A/in^2 intermittentSource quote & editorial note
operate close-wound naturally air-cooled coils at a current density not exceeding 750 amps per square inch of conductor area. For intermittent operation this may be raised to 1000 amps per sq. in.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable thermal sizing for coils matching the quoted conditions - close-wound, naturally air-cooled: 750 A/in^2 continuous, 1000 intermittent. A different winding style (open spacing, forced air, tubing with internal flow) carries different limits - dg-092's geometry table is the map.
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Favor large conductor cross-section and high current over many turns at high voltage; this simplifies both insulation and winding.
Source quote & editorial note
Most coil designs favor large conductor areas and correspondingly high amperages; this reduces total voltage and simplifies both the insulation and the winding problems.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 3
Editorial note, tabletop extrapolation: Directly applicable when choosing wire gauge and supply for a next machine's coils.
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Estimate dee capacitance by summing parallel-plate sections of the dee-to-chamber geometry - the memo's three-section sum gave 77.5 pF calculated (70.5 pF top+bottom, 7.04 pF edge) against the quoted 78.1 pF measured on an L-C meter: 'Nice agreement seen!'
C_total = 2*A_top*eps0/d_top + A_edge*eps0/d_edge; Rutgers: 70.5 pF (top+bottom) + 7.04 pF (edge) = 77.5 pF vs 78.1 pF measuredSource quote & editorial note
C_top+bottom = 2C = 70.5 pF ... C_edge = 7.04 pF ... For a total C of: 77.5pF. Measurement of the capacitance with an L-C meter yields a value of 78.1pF. Nice agreement seen!
Koeth, Theoretical Calculations and Measurements of the DEE Voltage in the Rutgers 12 Inch Cyclotron (2005) — p. PDF 1 (page 1 of the September 2005 Koeth memo) as cited
Editorial note, tabletop extrapolation: Directly usable on the reference machine's 8-inch dee: sum simple parallel-plate terms for top/bottom/edge and verify with a cheap L-C meter before winding the tank coil.
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Peak-to-peak dee voltage of an inductively coupled tank follows Vp-p = 2*sqrt(2*P*L/(Rs*C)), i.e. it scales as the square root of forward power; the square-root trend held over all measured power ranges (5 W to 1300 W).
Vp-p = 2*sqrt(2*P*L/(Rs*C)); Vpeak = sqrt(2*P*L/(Rs*C))Source quote & editorial note
the trend of DEE voltage to follow the square root law of the input RF power is accurate over all measured power ranges
Editorial note, tabletop extrapolation: The sizing equation for the reference machine's LDMOS upgrade - with P as the power actually DELIVERED to the tank: at a good match forward power approximates it; otherwise net out the reflected fraction first. Doubling dee voltage costs 4x power, so 1.3 kV to 5-13 kV needs a 15-100x power increase unless L/C or Rs improves (dg-239's knobs).
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Do not budget a tank's effective series resistance from the coil alone: the Rutgers coil computed ~50 mOhm (1.3 mOhm/inch of 1/4-inch Cu tube), but the assembled system behaved 'as if Rs had the value of 800 mOhm' - an INFERRED effective series resistance sixteen times the coil's, which the memo attributes to the stainless chamber return, the stainless Conflat stem support, and the feedthroughs.
Rutgers: Rs_coil ~ 0.05 ohm estimated, Rs_system 0.8 ohm measured (16x). The factor is specific to that return path, stem, feedthroughs and frequencySource quote & editorial note
as if Rs had the value of 800mOhm - sixteen times that of the expected coil Rs ... take into account the stainless steel vacuum chamber return, the stainless steel Conflat DEE stem support and RF feed throughs.
Editorial note, tabletop extrapolation: When predicting a next machine's dee voltage, include every RF current path - chamber return, stem, feedthroughs, contacts - and prefer copper returns where possible; then measure the assembled tank's Q and infer Rs from it rather than assume a multiplier. [Note revised 2026-08-23: earlier note told the builder to 'expect ~1 ohm scale Rs', a number that belongs to Rutgers' geometry.]
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For a given RF power the only knobs that raise dee voltage are minimizing Rs or increasing tank inductance L while decreasing dee capacitance C to hold the resonant frequency.
Vp-p = 2*sqrt(2*P*L/(Rs*C)) => maximize L/C ratio, minimize Rs at fixed f0 = 1/(2*pi*sqrt(LC))Source quote & editorial note
minimizing Rs, or increasing L2 while simultaneously decreasing C2 (to maintain the resonant frequency) are the only parameters that can be adjusted to increase the DEE voltage for a given amount of RF power.
Editorial note, tabletop extrapolation: For a next machine, shrinking dee-to-liner capacitance (larger dee-to-lid spacing) and a bigger low-loss coil raise dee voltage before amplifier watts do - bought, not free: more L usually brings more conductor and more Rs, and dee-to-lid spacing spends the magnet-gap budget (dg-163). Optimize the L/C-versus-Rs package together, then buy watts.
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Electric gap focusing helps only in the first few turns and only for ions crossing while the RF field is DECREASING; separately, the practical phase migration for an accelerated ion runs from zero to -pi/2 and back - one half-cycle of total excursion, the quote's limit.
phase focusing quadrant: field decreasing during transit; total phase excursion ~pi radians; internal targets tolerate up to ~3*pi/2Source quote & editorial note
the practical maximum migration in phase will be from zero to -pi/2 and back to zero, a total phase migration of pi radians or one half-cycle.
Livingston & Blewett, Particle Accelerators (1962) — p. 166-171
Editorial note, tabletop extrapolation: With a 3-4% field droop and 160 turns-scale acceleration, the reference machine's dee voltage sets how much phase slip they can afford: higher V = fewer turns = more field-shape tolerance.
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Raising dee voltage is the standard lever for marginal resonance - fewer turns, more phase-slip budget - but it trades against spark breakdown and RF power, and it cannot fix a frequency mismatch or an unsuitable field profile; most machines end up accepting a slightly smaller exit radius and energy to keep intensity.
N_turns ~ T_final/(2*e*V_dee); minimum V_dee vs energy and field droop delta per Cohen (Fig. 6-25)Source quote & editorial note
Increasing the D voltage requires fewer turns for acceleration to maximum energy and will compensate for a larger phase shift. However, D voltage is usually limited by ... power and spark breakdown.
Livingston & Blewett, Particle Accelerators (1962) — p. 172
Editorial note, tabletop extrapolation: At ~1.3 kV and ~150 keV the reference machine's ions make ~60 turns; doubling dee voltage halves turns and dramatically relaxes both field-uniformity and vacuum (scattering) requirements.
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Livingston & Blewett's oscillator practice: feed the dees through quarter-wave resonant lines (dee on the inner-conductor end), drive push-pull, and watch the push-push mode - with the quoted only-general-rule on parasitics: the simpler the structure and the shorter the leads, the fewer the parasitics.
f_pushpull = 1/(2*pi*sqrt(L(C+2C'))); push-push mode has higher Q and no dee-to-dee voltageSource quote & editorial note
The resonant circuit is electrically equivalent to a pair of quarter-wave coaxial transmission lines with the D's supported on the ends of the inner conductors. ... two power tubes in push-pull and two coupling loops is the more common arrangement.
Livingston & Blewett, Particle Accelerators (1962) — p. PDF pp.185-187 (printed pp.169-171)
Editorial note, tabletop extrapolation: If a next machine goes two-dee push-pull, watch for the push-push mode (no dee-to-dee voltage, oscillator happily locked); a single-dee-plus-dummy design sidesteps that mode entirely - one reason small machines favor it.
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Anticipate the blue-glow multipactor discharge: it clamps dee voltage to a few hundred volts, heats surfaces and liberates gas, and only fast pumping plus continued outgassing (and an oscillator that can drive through it) breaks the cycle.
Source quote & editorial note
This loading of the D circuit by discharge currents holds the D potentials down to a few hundred volts ... Unless the loading is removed, the chamber will continue to operate in the low-voltage, blue-glow discharge condition indefinitely.
Livingston & Blewett, Particle Accelerators (1962) — p. 188
Editorial note, tabletop extrapolation: The reference machine's dee operates in the range where these discharge phenomena live: the ~100 V-class multipactor band is crossed at every start, and blue-glow gas discharge appears when pressure and surfaces allow. Surface conditioning, low pressure, and drive that can snap up fast are the standard escapes - and whether a given stall is multipactor or gas discharge is diagnosed, not assumed (dg-1273).
Cited in: The Vacuum Budget of a Cyclotron
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Prefer a self-excited oscillator closely coupled to the high-Q dee circuit, so frequency follows dee warping and loading automatically; the grounded-anode push-pull variant with crossed neutralizing capacitors is, in the book's account, simple, compact, and free of delicate tuning requirements - the quoted advantages.
Illinois 42-in: two '880' tubes, ~60 kW total input; grounded-anode, cross-neutralized, low-Q grid coilSource quote & editorial note
The most significant advantage of this circuit is its simplicity and compactness along with the freedom from delicate tuning requirements or precise construction.
Livingston & Blewett, Particle Accelerators (1962) — p. 190-193
Editorial note, tabletop extrapolation: The same logic favors a drive that follows the dee on the reference machine: self-excited, or a PLL tracking the resonator - similar in spirit though not identical in dynamics, since a PLL adds its own loop behavior. Either way, mechanical drift retunes the drive instead of killing the beam.
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Set the RF frequency slightly below the central-field cyclotron frequency but above the edge-field value - the quoted window for a declining field; the phase error then migrates one way and back across the acceleration (dg-571's phase-turnaround strategy is the professional form of the same move).
f_edge < f_rf < f_centerSource quote & editorial note
apply a radio frequency oscillating voltage to the electrode that is slightly less than the cyclotron frequency given at the center of the field, but greater than [that] near the edges.
King, A Preliminary Design for a Small Permanent Magnet Cyclotron — Houghton College thesis (2002) — p. 20
Editorial note, tabletop extrapolation: A concrete tuning rule for the builder: do not tune RF to the central field alone - place it inside the quoted window and find the best point empirically by beam current; the phase-history reasoning is the theory behind the knob, not a substitute for turning it.
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Use one driven dee against the grounded chamber wall (dummy dee) instead of two dees: it halves the RF feedthrough count and the whole chamber becomes the return electrode - the standard simplification for small machines.
Source quote & editorial note
it has one dee-shaped copper electrode, and the grounded vacuum chamber functions as the other electrode
Editorial note, tabletop extrapolation: The reference machine already does this, and it stays attractive for a next machine - one HV feedthrough fewer, the chamber as return electrode - unless push-pull two-dee RF is wanted for higher energy gain per turn. A common choice among documented small machines, not a rule.
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Iowa State's dee geometry: thin sheet-copper dees 22.5 cm in diameter and 2.4 cm high, separated by a 1.5 cm gap and water-cooled through the supporting stems - about 0.89 of their pole diameter.
dee dia 22.5 cm vs 25.4 cm pole face (0.886); dee height 2.4 cm; dee-dee gap 1.5 cmSource quote & editorial note
The dees, made of thin sheet copper, arc 22.5 cm in diameter, 2.4 cm high, and they are separated by a gap of 1.5 cm.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 7
Editorial note, tabletop extrapolation: A documented dee geometry near the reference machine's scale - note it exceeds an 8-inch pole, so it fits 10-inch-class machines as-is: scale the proportions, not the dimensions. Dee cooling need tracks the dissipated RF power and construction, not a fixed kilowatt line: compute it from the RF budget (dg-313) and watch dee temperature during commissioning.
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Budget extraction realistically: the Argonne 60-inch extracted about 30% of the internal beam at the exit radius, and the quoted efficiency figure ran 10% at 120 uA of deflected deuterons, rising to 15% at 200 uA.
extraction ~30% of internal beam; beam power / RF DC input ~ 10-15%Source quote & editorial note
This value is about 10% for 120 uamp of deflected deuterons, increasing to 15% for a 200 uamp beam. About 30% of the internal beam at the exit radius is extracted.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 19
Editorial note, tabletop extrapolation: Sets expectations if a next machine attempts a deflector: capturing a third of the circulating beam was a mature machine's result, so plan around numbers of that order - and account for where the rest goes (septum heating, sputtering, and at higher energies activation), rather than booking the loss as free.
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Set the extraction gap by the empirical vacuum-breakdown limit d[mm] >= 1.41e-2 * U[kV]^1.5 (clean flat surfaces): 10 kV needs >=0.45 mm, 30 kV >=2.3 mm, 50 kV >=5 mm; smaller gaps arc, much larger gaps waste extraction field.
d[mm] >= 1.41e-2 * (U[kV])^(3/2)Source quote & editorial note
The voltage breakdown limit determines the necessary gap width. The empirically determined limit (valid for clean, flat surfaces) is d[mm] >= 1.41 x 10^-2 * phi[kV]^(3/2).
Wolf (ed.), Handbook of Ion Sources (1995) — p. 379
Editorial note, tabletop extrapolation: Direct rule for source-to-puller spacing - clean DC gaps are the law's home turf: a few-kV gap needs sub-mm minimum, with real margin because sputtered metal films spoil the 'clean surface' assumption fast. For dee-to-ground RF clearances use it only as a lower-bound sanity check: edges, insulators, RF conditioning and enhancement move the practical limit (dg-353, dg-662).
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Estimate turn number as N = T_final/(n_gaps*V0*sin(phi)) and turn spacing as dr/dN ~ r*(T1/T); low energy gain per turn means thousands of turns and micron-scale outer-orbit separation, which is what makes extraction hard.
N = T/(n*V0*sin(phi)); dr/dN ~ r*dT_turn/(2T) nonrelativistically (exactly r*(T+mc^2)/(T*(T+2mc^2))*dT_turn); source's example: 250 MeV at 17 keV/turn -> N ~ 15,000, spacing ~ 20 umSource quote & editorial note
250 MeV protons; 17 KeV/turn: N~15,000... 250 MeV protons r=0.3m: dr/dN ~ 20 microns!
Antaya, Cyclotron Basics — MIT 8.277, Unit 10, Lecture 14 (2010) — p. 43
Editorial note, tabletop extrapolation: For the builder: 1 MeV at 2 kV per gap (2 gaps) is ~250 turns with final-orbit spacing ~0.25 mm at r = 12 cm - which is why higher dee voltage directly eases both extraction and vacuum requirements.
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A single real dee working against its image in a grounded plate is a working small-machine RF architecture - the quoted machine's arrangement, tuned by physically twisting the inductor onto the cyclotron frequency; its commercial-amp drive chain is the same paper's setup (dg-118; chain details: scan re-read queued).
f = 1/(2*pi*sqrt(LC)), C fixed by dee geometry, L adjusted (deformable coil) to tuneSource quote & editorial note
The second DEE has been faked using the image of the real DEE on a grounded conductor ... By twisting the inductor, we can change the inductance to match our inductance requirements.
Chun, The Cyclotron Magnet and RF Oscillator (2003) — p. 11
Editorial note, tabletop extrapolation: This is the reference machine's exact topology, in use on a comparable documented machine; the deformable-inductor trim is a simple tuning mechanism worth copying on a next machine.
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Use single-dee construction (the grounded tank is the other 'dee') to simplify tank and oscillator; add a symmetric grounded dummy-dee edge for better ion focusing only after the machine works.
Source quote & editorial note
the 'single-dee' construction; this has many advantages ... Better ion focussing can be obtained by installing a 'dummy' grounded dee edge symmetric to the insulated dee, but this is a refinement
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 8
Editorial note, tabletop extrapolation: Exactly the reference machine's architecture. The dummy-dee edge is the source's named refinement for better ion focusing - a natural next-machine upgrade once the basic machine works, which is the sequencing the source itself implies ('but this is a refinement').
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Wouters recommends a grounded-grid self-excited oscillator arrangement for confining RF currents to intended paths, and - the quoted requirement - the dee-to-ground capacitance must be counted as the major portion of the tank-circuit capacitance (his circuit trims frequency with a small parallel capacitor; circuit details: scan re-read queued).
C_tank ~ C_dee-ground + C_trim; step-up by tapping plate down the coilSource quote & editorial note
The dee-to-ground capacity appears as the major portion of the capacitance in the tank circuit, which must be calculated taking this into account
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 8
Editorial note, tabletop extrapolation: Even with a modern solid-state chain, the builder must treat dee capacitance as the resonator's dominant C when designing the matching network; the confine-the-RF-current lesson is timeless.
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Provide short, broad RF ground paths, especially in the ground circuits, and keep the tube close to the tank but out of the magnetic field (the quoted requirements); Wouters' specific construction - the tube through a large hole in a copper ground sheet extended to the tank wall - is his implementation (scan re-read queued).
Source quote & editorial note
it is important to provide short, broad paths for current flow, especially in the ground circuits ... While the tube should be placed as close to the tank as possible, it must yet be kept away from the magnetic field
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 8-9
Editorial note, tabletop extrapolation: Directly applicable to the reference machine's amplifier: wide copper sheet or strap grounds and a short feed run, with magnetically SENSITIVE parts kept out of the fringe field - the tube in the quote; in modern gear whatever actually cares (fans, ferrites, meters - dg-670's shield-or-relocate).
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Treat the cyclotron's hazardous supply voltages as deadly — 'proper precautions must be taken, even during preliminary testing': interlock switches on power-supply covers, grounding hooks by the machine, and a well-grounded copper screen box around the oscillator, which also keeps its RF out of the other circuits — all one safety paragraph.
Source quote & editorial note
The voltages employed on the various cyclotron components are deadly; proper precautions must be taken, even during preliminary testing ... Interlock switches on the power supply covers and grounding hooks
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 9
Editorial note, tabletop extrapolation: Directly applicable home-lab safety baseline for the HV systems of a next machine - covers interlocked, hooks in reach, and the full discharge discipline around them (dg-522).
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Thin chamber lids over a wide flat span bow inward under vacuum, changing dee capacitance (detuning the RF) and reducing flashover voltage - the source machine tack-welded internal support posts under its lids to stop it.
the source machine's case: 3/16-in lids over a ~2 ft span bowed enough to need postsSource quote & editorial note
the top and bottom of the chamber to bow in, which affected the capacitance of the dee and reduced the maximum voltage that the dee could withstand before flashing over.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2
Editorial note, tabletop extrapolation: Directly relevant to any thin-lid chamber on a next machine squeezed into a small magnet gap: design the lids to a calculated stiffness (the lid-deflection calculator) from the start. Internal posts clear of the beam spiral and the RF high-field region are one remedy; thicker or dished lids and external ribs are others, and each needs its own deflection, buckling, venting and weld checks. [Note revised 2026-08-23: earlier note planned posts as the remedy.]
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A single dee plus grounded dummy dee doubles the required dee-to-ground voltage compared to two dees, but reduces RF feedthrough cost and complexity (two become one) - often the right trade at amateur scale. [Corrected 2026-08-23: 'the right trade' was stated without the 'often'.]
1 dee: V_required x2, feedthroughs /2Source quote & editorial note
Having only one dee rather than two doubles the voltage requirement, but reduces the cost and complexity of having two RF feedthroughs in the vacuum chamber.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2
Editorial note, tabletop extrapolation: Supports the single-dee choice for a next machine unless attainable dee voltage, insulation or the coupling scheme becomes the binding constraint.
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A tabletop cyclotron RF chain can be assembled from commercial units - the Houghton chain: function generator (HP 33120A) -> RF power amp (ENI 155LCRH) -> ham autotuner (LDG AT-200PC) -> Bird 43A wattmeter -> dee - with fr = 1/(2*pi*sqrt(L*C)) as the first-cut resonance estimate for the tuned circuit.
fr = 1/(2*pi*sqrt(L2*C))Source quote & editorial note
HP 33120A Function Generator - ENI 155LCRH Power Amp - LDG AT-200PC Tuner - Bird 43A RF Power Meter - Dee
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 12-14
Editorial note, tabletop extrapolation: Essentially the reference machine's current architecture. A ham antenna tuner can match a dee-shaped load in this frequency range - but its voltage ceiling is construction- and tuning-dependent: expect the ~kV class rather than the 5-13 kV a dedicated resonator supports (the LDMOS upgrade path), and MEASURE the dee voltage (dg-quoted methods in the dee-coupling deep dive) instead of inferring it from the tuner's rating.
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Through an autotuner chain, tens of watts yields low-kV dee voltage: Houghton reported 1700 Vpp from 26 W and 800 V from 10 W at ~3.5 MHz. [Corrected 2026-08-23: earlier text called the two points 'roughly consistent with sqrt(P) scaling'; they are not (ratio 2.1 vs 1.6 expected), and the 800 V figure's convention (peak, peak-to-peak, RMS) is not preserved in the source.]
26 W -> 1700 Vpp; 10 W -> 800 V (convention unstated). sqrt(P) scaling holds only at unchanged coupling and loaded Q; these points differ from it by ~30%Source quote & editorial note
3.55 MHz 1700 Vpp (26 W) ... 3.48 MHz 800 V (10 W)
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 17-19
Editorial note, tabletop extrapolation: A benchmark for the order of magnitude the reference machine's autotuner path reaches (its ~1.3 kV from a 5 W amplifier is in the same band), not a curve to read values off: state the voltage convention, tuning and loading before comparing, and do not infer a plateau from two points.
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Low dee voltage caps the usable field and energy through orbit count: at 800 Vpp, no beam peaks appeared for fields above ~0.5 T, where reaching full radius takes more than the ~44 orbits that worked - consistent with turn-count-limited survival at their pressures (the quote reports the disappearance; the survival reading is the team's interpretation).
N_orbits = T_final/(e*Vpp); 35 keV / 800 eV ~ 44 orbits was the practical survival limitSource quote & editorial note
No peaks for magnetic fields larger than H2+ at 0.5 T -> 35 keV; 44 orbits at 800 Vpp
Yuly et al., Modifications on the Houghton College Cyclotron (2010) — p. 21
Editorial note, tabletop extrapolation: Quantifies why the reference machine's dee-voltage upgrade matters: at 1.3 kV their protons need ~hundreds of turns to reach interesting energies, and ~44 turns was already the survival ceiling at Houghton's pressures.
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Use a resonant tank because Q = wL/Rac multiplies stored voltage for modest power, and the highest dee voltage for a given forward power occurs at critical coupling, where Qloaded = Q0/2.
Q = omega*U_stored/P_loss (the slide's Q = wL/R_AC is the series-equivalent form); highest dee voltage for given forward power at critical coupling: Q_loaded = Q0/2 (the quoted condition)Source quote & editorial note
To develop high voltages with modest RF power. The highest voltage for given power occurs when: Qloaded = 1/2 Qo
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 18
Editorial note, tabletop extrapolation: The one-slide justification for the builder to move from an antenna-tuner match to a true high-Q tank circuit in a next machine.
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Rutgers' record operating point: 2 kW forward power produced 8.4 kV peak dee voltage on the 12-inch machine (measured via calibrated pickup and Bird thruline wattmeter).
2 kW -> 8.4 kV peak (~16.8 kVp-p)Source quote & editorial note
Record Input Power 2kW: 8.4 kVpeak
Koeth et al., The Rutgers 12-Inch Cyclotron for Students (2010) — p. 19
Editorial note, tabletop extrapolation: Anchors the power budget with one measured point: 2 kW bought 8.4 kV peak on that 12-inch tank. Scaling to the reference machine's planned LDMOS runs through ITS shunt impedance (dg-313's formula with measured Q and C): at comparable impedance, 500 W supports roughly 1/2 the voltage (P ~ V^2), a ~4 kV class - measure, then budget.
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Vacuum surface flashover is set by the insulator material, not the electrodes: over a 2.2-cm butt-jointed cylinder, stainless+Pyrex held 100 kV while copper+Pyrex held only 44.5 kV and most ceramics 40-50 kV - which works out to roughly 2-4.5 kV/mm of creepage on that fixture, and breakdown stress falls further for longer insulators.
2.2-cm insulator in vacuum: SS/Pyrex 100 kV; Cu/polystyrene 75 kV; Cu/Teflon 50 kV; Cu/steatite 50 kV; ~2-4.5 kV/mm creepage, sublinear with lengthSource quote & editorial note
Gleichauf also found that the breakdown voltage was strongly dependent on the material of the insulator but independent of the material of the electrodes.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 113-114
Editorial note, tabletop extrapolation: The source's fixture works out to 2-4.5 kV/mm of creepage - a first sanity check for an extraction stalk, not a design allowable: flashover depends on triple-junction geometry, finish, contamination and conditioning, and does not scale linearly with length (the source's own longer insulators held less per mm). Size real hardware by test, with margin.
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Never leave a thin gas/void gap in series with a solid dielectric: the field in the void is multiplied by the solid's dielectric constant k (stress ~ V*k/d for a thin gap), so it sparks first -- fill every gap between conductor and insulator with a compatible potting or liquid dielectric.
E_gap = V*k/(d + x*(k-1)) -> V*k/d for thin gap x << d; grading works: graded bushing held 1 MV over 30 cm vs 0.6 MV over 90 cm conventionalSource quote & editorial note
Air spaces exist in solid and liquid dielectrics... the air will have the higher stress, possibly causing sparkover through the air space... The stress in the air gap can thus be k times that in the solid.
Miley & Murali, Inertial Electrostatic Confinement (IEC) Fusion: Fundamentals and Applications (2014) — p. 116, 119
Editorial note, tabletop extrapolation: The classic failure of home-built HV feedthroughs: a loose PTFE sleeve over a rod arcs in the annular air film. Fill the gap - potting or liquid dielectric - so no gas layer sits in series with the solid. Evacuating the annulus removes the Paschen path but leaves field-emission breakdown and surface flashover, so vacuum is not a substitute for filling.
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Trade focusing against phase slip explicitly: you may drop Bz at large radius for extra focusing only if the ions have few turns left there, so raise the Dee voltage to cut the number of revolutions - fewer turns also means shorter path length and fewer gas collisions.
Source quote & editorial note
The axial component of the magnetic field can be decreased at larger radii in order to increase the radial (focusing) component, provided the ions only have a few revolutions left once they reach this portion of the field.
Morrow, Focusing in the Houghton College Cyclotron — Houghton College thesis (2015) — p. 27-28
Editorial note, tabletop extrapolation: One candidate for the reference machine's next big win: at ~150 keV on a low Dee voltage the turn count is large, and cutting it relaxes both the phase budget and gas-scattering exposure. Whether Dee voltage or field shaping pays more on a given machine is a diagnosis - measure what actually limits the beam first; the quote's own condition is narrower: late-radius focusing tricks need few turns remaining.
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Raise dee voltage to raise beam current: fewer turns to a given radius means less path length and fewer gas collisions, and measured current increased with dee voltage at fixed field and pressure.
N_turns ~ E_final/(2*q*V_dee); higher V_dee -> shorter path -> higher transmitted currentSource quote & editorial note
It can be seen that in general, an increase in dee voltage results in a higher beam current.
Editorial note, tabletop extrapolation: For a fill-gas machine, dee volts are a strong current knob - the measured trend here: fewer turns, less path, fewer collisions. Whether they are THE binding knob depends on what limits the machine that day: source output, pressure, phase acceptance and detuning all compete (dg-359, dg-525). Measure before spending.
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Houghton's autotuner-matched dee circuit measured Q = 16.1 (f0/dF = 3.55/0.22 MHz; their earlier chamber measured 22) - far below the Q a directly coupled copper tank can reach.
Q = omega0/delta-omega_FWHM = 3.55/0.22 = 16.1Source quote & editorial note
the quality factor of the Houghton College cyclotron was determined to be Q=16.1. The previous chamber and dee constructed in 2006 had a quality factor of 22.
Editorial note, tabletop extrapolation: Quantifies the architecture choice: the reference machine's antenna-tuner match delivers kV-class dee voltage at low measured Q, and multi-kV wants a high-Q tank coil. The caveat travels: a low measured LOADED Q reflects the whole coupled system, matching-network losses included - so measure Q on the actual assembly and compare loaded with loaded when weighing the upgrade.
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The paper's machine oscillates the Dee at amplitudes up to approximately 3000 V against the grounded dummy Dee, and normal operation takes 10-40 W of RF - two statements about the same tank (its maximum and its routine point), not a measured pairing of the two.
10-40 W forward RF -> up to ~3 kV Dee amplitude; typical running 2100 VppSource quote & editorial note
the Dee may be oscillated with voltage amplitudes of up to approximately 3000V relative to the grounded Dummy Dee ... For normal operation, 10-40 W of RF power are required
Editorial note, tabletop extrapolation: Tells the builder that Dee voltage is a tank-Q problem, not a brute-force power problem: a modest amplifier into a good resonator beats a big amplifier into a lossy one - and dg-313's formula computes the actual watts-per-kV pairing for any target.
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Operate at as low an RF frequency as other constraints allow - ORNL's 1950s reasoning: far more oscillator engineering information existed below 15 megacycles.
prefer f < ~15 MHz where B and size permitSource quote & editorial note
It was believed desirable to operate at as low a frequency as possible because of the larger amount of engineering information available for oscillators in the region below 15 megacycles/sec.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 15
Editorial note, tabletop extrapolation: The reference machine's 9 MHz benefits from the modern form of the same effect: HF amateur-radio technique and parts are abundant below ~30 MHz. Today's sweet spots follow ham bands and ISM frequencies rather than a 15 MHz line; the transferable point is choosing field and frequency where the RF art is cheap.
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Budget dee excitation power from P ~ pi*f*C*V^2/Q with V the PEAK dee-to-ground voltage: the 86-inch's measured curve gave 96 kW of RF for 400 kV dee-to-dee with C = 176 pF, f = 13.5 MHz, loaded Q = 3700 (unloaded 12,300). [Corrected 2026-08-23: the earlier text did not say which voltage it meant, and the two readings differ by a factor of four. With those parameters the formula gives ~81 kW for 200 kV dee-to-ground (400 kV dee-to-dee, the source's figure, in sensible agreement with the measured 96 kW) and ~323 kW if 400 kV is read as dee-to-ground. State the convention, and peak versus RMS, every time this formula is used.]
P = pi*f*C*V_pk(dee-to-ground)^2/Q: with Q = unloaded Q0 this is resonator wall dissipation; with loaded Q_L it approximated the 86-inch's total RF input at their coupling (measured 96 kW vs 81 computed). For amplifier sizing use Q0 for the walls, then add coupling and beam losses and margin. 86-inch: f = 13.5 MHz, C = 176 pF, Q_loaded = 3700 (unloaded 12,300), V = 200 kV per deeSource quote & editorial note
This curve indicates that 96 kW of rf power is required for exciting the dees to 400 kv. ... The oscillator input was 162 kw.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 16, 25
Editorial note, tabletop extrapolation: Formula transfers once the conventions are fixed: at 9 MHz, ~50 pF and unloaded Q ~ 1000, 5 kV peak dee-to-ground dissipates ~35 W in the resonator - tens of watts, the FLOOR an amplifier must clear with margin for coupling loss, detuning and arcs. Double the voltage, four times the power.
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There is a calculable minimum (threshold) dee voltage to reach a given energy in a given field profile; design the RF system to exceed it with margin rather than discovering it empirically.
V_dee,min = f(E_final, B(r) profile); see ORNL-1196 Fig. 4 / Y-757Source quote & editorial note
It is possible to calculate the various effects quantitatively and to predict the minimum dee voltage required to obtain a given energy in a particular cyclotron.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 17-19
Editorial note, tabletop extrapolation: Directly applicable design step for a next machine: compute threshold voltage for the target energy and field taper before freezing the RF chain power budget.
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Expect gross RF-to-beam efficiency in the few-percent range: the 86-inch measured 2.6-12.5% gross (beam kW over oscillator DC input) and 30-44% counting all accelerated ions, with efficiency rising with dee-to-dee potential and beam power - the quoted trend. [2026-09-06 erratum, scan re-read: the gross span previously read 2.6-9.3%; Table I's beam-power test measured 12.5% (41.7 kW calorimetered on 333 kW input), and 9.31% is only Table II's maximum. Net figures 30.2/41.8/44.2% confirmed.]
gross eff = beam kW / oscillator DC input kW; 86-inch: 2.6-12.5% gross (Table I) and 5.86-9.31% (Table II), rising with V_dee and beam power; net 30.2-44.2%Source quote & editorial note
As measured, efficiency tends to increase with dee-to-dee potential and with beam power.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 24-26
Editorial note, tabletop extrapolation: The order of magnitude transfers as expectation-setting: most RF power goes to resonator and ion-loading losses, so size a next machine's RF from resonator dissipation (dg-313), not from beam power.
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Bias the dees negative - insulated, DC-biased dees were the 86-inch's cure for oscillator starting difficulties due to ion loading - so the self-excited oscillator starts cleanly.
insulated dee + negative DC bias, interlocked to RF (magnitude tuned in commissioning)Source quote & editorial note
Oscillator starting difficulties due to 'ion loading' are avoided by the use of insulated negatively-biased dees.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 7, 47
Editorial note, tabletop extrapolation: Directly applicable if a next machine's RF start-up stutters or the dee glows at low voltage: insulate the dee for DC and feed a negative bias through an RF choke. The same lever also bears on multipactor (dg-324), which lives in the same low-voltage start regime. The source records the method; the bias magnitude is found on the machine.
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MAXIMUM energy gain per dee crossing is q*2*V0*sin(N*theta/2) for dee angular width theta at harmonic N - the particle's phase only reduces it - so half-dees and cut-away lips tax energy gain, and the tax grows with harmonic number.
dE_max per crossing = q*2*V0*sin(N*theta/2); actual gain carries the particle phase on topSource quote & editorial note
the maximum voltage gain/dee is Vd = 2*V0 sin(theta/2); for particles rotating on subharmonics of the dee frequency the angular width of the dee is n*theta to the particle
Editorial note, tabletop extrapolation: Directly applicable when trimming a next machine's dee for probe or source clearance: keep the dee close to 180 degrees or compute the sin(N*theta/2) penalty for the harmonic in use. Fundamental-mode trims are gentle - 15 degrees off costs about 1% at N = 1 - but the same trim costs more at higher harmonics.
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High dee voltage at practical drive power comes only from a high-Q resonant circuit - the quote; ORIC's implementation treats the dees and stems as a quarter-wave line foreshortened by dee capacitance, tuned via C, stem length, or stem impedance - the report's model, common for stem-fed dees though not universal.
dee system = lambda/4 line foreshortened by C_dee; tune via C, l, Z0Source quote & editorial note
The high dee voltage required in cyclotrons can be achieved for practical driving power only by using a high-Q resonant circuit.
Editorial note, tabletop extrapolation: Directly applicable framing for the reference machine's matching network: every dB of resonator Q lost to bad joints or lossy insulators is paid in amplifier watts.
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If multipactor blocks RF turn-on, either bias the dees or accept a more complex drive scheme; anticipate the problem at design time rather than after assembly.
Source quote & editorial note
it is possible to bias the dees to prevent multipactoring, and a more complex booster oscillator circuit is required
Editorial note, tabletop extrapolation: Directly applicable: multipactor lives in the low-voltage, MHz regime every starting tabletop dee passes through, so anticipate it - designing the dee stem so DC-bias insulation CAN be added is cheap at design time and expensive after. Whether the bias is actually needed is learned at first RF turn-on.
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MIT's measured beam envelope: width limited by the dees' internal aperture out to about one-third of final radius, then narrowing nearly linearly to the exit slit - their amplitudes damping from 0.8 in initially to ~0.1 in at the slit.
adiabatic damping (n^(-1/4)-class) is the standard interpretation; MIT's measured center-to-exit damping factor ~0.12Source quote & editorial note
the beam width was found to be limited by the internal aperture of the D's out to about one-third of the final radius and then to narrow in a nearly linear fashion out to the exit slit.
Livingston & Blewett, Particle Accelerators (1962) — p. 163-167
Editorial note, tabletop extrapolation: Give the first third of radius generous vertical aperture - that is where the envelope filled the dee aperture on MIT's machine - and let the outer region run tighter, which also helps RF economy. Confirm on the actual machine (witness strips, dg-695) rather than assuming the same profile.
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There is no magnetic vertical focusing at the machine center (n=0 by symmetry); the first turns survive because the dee-gap electric field acts as an electrostatic immersion lens - so central-region electrode geometry and RF phase matter most in the first few turns.
n(r) ~ r^2 near center -> no magnetic focusing at r=0; gap E-field provides focusing, modified by transit timeSource quote & editorial note
There is no vertical magnetic focusing at the center of the magnet. By a fortunate coincidence, electrostatic focusing by the accelerating fields is effective for low-energy ions.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 524, 526
Editorial note, tabletop extrapolation: Explains why source-to-dee geometry (chimney position, puller gap, aperture height) dominates beam capture on small machines: at the center magnetic vertical focusing vanishes and only builds as n grows off zero with radius, so the electric gap lens is what the first turn or two get. Central-region electrode design is where capture is won on the documented machines.
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Design the chamber, dee, dummy dee and filament to disassemble with screws rather than glue or solder - the 2006 Houghton chamber's glued glass insulation could not be repaired after a dee-to-wall spark, forcing a complete rebuild.
Source quote & editorial note
This design strategy made it impossible to fix a single component of the apparatus, such as the insulation, without replacing the entire piece.
Editorial note, tabletop extrapolation: A next machine should assume sparks and insulator damage happen across a machine's life: modular fastening where practical turns rebuilds into part swaps - the source's glued chamber is the cautionary case. Where glue or solder is structurally necessary, design the bonded assembly itself as the replaceable unit.
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Electric-field defocusing near the center loses roughly 90% of starting ions to the dee surfaces; reduce the loss by raising dee voltage so ions make fewer turns and accumulate less phase shift.
higher V_dee -> fewer turns -> smaller phase slip and center lossSource quote & editorial note
some 90% of the initial supply of ions are lost to the dee surfaces. The loss may be reduced by increasing the dee voltage, thus reducing the number of turns an ion makes
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 18
Editorial note, tabletop extrapolation: Directly applicable: at 1.3 kV the reference machine's protons make many turns, and the quoted machine cut its central losses with more dee volts. A strong transmission lever - alongside central-region geometry (dg-348), which shapes what the first turns even see; measure which binds before spending (dg-303).
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Prefer oil diffusion pumps over mercury for accelerator columns: mercury vapor promotes autoelectronic (field-emission) discharges from high-voltage electrodes, and fast pumping is needed for steady discharge conditions.
Source quote & editorial note
Fast pumping is required and it is desirable to use oil rather than mercury diffusion pumps as mercury seems to promote autoelectronic discharges from the electrodes.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 259-260
Editorial note, tabletop extrapolation: Moot for pump choice today; the observation transfers cautiously: the source found mercury vapor SEEMED to promote field emission from HV electrodes, and condensable conductive films on electrodes are a recognized breakdown risk generally - keep electrode surfaces free of deposition, sputtered films included (dg-261's clean-surface caveat).
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Livingston & Blewett's worked hot-cathode arc source: 3 A discharge at 100 V, ~2 A electron beam from the exit hole, gas flow 2 cm3/min at atmospheric pressure - and a resonant ion beam that 'might be about 0.5 mA'.
arc 3 A at 100 V; electron beam ~2 A; gas 2 cm3/min (STP); resonant beam 'might be about 0.5 mA' (their words)Source quote & editorial note
arc current, 3 amp; arc voltage drop, 100 volts; electron beam from exit hole, 2 amp; gas flow, 2 cm3/min at atmospheric pressure. The resonant ion beam pulled from such a source ... might be about 0.5 ma.
Livingston & Blewett, Particle Accelerators (1962) — p. 175-178
Editorial note, tabletop extrapolation: The architecture point transfers at any size: a differentially pumped source cavity running much higher pressure than the chamber, fed through the exit hole (the Penning-table rules carry pressure numbers - dg-372). The single operating point is a sanity anchor for a similar source, not a spec or a promise of half a milliamp.
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MIT's machine: base pressure better than 1e-6 mm Hg with no gas flow, about 2e-5 mm Hg operating with deuterium flowing - the ion-source gas load, not outgassing, set the working pressure on that machine (2400 l/s of pumping on a 2000 l volume).
MIT: 2400 l/s on 2000 l volume; base <1e-6 mm Hg, operating ~2e-5 mm Hg with D2 flowSource quote & editorial note
With no gas flow, chamber pressures of better than 1 x 10-6 mm Hg are obtained. With the deuterium gas flow from the ion source, the operating pressure is about 2 x 10-5 mm Hg.
Livingston & Blewett, Particle Accelerators (1962) — p. 198
Editorial note, tabletop extrapolation: Expect a large pressure rise when source gas flows: on a tight system the flow-on/flow-off ratio identifies the source as the load, while a rise WITHOUT flow is the leak-or-outgassing signature. What operating pressure a machine can afford is the beam-survival calculation's answer (the vacuum calculator's orbit mode), not MIT's 2e-5.
Cited in: The Vacuum Budget of a Cyclotron
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Penning-source housekeeping numbers from the handbook's table: gas consumption ~0.2 sccm (hot- and cold-cathode columns; 0.2-0.6 heated, 0.2-1.1 low-duty), source pressure 1-10 Pa, ignition 3 kV (hot-cathode column) to 5 kV (cold-cathode) - single values per column, a span across columns, not a printed range - though the running arc is 0.3-1.3 kV (1-5 kV for the high-arc column); the same table carries extraction voltages, anode apertures and cathode spacings for the larger machines.
gas ~0.2 sccm; p_source = 1-10 Pa; V_ignition = 3 (hot) / 5 (cold) kV per column; V_arc = 0.3-1.3 / 1-5 kVSource quote & editorial note
Operating Data of Penning Ion Sources: Arc voltage 0.3-1.3 / 1-5 kV; Ignition volt. 3 / 5 kV; Gas pressure 1-10 Pa; Gas consumption 0.2 sccm; Extraction voltage 5-25 / 5-35 kV; Anode aperture 1 x 25 / 1.5 x 25 mm; Cathode distance 10 / 6.5 cm.
Wolf (ed.), Handbook of Ion Sources (1995) — p. PDF p.101 (printed p.90), TABLE 5.5 in section 5.3.7 Operating Data
Editorial note, tabletop extrapolation: The reference machine's MFC should be sized and calibrated around the table's ~0.2 sccm scale, and the arc supply must tolerate a several-kV open-circuit ignition transient before folding back to run voltage - the table's ignition/run split is the reason.
Cited in: The Vacuum Budget of a Cyclotron
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Size thermionic cathodes with the Richardson formula, where temperature is the STEEPEST knob - a 10% temperature change swings emission ten- to a hundred-fold, the quoted sensitivity - so regulate filament heating tightly.
j_sat = A*b*T^2*exp(-e*phi/kT) A/cm^2, A = 120.4 A/cm^2K^2; W: phi = 4.54 V, A*b = 60; Ta: phi = 4.12 V, A*b = 60; thoriated W (Th on W): phi = 2.63 V, A*b = 3.0Source quote & editorial note
The increase of the saturation current with temperature is very strong; a 10% change in temperature corresponds to a 10-fold increase of 20% to a 100-fold increase.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 38-39
Editorial note, tabletop extrapolation: The reference machine's hydrogen filament source lives or dies on filament temperature stability, so a finely adjustable constant-current supply is worth more than raw power. Area, work function and surface condition set the baseline the temperature knob multiplies - and space-charge-limited extraction caps what raw emission increases can deliver.
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Budget filament heater power from radiation: refractory-metal filaments radiate roughly 20 W/cm^2 of surface at 2000 K, and nearly all input power leaves as radiation rather than end conduction, so the surrounding chimney/anode must take that heat.
P_rad ~ 20 W/cm^2 at 2000 K (W, Ta, Mo similar); at fixed temperature: I ~ d^1.5, V ~ l/sqrt(d)Source quote & editorial note
Most of the power put into a filament is radiated and very little is lost through the ends. Most high-temperature metals show similar radiation behavior (~20 W/cm2 at 2000 K).
Wolf (ed.), Handbook of Ion Sources (1995) — p. 39
Editorial note, tabletop extrapolation: A few cm^2 of hot filament dumps tens of watts into the reference machine's source body; the hood/chimney around the filament needs a conductive heat path to the pole or water cooling.
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Discharge-type sources with good confinement reach >=50% gas efficiency (multicusp: >50% for hydrogen), while poorly confined sources run 10-20%; every neutral that escapes the chimney loads the main vacuum, so gas efficiency is a vacuum-design parameter.
gas efficiency: multicusp/e-bombardment <=50% (H2 >50%); plasmatron family 10-20% to 50%Source quote & editorial note
Gas efficiency: >50% for hydrogen and higher for other gases.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 57, 69, 110
Editorial note, tabletop extrapolation: At 0.2 sccm feed and 50% efficiency only ~0.1 sccm leaves the chimney as neutrals - but the extracted ions end their lives in the same vacuum envelope (implanted, neutralized, desorbed later), so higher gas efficiency shifts where and when the load appears more than it deletes it. It still pays: neutral leakage at the source is continuous and concentrated in the beam region, so better confinement is worth real pumping speed there even though total throughput is conserved.
Cited in: The Vacuum Budget of a Cyclotron
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PIG/Penning discharges split into two useful regimes: cold-cathode (arc above 1 kV at 0.5-5 A) and hot-cathode (arc below 1 kV at 1-50 A); the handbook adds that the magnetic field matters little above a minimum around 0.1 T, and that arc voltage rises as gas flow is cut until the discharge goes unstable.
cold cathode: V_arc > 1 kV, I = 0.5-5 A; hot cathode: V_arc < 1 kV, I = 1-50 A; B_min ~ 0.1 T; high-pressure regime 0.1-100 PaSource quote & editorial note
the arc voltage increases with decreasing gas flow... until the discharge becomes unstable... 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. PDF p.82 (printed p.71), section 5.2.2 Characterization of the PIG Discharge
Editorial note, tabletop extrapolation: The reference machine's center field clears the handbook's 0.1 T minimum, which makes an internal PIG a candidate - trading the fragile filament for a self-heated cathode running a sub-kV, multi-ampere arc. Suitability is more than field magnitude: geometry, cathode cooling at multi-ampere currents (dg-416) and pumping all vote; the regime table is the starting point, not the qualification.
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Expect the open-filament arc to run 0.5-2 A at 100-500 V at ~1e-4 mm of hydrogen (the source prints 'mm H2' - the operating gas - where this card previously transcribed 'mm Hg'); Wouters' procedure strikes it at 0.5-1 A and 100-200 V, with filament emission set to 10-20 mA at 200-300 V bias under high vacuum before admitting gas.
arc: 0.5-2 A @ 100-500 V @ ~1e-4 mm H2 (source's unit as printed); emission set-point 10-20 mA @ 200-300 VSource quote & editorial note
a moderate emission current (10-20 ma.) is observed with 200-300 volts arc bias ... an arc of 1/2 to 1 amp at 100 to 200 volts is usually satisfactory.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. PDF p.10 (printed -11-) for the procedure; PDF p.7 (printed -8-) for the arc range - NOT PDF p.6
Editorial note, tabletop extrapolation: A documented operating envelope for a simple hot-filament source at the reference machine's scale - a starting point whose actual values shift with geometry and field: commission against it, not to it.
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Wouters suggests ~0.025-inch tungsten ('perhaps', his word) over fragile automobile-lamp filaments - a 0.025-in tungsten filament takes about 25 A DC - and floats the filament supply across a storage battery to filter the ripple that vibrates the filament.
0.025 in W filament ~ 25 A dc at a few voltsSource quote & editorial note
an automobile headlight filament has been used, but the breakage has been high ... perhaps .025 in. tungsten ... A .025 in. tungsten filament requires about 25 amps d.c.
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 6-7
Editorial note, tabletop extrapolation: Filament sizing starts from emission demand and temperature, with Wouters' 0.025-in / 25 A as the documented anchor rather than a universal spec. The modern equivalent of the battery is a well-filtered DC filament supply - raw rectified current drives magnetically induced filament vibration in the cyclotron field.
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Shield the ion-source filament from the dee's RF field with a small metal 'chimney' tube (1/4 in) and let the dee field extract ions through a small side hole facing the gap.
1/4 in chimney tube over filament, side extraction holeSource quote & editorial note
A quarter-inch tube called a 'chimney' sits on top of the filament, which shields it from the electric field of the dee. Ionized hydrogen is drawn out of a small hole.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 3
Editorial note, tabletop extrapolation: A worthwhile arrangement for a next machine: the chimney gives a defined source position and shields the filament from the dee field - the quote's stated purpose. Comparisons against a bare filament (loading, output) are the builder's to measure, not the source's claim.
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DC glow discharges are organized by the pressure-distance product pd, not pressure alone; the glow regime runs ~300-1500 V at mA-level currents, and nearly the whole applied voltage drops in the few-mm cathode sheath.
breakdown V = f(p*d) (Paschen); glow: 300-1500 V, mA currents; cathode fall occupies first few mmSource quote & editorial note
The product of pressure and distance between the electrodes (pd) is a better parameter to characterize the discharge... The voltage is mostly in the range between 300 and 1500 V, but... the current is generally in the mA range.
Editorial note, tabletop extrapolation: When scaling chamber geometry or pressure for the p-B11 test cell, pd similarity is the right first knob - it organizes breakdown - but sustained-glow behavior also moves with gas, electrode material and area, and current density, so expect to re-tune rather than translate. Either way, sputter damage concentrates at the cathode sheath edge.
Cited in: The Vacuum Budget of a Cyclotron
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Know the V-I ladder of a low-pressure DC discharge -- background/saturation, Townsend dark discharge, corona at sharp points, breakdown, normal glow (V roughly constant over decades of current), abnormal glow, then glow-to-arc when the cathode overheats -- and note the hysteresis: the glow persists below its striking condition once lit.
sequence: dark -> Townsend -> breakdown -> normal glow (V ~ const) -> abnormal glow -> arc; hysteresis on the way back downSource quote & editorial note
A hysteresis effect occurs; wherein instead of retracing the path... the discharge maintains itself in the normal glow regime... at considerably lower currents... Only then does it make the transition back to the Townsend regime.
Editorial note, tabletop extrapolation: Explains the striking-vs-running asymmetry a source can show: ignition up on the breakdown branch, then sustaining down on the glow branch at much lower voltage - the Penning table's several-kV-ignite / sub-kV-run split (dg-372) is this physics - and why current-limited (ballasted) supplies are needed to stop glow-to-arc runaway. The actual voltages move with gas, pd and geometry.
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A cold-cathode PIG the paper builds from an iron cathode body, a ~3 kG SmCo permanent magnet, a folded 0.13 mm stainless-sheet anode and an iron faceplate with a 6.4 mm axial aperture delivered a continuous 1 mA beam of positive hydrogen ions at 1 mTorr, on 5.4 kV and 32.4 W.
3 kG SmCo; 5.1 cm iron cathode body; 6.4 mm faceplate hole; 1 mA H+ at 1 mTorr, 5.4 kV, 32.4 WSource quote & editorial note
A samarium cobalt permanent magnet with a surface flux density of approximately 3 kG... The anode is fabricated by forming 0.13-mm-thick nonmagnetic stainless steel sheet metal into the shape of a cup... machined with a 6.4-mm-diameter hole on centerline.
Rovey, Ruzic & Houlahan, Simple Penning Ion Source for Laboratory Research and Development Applications (2007) — p. PDF p.1 (printed 106101-1) for the construction text; PDF p.2 (printed 106101-2) for Fig. 1 dimensions
Editorial note, tabletop extrapolation: A directly copyable permanent-magnet source recipe at hobby machining tolerances - copy from the paper's drawings, and treat the output as mixed hydrogen species (H+, H2+, H3+) until a bend or velocity filter resolves it (dg-001).
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An internal cold-cathode PIG source is a low-maintenance choice: the Rutgers source runs more than 40 hours between servicings.
>40 h service intervalSource quote & editorial note
The ion source is an internal cold cathode Penning Ion Gauge (PIG) source that operates in excess of 40 hours before requiring service.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 2
Editorial note, tabletop extrapolation: Benchmarks source maintenance for a next machine: one documented internal cold-cathode PIG ran 40+ hours between servicings. Filament sources trade shorter cathode life for simpler supplies (dg-704's census practice) - lifetimes vary with design and duty on both sides of that trade.
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Forringer's cold-cathode PIG ran from a ~3 kV current-limited supply - after striking, arc voltage drops to whatever sustains the set current - and the 1.9-3.8 mm cathode-anode gap was 'not a critical parameter for the source's operation'.
strike supply 3 kV / 1 A current-limited; running arc voltage < 3 kV; gap 0.075-0.150 in non-criticalSource quote & editorial note
For this source a Glassman High Voltage KL series high voltage supply rated at 3kV and 1A provided the necessary potential. When the plasma is established, the power supply shifts to current limited operation ... The cathode anode gap was between 0.075” (1.9 mm) and 0.150” (3.8 mm)
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. PDF p. 29 (printed p. 19)
Editorial note, tabletop extrapolation: Relaxes the machining tolerance on a next machine's source gap and anchors the supply class: a ~3 kV current-limited unit ran this source. Strike voltage moves with pressure, gas, field and surface condition, so provide voltage headroom (or an ignition boost) rather than assuming the same number transfers.
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Water-cool the cathode rod and anode base of an internal PIG - copper parts melted when the source was run without cooling - and prepare cathode faces by sanding with 100-grit paper to a uniformly rough surface for reliable arc striking.
Source quote & editorial note
Water cooling for the cathode rod and the anode base are essential (some copper parts were melted when the ion source was run without proper cooling).
Editorial note, tabletop extrapolation: The source's warning stands as written: they melted copper running without cooling. A reference-machine-class source at much lower arc power may not need water - but that is a claim to establish by thermal estimate and a supervised first run with temperature monitoring, not by assumption. The sanded-cathode arc-striking preparation transfers directly.
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A DC extraction test stand characterizes an internal source before installation: a puller with 12.7 mm radius of curvature held 50 kV across a 5.0 mm minimum source-puller gap on that stand, and a 2.9 mm gap held about 25 kV.
R_puller = 12.7 mm: gap 5.0 mm -> 50 kV; gap 2.9 mm -> ~25 kV (that stand's measured holdoff)Source quote & editorial note
This puller was designed for the ion source test stand to hold 50 kV... The minimum source to puller gap is 0.196 (5.0 mm).
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 68, 75
Editorial note, tabletop extrapolation: Two measured holdoff points from one clean DC stand - anchors for a dee-tip/puller voltage budget, not a kV-per-mm allowable: vacuum holdoff is nonlinear in gap and hostage to finish, conditioning, and RF-vs-DC differences. Do what the source did: measure the actual geometry on a test stand rather than applying a scaling law.
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Run the hot-cathode source arc chamber in graphite (86-inch: 0.563-in OD graphite tube), feed 2-3 cc/min of hydrogen, and expect arc conditions of 0.5-1.5 A at 100-300 V with a 0.062 x 2.5 inch exit slit.
H2 flow 2-3 cc/min; arc 0.5-1.5 A @ 100-300 V; slit 0.062 in x 2.5 inSource quote & editorial note
The rate of flow required during operation is from 2 to 3 cc/min ... Electrons are accelerated from the filament into the arc chamber by a 100 to 300 volt potential, the normal arc current being 0.5 to 1.5 amperes.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. 62, 64
Editorial note, tabletop extrapolation: Documented arc conditions for a hot-cathode chimney source. Scaling to a much smaller chimney shifts gas flow and arc balance with geometry and pumping, so treat 0.5-1.5 A / 100-300 V / a few cc/min as the class of numbers to expect and tune on the machine. The robust transfer is the material lesson: graphite chimney and slit parts resist sputtering far better than copper or steel.
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Treat alignment of the ion source with the magnetic field and the accelerating slits as the critical tune - the quote; the report's specific geometry (filament fully covering the defining slot, slot edge tangent to the arc-slit plane) is its own practice (scan re-read queued).
Source quote & editorial note
The filament is aligned to completely cover this circular defining slot. The front edge of the defining slot is placed tangent to the external plane of the arc slit.
Livingston & Boch, The Oak Ridge 86-Inch Cyclotron — ORNL-1196, OSTI 4357145 (1952) — p. PDF p. 64 = printed p. 64 (section 'The Ion Source')
Editorial note, tabletop extrapolation: Directly applicable: build a next machine's source mount with repeatable rotation/translation adjustment from outside vacuum; source-to-puller alignment is worth more beam than any power knob.
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Provide pumping speed of at least 1 liter/sec (at 1e-5 mm Hg) per liter of chamber volume, and size the roughing pump to reach diffusion-pump backing pressure in 15-20 minutes.
S >= 1 (l/s)/liter of volume at 1e-5 torr; roughing time to backing pressure 15-20 minSource quote & editorial note
A good rule of thumb is to provide a pumping speed of at least 1 liter/sec at 10-5 mm Hg per liter of volume ... 15 to 20 min is considered a good design figure.
Livingston & Blewett, Particle Accelerators (1962) — p. 197-198
Editorial note, tabletop extrapolation: For a ~30-50 liter tabletop chamber the rule asks for 30-50 l/s DELIVERED at the chamber; the SI100's 100+ l/s class inlet rating leaves margin that the plumbing then spends - baffle, elbows and port conductance cut delivered speed (1/S_eff = 1/S + 1/C, dg-906) - so compute the delivered figure before crediting the margin. On a gas-fed machine the source load dominates either way.
Cited in: The Vacuum Budget of a Cyclotron
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Never exceed a diffusion pump's critical forepressure (25-75 Pa, i.e. 0.2-0.6 Torr, design-dependent); above it the jets collapse and inlet pressure rises uncontrollably, and at maximum throughput the tolerable forepressure drops to ~3/4 of its normal value.
critical forepressure 25-75 Pa; at max throughput reduce limit to ~0.75x; boiler pressure ~200 PaSource quote & editorial note
This maximum value called the 'critical forepressure,' ranges from 25-75 Pa (0.2-0.6 Torr)... The critical forepressure should never be exceeded.
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 232-233
Editorial note, tabletop extrapolation: Size and maintain the backing pump so the foreline stays well under the pump's critical forepressure during beam-gas loads - for the SI100, take the manufacturer's figure; the quoted 0.2-0.6 Torr is the generic design range. A tired rotary pump silently pushes the foreline over the cliff and dumps oil vapor into the chamber.
Cited in: The Vacuum Budget of a Cyclotron
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Budget unbaked, uncleaned stainless steel at ~1e-5 Pa-m/s (~7.5e-9 Torr-L/s-cm2) after 10 h of pumping, reduced 10-100x for high-vacuum suitability - the quoted figures; the book's bake schedules (mild vs 150 C) and UHV reduction factors are its adjacent material (scan re-read queued).
q(304 SS, unbaked, 10 h) ~ 1e-5 Pa-m/s; HV needs 10-100x reduction; UHV needs 1e4-1e5x; unbaked systems ~1e-6 Pa base, UHV bake ~150 CSource quote & editorial note
The outgassing rate of unbaked, uncleaned stainless steel is of order 10-5 Pa-m/s after 10 h of pumping... reduced by a factor of 10-100... to be suitable for high vacuum
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 308
Editorial note, tabletop extrapolation: Multiply the next machine's internal area by 1e-5 Pa-m/s and divide by delivered pumping speed to predict the 10-hour base pressure before drilling a single hole.
Cited in: The Vacuum Budget of a Cyclotron
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No structure can beat the aperture limit: molecular-flow conductance of any opening is at most 11.6 L/s per cm2 for room-temperature air, and any real tube delivers only a fraction a (transmission probability) of that.
C(L/s) = 11.6*A(cm2) for a thin aperture; C = 11.6*a*A for a real duct; long round tube a ~ 4d/(3l)Source quote & editorial note
the molecular conductance per unit area of any structure in molecular flow has a maximum value [11.6 L/(s-cm2) for air at 22C]
O'Hanlon, A User's Guide to Vacuum Technology, 3rd ed. (2003) — p. 48-50
Editorial note, tabletop extrapolation: Sets the ceiling on what the SI100 can actually pump through the chamber port: a 4-inch (81 cm2) opening passes at most ~940 L/s, and a baffled elbow far less - size the pump port as large and short as possible.
Cited in: The Vacuum Budget of a Cyclotron
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Elastomer-sealed flange systems (ANSI/ISO/KF) are realistically good to ~1e-6 Torr (rated 1e-8) and limited to ~150 C bakes; if a joint must ever be baked hotter or hold UHV, design in a metal seal (Conflat copper 300+ C) from the start.
elastomer flanges: rated 1e-8 Torr, better suited to 1e-6 Torr, 150 C max; metal seals (CF/VATSEAL) bakeable to 300 CSource quote & editorial note
Vacuum rated to 1 x 10-8 Torr (better suited to 1 x 10-6 Torr). Temperature rating is dependent on which elastomer o-ring is used (usually 150C)
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 443-446
Editorial note, tabletop extrapolation: Matches the reference machine's observed 1e-6-range vacuum with Viton seals - typical of all-elastomer systems, where permeation and outgassing usually hold operation near the recommended regime, though well-designed elastomer systems can run lower. A CF port or two on a next machine (gauge, RGA) buys bake and UHV headroom cheaply.
Cited in: Cyclotron Glossary · Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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A virtual leak is trapped atmospheric gas bleeding out through a blind path; its gas load is bounded by Santeler's envelope Q <= Pa*V/(e*t), and the classic culprits are unvented screws in blind tapped holes, double welds enclosing a void, and unvented double O-rings - vent (drill or slot) every trapped volume.
Q_max(t) = Pa*V/(e*t) - the worst case at time t over all connecting conductances; a specific path with conductance C gives Q(t) = C*Pa*exp(-C*t/V) (Santeler, NASA SP-105)Source quote & editorial note
A virtual leak is a volume of trapped atmospheric gas that leaks into the vacuum vessel through holes or cracks that do not go all the way through the vessel wall. [Examples:] Unvented Screw, Two Welds in Series, Unvented Double O-rings
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 59-63
Editorial note, tabletop extrapolation: Every internal socket-head screw in the next machine (dee supports, ion source mounts) needs a vent hole, a slotted thread, or a vented washer; a slot machined in the O-ring groove floor serves the same purpose.
Cited in: Cyclotron Vacuum Chamber Design and Sealing · The Vacuum Budget of a Cyclotron
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O-ring seal design for accelerator vacuum: prefer face seals, use as heavy a squeeze as possible, consider lubrication only when heavy squeeze is impossible, expect heavy flange construction to react the squeeze, and use two O-rings with a guard vacuum between them to drastically cut permeation.
guard vacuum example: 760 Torr across 1st ring reduced to 1e-2 Torr across 2nd ring (DARHT-II: 15 mTorr guard, 5e-8 Torr design pressure)Source quote & editorial note
Face-type o-ring seals are recommended. Use as heavy a squeeze as possible... Two o-rings in series can drastically reduce permeation.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 71-74
Editorial note, tabletop extrapolation: To push an elastomer-sealed system's floor lower on a next machine, a double O-ring lid groove with a guard vacuum from the existing roughing pump attacks the permeation term specifically - the dominant elastomer floor once outgassing is conditioned down - for the cost of one groove and a hose barb. The guard reduces pressure-driven permeation through the inner seal (DARHT's numbers are that installation's); the inner ring's own outgassing remains, so the floor drops rather than disappears.
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Vacuum-weld discipline: use single, continuous seam welds arranged so no unvented trapped volume or vacuum-side crevice remains, and stagger-weld internal bracing so it cannot form sealed pockets - Argonne welded its seams on the atmosphere side only and stagger-welded the braces 'to keep virtual leaks at a minimum'. [Corrected 2026-08-23: earlier text made 'weld only on the atmosphere side' a universal rule and said virtual leaks 'cannot form'. Vacuum-side or full-penetration welds are normal where they avoid a vacuum-side crevice; the invariant is no double-sealed unvented pocket, and Argonne's own word is 'minimum', not zero.]
Source quote & editorial note
Seam welds are continuous, with welding only on the atmosphere side. The internal braces are stagger welded to keep virtual leaks at a minimum.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 7
Editorial note, tabletop extrapolation: On any welded chamber or fitting for a next machine the question to ask of every joint is: is there a pocket sealed on both sides, or a crevice open to vacuum? Vent it, or weld it through. Argonne's atmosphere-side seams are one way to satisfy that, not the rule itself.
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Attain about 1e-5 mm Hg before starting, tolerate no worse than ~1e-3 mm Hg during RF bakeout, and cyclotron operation 'can be attempted' - the source's phrasing - at 1e-4 mm Hg or less.
base ~1e-5 torr; bakeout ceiling ~1e-3 torr; operation <= 1e-4 torrSource quote & editorial note
a preliminary vacuum of about 10^-5 mm hg should be attained; during 'bakeout' pressure should not exceed ~10^-3 mm. Operation as a cyclotron can be attempted with a pressure of 10^-4 mm or less
Wouters, General Recommendations for Design of Small Cyclotrons — UCRL-476 (1949) — p. 6
Editorial note, tabletop extrapolation: Historically grounded milestones, and the regime the reference machine operates in. What pressure a given machine NEEDS is the charge-exchange survival calculation (dg-460; the vacuum calculator's orbit mode) - at 1e-4 torr a proton spiral loses heavily, which is why this collection's operating rules sit in 1e-5-class territory.
Cited in: The Vacuum Budget of a Cyclotron
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Run a short, fat (3-inch diameter) pump duct straight down from the chamber to maximize conductance - the paper's design choice, on a machine that holds ~1e-7 Torr base while feeding its ion source.
3 in dia straight vertical duct; base ~1e-7 Torr with gas loadSource quote & editorial note
a 3 inch diameter tube in the corner can extend directly downwards to a vacuum pump underneath. This design choice maximizes vacuum conductance.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2
Editorial note, tabletop extrapolation: Pumping a gas-fed cyclotron is conductance-limited, so place the pump under the chamber with the largest, straightest duct possible - the term you control at layout time. What pressure results is the whole budget's answer: throughput, pump speed and conductance together (the vacuum calculator).
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A 1e-6 torr operating vacuum via diffusion pump plus liquid-nitrogen cold trap (roughing to 1e-3 torr mechanically) is the proven recipe at the 15 cm, few-hundred-keV scale; monitor with thermocouple gauges above 1e-3 torr and an ion gauge below.
rough to ~1e-3 torr, diffusion+trap to ~1e-6 torr; TC gauge >=1e-3, ion gauge to 1e-8Source quote & editorial note
an Innovac R220 diffusion pump and Kurt J Lesker TNR6XA150QF cold trap are used, which can lower the pressure to about 1e-4 Pa (1e-6 torr)
Loucks, Initial Results from the Houghton College Cyclotron — Houghton College thesis (2007) — p. 41-43
Editorial note, tabletop extrapolation: Matches the reference machine's scale exactly: 1e-6 torr base, bled up with source hydrogen, is the working point of the documented machines in this peer group (Houghton, the Rutgers 12-inch, the reference machine - the census's compare rows carry the values). The recipe is the proven one at 15 cm scale; the pressure a machine actually needs remains the survival calculation's answer (dg-460).
Cited in: The Vacuum Budget of a Cyclotron
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Match the chamber to the magnet - the paper's build: a 2.54 cm thick aluminium ring of 9.9 cm outer / 8.5 cm inner radius, ten KF-16 ports secured with vacuum epoxy, with 0.65 cm lids carrying a Viton O-ring groove, reaching 2e-6 Torr.
wall ring 2.54 cm thick, r_out 9.9 cm, r_in 8.5 cm; lids 0.65 cm; 10 x KF-16; Viton O-ring; base 2e-6 TorrSource quote & editorial note
Two 0.65 cm thick circular lids ... included a gland for a Viton O-ring for the vacuum seal. ... The chamber can be evacuated down to a final pressure of approximately 2 × 10−6 Torr
Yuly, The Houghton College Cyclotron: a Tool for Educating Undergraduates — Cyclotrons 2013, WE1PB01 (2013) — p. PDF p. 2 for the lids and Viton seal; PDF p. 3 for the 2 × 10−6 Torr
Editorial note, tabletop extrapolation: A complete documented chamber design for an 8-inch-pole machine, including the epoxied-flange trick that avoids welding. Copy from the paper - then qualify your own copy: epoxy joints and lid stiffness are workmanship-dependent, so leak-check the flanges and run the lids through the lid-deflection calculator rather than inheriting the paper's result.
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Avoid welding lids onto a thin flat vacuum chamber: weld shrinkage warped the whole frame; grinding off the weld and sealing with a flat Viton gasket fixed it - prefer demountable elastomer seals for flat chambers.
Source quote & editorial note
after the welding, the bottom plate contracted so much that it bent the whole frame out of shape... seal the bottom plate against the frame using a flat Viton ring.
Baumgartner, The Cyclotron Kids' 2 MeV Proton Cyclotron — Cyclotrons 2013, WE1PB05 (2013) — p. 2-3
Editorial note, tabletop extrapolation: A fabrication trap the builder can sidestep: demountable elastomer seals on both lids avoid weld distortion entirely on a thin flat chamber - the route the source machine retreated to after its frame warped. Where welding is preferred, controlled sequence and post-weld machining are the professional counters; for a garage build, not welding thin flat plates is the cheap answer.
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Size the deflector with septum radius increment dR ~ 0.15R - MIT's typical figure, with the formula showing voltage cost growing with dR - and taper the channel gap, the quoted 1/8 in at entry opening to 1/2 in or greater at exit, to accommodate divergence.
V_d ~ (2T/e)*d*(1/R - 1/(R+dR)); MIT 16 MeV, d=0.3 in: dR=0.1R -> 47 kV, dR=0.2R -> 87 kV; typical dR=0.15RSource quote & editorial note
A typical figure, used in the MIT cyclotron, is a dR of 0.15R. The deflector gap is usually tapered ... Spacings as small as 1/8 in. can be used at the entry slit, opening to 1/2 in. or greater at the exit.
Livingston & Blewett, Particle Accelerators (1962) — p. 180-181
Editorial note, tabletop extrapolation: Scaled to ~150 keV the same normalized geometry needs only ~500-900 V on the deflector - an easy supply. Entry-slit width is set against the local turn separation and beam width together (dg-495), not by a fixed prescription.
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Choose 304L (not 304) stainless for welded vacuum chambers - the low-carbon grade is the standard vacuum choice for weld integrity - and remember TIG/MIG joint design, cleanliness, and (for aluminum) high weld speed control distortion and leaks.
Source quote & editorial note
304L SS, most commonly used in vacuum, a little more expensive... Joint design is critical from vacuum, metallurgical and distortion standpoints. Cleanliness is essential.
Bertolini, Accelerator Vacuum and Mechanical Engineering — USPAS course, UCRL-MI-201847 (2004) — p. 355-360
Editorial note, tabletop extrapolation: For a next machine's chamber welds, specify 304L filler and stock where practical: the low-carbon grade resists weld sensitization (carbide precipitation and intergranular attack near welds). Plain 304, welded cleanly, also serves - the lecture's 'most commonly used' is a preference with reasons, not an exclusion - and leak-tightness comes from joint design and cleanliness either way.
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Verify chamber lid thickness with the fixed-edge circular-plate deflection formula (Roark): the thesis's example - a 10 cm radius aluminum lid only 3.5 mm thick deflects under 1 mm at full vacuum. Deflection is set by elastic modulus and thickness (D ~ E*t^3), which alloy choice barely moves; a higher-yield alloy like 7075-T6 raises the stress margin, not the stiffness.
delta_center = -q*a^4/(2D)*(L14-L11), D = E*t^3/(12(1-v^2)); alloy trades yield margin (7075-T6 505 MPa vs 6061-T6 275 MPa), not deflection - E is nearly identicalSource quote & editorial note
a lid with radius 10 centimeters and thickness of 3.5 millimeters would undergo less than 1 mm of deflection when covering a chamber with internal pressure of 1e-3 Torr
Editorial note, tabletop extrapolation: The actual formula for trading a next machine's lid thickness against magnet gap: a few mm of plate suffices at 8-12 inch chamber diameter IF the edge support is real (the lid-deflection calculator covers both edge conditions). Alloy choice buys yield margin at the price of 7075's poorer weldability and corrosion behavior - it stiffens nothing.
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Everything inside a strong cyclotron field must be magnetically transparent - aluminum, copper, brass - since ferromagnetic parts distort the field and disrupt measurements.
Source quote & editorial note
all cyclotron components must be made of magnetically transparent materials such as aluminum, copper, or brass
Editorial note, tabletop extrapolation: Standard but easily violated rule: screws, feedthrough bodies, and detector hardware inside the reference machine's gap should be checked with a hand magnet before installation.
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Design for maintenance access from day one: ANL mounted the dee assembly on a motor-driven rail carriage so the entire dee system rolls out of the chamber for service - the quote; the mobile diffusion-pump provision is the report's neighboring detail (scan re-read queued).
Source quote & editorial note
the VTO box and obround are mounted on a motor-driven carriage which operates on a rail system. This permits the removal of the dee heads... to facilitate maintenance.
Ramler & Parker, The Argonne 60-Inch Cyclotron — ANL-5907 (1959) — p. 6-7
Editorial note, tabletop extrapolation: At tabletop scale this means: chamber slides out of the gap, dee removable through a lid, pump cart disconnectable - the difference between a research tool and a sealed monument.
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p-B11 disintegration alphas were observed from ~60-70 kV proton energy in the 1933 experiment - an observed onset under their target and detector arrangement, not a reaction threshold - with yield rising steeply toward 200 kV and a maximum alpha range of 4.7 cm in air; thick-target Li appeared from ~30 kV for comparison.
B threshold(observed) ~60-70 kV at ~50 uA and 0.7 sr; max alpha range 4.7 +/- 0.15 cm airSource quote & editorial note
It is seen that particles are detected at about 70 kv. and the numbers increase more rapidly with increase of bombarding energy than with the lithium film.
Oliphant & Rutherford, Experiments on the Transmutation of Elements by Protons (1933) — p. 266-270
Editorial note, tabletop extrapolation: Proof that p-B11 alphas are observable far below the 675 keV resonance: the 1933 apparatus saw them at 60-70 kV using tens of microamps and large solid angle, so a lower-current machine compensates with integration time and geometry. Their alphas stopped in under 5 cm of air, hence the vacuum path to a PIPS detector.
Cited in: Experiments by Energy Band
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Check that beam probes/collectors are thinner than the local turn spacing: at 10 kV Vp-p and 1.0 T the turn spacing near r = 4 in is only 0.04 in, so a 0.06-in-thick RF shield on the collector tip masks real beam.
dr = V_gain/(2E_total) * r; Rutgers: dr = 0.04 in at r = 4 in for 10 kVp-p, 1.0 TSource quote & editorial note
the ion revolution turn spacing near r = 4 inches, in a B-field of 1.0T will be just 0.04 inches, which is smaller than the 0.06 inch RF shield of the tip
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 1
Editorial note, tabletop extrapolation: At the reference machine's ~1.3 kV the turn spacing is smaller still, so geometry matters doubly: a thick tip costs single-turn radial resolution first, and a shield mounted AHEAD of the collector can shadow it into reading zero while beam exists - the quoted case. A bare, grooved copper collector is the safe default until turn-resolved measurements are wanted.
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Entry-slit width is set by the turn separation dr = (r/2)*(dT_turn/T) - energy gain per turn over total energy, halved (nonrelativistic); make the septum and deflector radially adjustable because calculated positions are only approximate. [2026-08-28: 'nonrelativistic' scoping adopted from the upstream erratum of 2026-08-26 - the turn-separation form drops the relativistic factor.]
dr/r per turn = (1/2)*dT_turn/T (nonrelativistic); MIT: dr ~ 0.1 in at extractionSource quote & editorial note
The limit at the entry is set by the dr between successive turns at this radius ... it is desirable to have adjustable controls on deflector spacing and location which can be trimmed empirically.
Livingston & Blewett, Particle Accelerators (1962) — p. 181-183
Editorial note, tabletop extrapolation: With ~2.6 keV total gain per turn at ~150 keV, the reference machine's turn spacing at extraction is ~0.9% of r - about 0.7 mm at r = 3.2 in - so build the septum mount with millimetre-scale radial adjustment.
-
Expect extraction well below circulating current: MIT obtained up to ~25% of the resonant beam under optimum conditions (150 uA of ~600 uA circulating), with practical operation at 80-100 uA.
extraction efficiency <= ~25% (MIT: 150 uA extracted of ~600 uA circulating; routine 80-100 uA)Source quote & editorial note
Emergent beam intensities up to 25 per cent of the resonant beam intensity have been obtained under optimum conditions ... practical operating intensities would in this case be limited to 80 or 100 ua.
Livingston & Blewett, Particle Accelerators (1962) — p. 182
Editorial note, tabletop extrapolation: Judge a next machine first on internal-probe current at full radius: documented machines commonly ran internal currents several times their extracted beam (MIT's optimum was 4:1), so a gap of that order is precedented rather than failure. The rung-by-rung extraction picture is dg-595's; the census cross-checks are dg-260's.
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Turn-to-turn orbit separation is dR = (R/2)*(2*q*V0*sin(phi_s)/T) - it shrinks as energy grows (100 kV dee, R=1 m, 20 MeV gives only 4.4 mm), which is what makes septum extraction hard late and easy never.
dR = (R/2)*(2*q*V0*sin(phi_s)/T)Source quote & editorial note
The separation for non-relativistic ions is dR = (R/2) (2qVo sin phi_s/T)... Eq. (15.3) implies that dR = 0.44 cm.
Humphries, Principles of Charged Particle Acceleration (1986) — p. 527
Editorial note, tabletop extrapolation: Lets the builder compute whether a probe or future septum can distinguish final turns: at ~150 keV, r ~ 9.6 cm and the reference machine's 2.6 keV total gain per turn, dR = (r/2)*(2.6/150) ~ 0.8 mm - tight for a probe, and doubling volts-per-turn doubles it.
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Design the p-B11 experiment around the 675 keV resonance: the fitted alpha yield coefficient A0 rises from 0.91 mb/sr at Ep=0.15 MeV to 218 mb/sr at 0.65 MeV - a factor of ~240 - so every keV of proton energy toward 650-675 keV multiplies count rate.
A0(0.15 MeV)=0.91 mb/sr; A0(0.30)=20.8; A0(0.49)=114; A0(0.65)=218 mb/srSource quote & editorial note
0.15 0.91 +/- 0.015... 0.65 218.42 +/- 0.55
Spraker et al., The 11B(p,α)8Be → α+α and the 11B(α,α)11B Reactions at Energies Below 5.4 MeV (2012) — p. 360
Editorial note, tabletop extrapolation: The master rate table for the reference machine's PIPS window (150-675 keV) - as fitted A0 coefficients: a count-rate prediction folds in the angular terms, solid angle, target thickness and integration time (the experiments-by-energy arithmetic). What the table quantifies exactly is what reaching the resonance is worth: ~240x in A0 from 150 to 650 keV.
Cited in: Experiments by Energy Band
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Size an electrostatic deflector from Vd/d = (2T/e) * dR/(R(R+dR)): peeling a 0.472 MeV proton beam from R = 4 in to 4.5 in with a 0.291-in channel requires ~32.5 kV on the electrode.
Vd/d = (2T/e)*dR/(R*(R+dR)); the slide states Vd = 32.531 kV for B = 0.976 T, T = 0.472 MeV, d = 0.291 in - which this formula with these inputs does not reproduce (~7.6 kV). [2026-09-06 page-image re-read: the printed 32.531 kV and its inputs are exactly as transcribed - the discrepancy is the source's own, not OCR.] Use the formula with your own geometry and verify on the benchSource quote & editorial note
Our parameters: B=.976 T ... T=.472 MeV ... d=.291 inches ... Combining yields: Vd/d = (2T/R)(dR/(R+dR)) ... Vd = 32.531 kV
Ponter, Beam Energy Measurements with a New HV Deflection System and Ion Source Upgrades on the Rutgers 12-Inch Cyclotron (2010) — p. 6 (R and dR on 7)
Editorial note, tabletop extrapolation: Gives the builder the extraction-voltage scale for a next machine: deflector voltage scales linearly with beam energy at fixed geometry, so a ~100 keV beam needs about a fifth of a 472 keV machine's figure in the same channel. Given the source's formula/number discrepancy (see formula field), size from the formula and confirm by measurement.
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Fusion rate climbed steeply with grid voltage in the thesis's runs - their sweep: 10 cpm at -16 kV rising through 60 cpm at -25 kV (the quoted point) to 130 cpm at -31 kV, at 13-18 mTorr and ~10 mA - roughly 13x for a 2x voltage increase.
BF3 moderated counter: 16 kV -> 10 cpm; 25 kV -> 60-100 cpm; 31 kV -> 130 cpmSource quote & editorial note
Voltage -kV dc / Current milliamps / Pressure millitorr / Neutrons cpm: 16, 11, 18, 10 ... 25, 8.1, 14, 60 ... 31, 10.8, 13, 130. Figure 25 - Neutron readings versus other chamber parameters.
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. PDF p.46 = printed p.46 (Kovalchick, 'Experiment 7 - Observations', Figure 25)
Editorial note, tabletop extrapolation: The same lesson as the p-B11 cross-section curves: sub-barrier yield rises steeply with particle energy, so extra beam energy buys far more counts than the same fractional increase in current. The specific sweep numbers are one fusor's; the steepness is the physics.
Cited in: Experiments by Energy Band
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Neutron yield in Hull's fusor line climbed steeply with drive voltage: the 22 kV supply gave 1e3 n/s, 33 kV gave 1e5 n/s - a hundredfold - and his current machine, on a larger supply, exceeds 6e5 n/s; his investment order is voltage, vacuum cleanliness, and gas handling first.
22 kV -> 1e3 n/s; 33 kV -> 1e5 n/s; current machine > 6e5 n/s (that machine's supply voltage: scan re-read queued)Source quote & editorial note
It was limited to low level output by its 22kv internal supply. 103 n/sec... a 33 kilovolt supply. 105 n/sec... currently produces in excess of 600,000 neutrons per second
Hull, Fusor: An Easy to Construct Fusion Reactor Based on Inertial Electrostatic Confinement (2009) — p. 36-39
Editorial note, tabletop extrapolation: Reinforces energy-over-current for the builder: sub-Coulomb-barrier reaction rates reward every extra keV steeply - though not by a fixed orders-per-10-kV law; Hull's own steps differ between jumps.
Cited in: Experiments by Energy Band
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The circulating beam is not continuous: frame-by-frame analysis on this machine showed ions populating about 40 degrees of the 360-degree RF cycle - implying peak current roughly ninefold above average IF the bunch is near-uniform (the rectangular estimate).
bunch width ~40 deg of RF cycleSource quote & editorial note
Frame-by-frame analysis... revealed that ions nominally populate 40 degrees of the 360 degree RF cycle in our cyclotron.
Koeth, Undergraduate Education with the Rutgers 12-Inch Cyclotron (2015) — p. 9
Editorial note, tabletop extrapolation: Sets expectations for fast diagnostics and duty-factor arithmetic on any machine: measure your own bunch width (capacitive pickup, gated counting) and use it - 40 degrees is one measured machine's figure, not a constant.
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Sub-resonance p-B11 measurements were made with only 0.5-10 nA of protons on target (with ~60-70 keV beam energy resolution); the paper's setup - small-solid-angle detectors, thin targets - produced usable alpha spectroscopy at that current.
0.5-10 nA on target for Ep = 0.15-0.4 MeV data; 100-200 nA at higher energiesSource quote & editorial note
At these energies beam intensities varied from 0.5 to 10 nA on target ... detected by eight silicon surface barrier detectors ... each detector subtending a solid angle of approximately 2.5 x 10^-4 sr.
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. PDF 3 (printed 359), continuing on PDF 4 (printed 360)
Editorial note, tabletop extrapolation: The single most encouraging number in the batch: professional low-energy p-B11 data at exactly the reference machine's nA beam scale. Whether nA suffices for a given measurement follows from the rate arithmetic - cross-section, solid angle, integration time (the experiments-by-energy worked examples) - not from precedent alone.
Cited in: Experiments by Energy Band
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Accept that the honest headline number for a small machine is small: Houghton's best was ~0.1 uA at a B/3 resonance (the paper's figure), and 3 pA at the highest proton energy reached - 160 keV at 796 mT and 12.1 MHz; the paper names more magnet current, cooling and RF frequency as what higher energy would take.
0.1 uA best (B/3 resonance); 3 pA at 160 keV, 796 mT, 12.1 MHz; 400 keV theoretical needs more magnet current, cooling, and higher RF frequencySource quote & editorial note
The highest proton energy obtained so far is about 160 keV, with a 3 pA peak near the correct magnetic field of 796 mT for 12.1 MHz.
Editorial note, tabletop extrapolation: Calibrates expectations exactly at the reference machine's operating point (~150 keV): currents fall steeply near a machine's energy limit, and the gating items the paper lists are the ordinary ones - magnet current, cooling, RF range.
Cited in: Choosing Your Machine
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Signal-to-noise degrades with total input capacitance (detector + cable + stray), and feedback cannot recover it - keep the preamp physically at the detector and minimize cable before the first amplification stage.
V_signal = Q/C_total; equivalent noise charge grows with C_total; S/N cannot be improved by feedbackSource quote & editorial note
S/N cannot be improved by feedback. This result is generally valid, i.e. it also holds for active integrators (charge-sensitive amplifiers).
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 24
Editorial note, tabletop extrapolation: For the builder: mount the preamp on the vacuum feedthrough, not at the far end of a coax run. Cable capacitance raises the series-noise term, and at alpha-spectroscopy resolutions it competes with detector leakage and shaping-time choices for the noise budget - short cable is the cheapest term to fix.
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Read out silicon detectors with a charge-sensitive (feedback-capacitor) preamplifier so gain is set by Cf and is insensitive to detector capacitance, which varies with bias voltage in a partially depleted diode.
Q_signal integrated on Cf; dVout/dQ = 1/Cf independent of C_detSource quote & editorial note
Detector capacitance may vary within a system or change with bias voltage (partially depleted semiconductor diode)... Amplifier output directly determined by signal charge, insensitive to detector capacitance
Spieler, Semiconductor Detectors Part 2 — SLUO Lectures on Detector Techniques, Lecture 7 (1998) — p. 3-8
Editorial note, tabletop extrapolation: Confirms the standard PIPS chain for the p-B11 experiment: a charge-sensitive preamp at the feedthrough - the spectroscopy-grade choice, since a plain voltage amplifier's gain rides on the diode's bias-dependent capacitance. Voltage readout keeps niche uses (fast timing, very high rate) that energy spectroscopy is not.
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In the thesis's IEC context D-D fusion technically begins near 10 kV, but detectable fusion 'generally does not occur' below about 15 kV - their first clean counts came at -25 kV.
detectable onset (their setup): >= ~15 kV; first clean counts at -25 kVSource quote & editorial note
D-D fusion can occur in an IEC device at voltages as little as 10 kV or less, but detectable fusion generally does not occur until voltages are at least 15 kV
Kovalchick, Deuterium Fusion Using Inertial Electrostatic Confinement (2012) — p. 18
Editorial note, tabletop extrapolation: Calibrates expectations for any sub-threshold nuclear signal at home: being physically above a reaction threshold is not enough - the detectable onset sits well above it, and where it sits depends on geometry, gas pressure and loading, current, and the counting setup.
Cited in: Experiments by Energy Band · Shielding a Small Cyclotron
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For amateur fusion work the source recommends D-D fuel, branching about 50:50 to T+p and 3He+n; in their account D-T brings licensing and tritium handling, and 3He is prohibitively expensive.
D+D -> T + p (~50%); D+D -> 3He + n (~50%)Source quote & editorial note
The amateur is limited to the middle or D-D reaction which yields a split 50:50 reaction D+D to T + Proton, D+D to He3 + neutron
Hull, Fusor: An Easy to Construct Fusion Reactor Based on Inertial Electrostatic Confinement (2009) — p. 19-20
Editorial note, tabletop extrapolation: The reference machine's p-B11 choice sidesteps this entirely. If deuterium ever runs in the cyclotron, D-D is the accessible fusion fuel in the source's US hobbyist-era framing - but licensing attaches by jurisdiction and by what the device produces (see /legal/), so verify locally rather than treating any fuel as license-free. The safety fact is the neutron branch: half of D-D reactions emit a 2.45 MeV neutron.
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The fusor doc's grid rule: make it from tantalum or tungsten wire, fusion- or resistance-welded - their experience: a silver-soldered joint fails fast under a discharge that keeps the electrode incandescent (their 0.024-in Ta grid replaced a 0.030-in stainless one that glowed red at ~120 W).
0.024 in Ta wire replaced 0.030 in SS; grid glowed red at 2 kV x 60 mA (120 W) at 40 micronsSource quote & editorial note
The grid should be made from tantalum or tungsten wire and be fusion or resistance welded.
Hull, The Farnsworth/Hirsch Fusor — The Bell Jar, Vol. 6 No. 3/4 (1997) — p. 5-8
Editorial note, tabletop extrapolation: Applies in spirit to a next machine's chimney slits, puller edges and beam stops: anything the beam or arc dwells on gets a material-and-joint choice made against its actual power density. Refractory metal with welded joints is the robust default where cooling is absent; cooled copper or graphite are engineered alternatives (dg-426, dg-939).
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Expect a serious commitment: Iowa State's project was 'long and laborious' and got first beam three years after starting, in spring 1957 (the start-year and team details are the article's: scan re-read queued).
3 years from start to first beamSource quote & editorial note
The project was a long and laborious one, but the efforts were well-rewarded when the first beam was obtained three years later, in the spring of 1957.
McGuire, The Iowa State University 1.5 MeV Undergraduate Cyclotron (1961) — p. 3
Editorial note, tabletop extrapolation: Schedule reality check consistent with the census: documented start-to-first-beam gaps run one to six years (the builds page's computed spread), and Iowa State's three sits mid-pack.
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Budget realistically before scrounging: a modest small accelerator bought new costs ~$128k (vacuum ~$20k, RF ~$17k, instrumentation ~$41k, magnet ~$15.5k, chamber ~$14k, detectors ~$20k) - which is why surplus procurement is the core amateur skill.
new-price line items total ~$127.5k (the article's rounded '$128,500' headline; 2010 dollars)Source quote & editorial note
TOTAL: $128500. Who has >$125k to blow on a very modest strawman small particle accelerator?
Niell, Effective Scientific Equipment Procurement Strategies: Building on a Budget (2010) — p. 2-3
Editorial note, tabletop extrapolation: Calibrates a next machine's budget: every subsystem not scrounged or fabricated costs thousands new (the article's line items), which is why surplus procurement dominates documented amateur practice - the census's cost trail says the same.
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Buy surplus using a three-line envelope - hard cost cap, minimum performance spec, and required function/condition: the quoted example ($400 cap; measure 40 MHz sine waves; in calibration and nearly bombproof); the article's tour of vendor tiers is its own commentary (scan re-read queued).
Source quote & editorial note
Cost: Can spend no more than $400. Performance: Want to measure 40MHz sinewaves... Function: Must be in calibration, and nearly bombproof
Niell, Effective Scientific Equipment Procurement Strategies: Building on a Budget (2010) — p. 7-10
Editorial note, tabletop extrapolation: A disciplined method for the next machine's shopping list: define the B-field, vacuum and RF numbers first, then match each purchase to the cheapest vendor tier whose reliability that subsystem can tolerate - judged per purchase, not by a permanent vendor ranking.
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Analyze all betatron resonances of order below 4 (plus any structure resonance whose order equals the sector number); the Qr = 1 resonance near the center is survivable only because it is crossed in 1-3 turns with no large first-harmonic field error.
check |nr|*Qr + |nz|*Qz = k for order |nr|+|nz| < 4; cross Qr = 1 in 1-3 turns with small B1Source quote & editorial note
its passage without noticeable losses of particles becomes possible only due to the fact that the beam crosses it for 1-3 revolutions, and the first harmonic of the magnetic field with a large amplitude is absent
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 37
Editorial note, tabletop extrapolation: In the reference machine Qr = sqrt(1-n) sits just below 1 everywhere, so first-harmonic field symmetry is the load-bearing tolerance: a coherent distortion driven by B1 grows while the resonance condition holds, and the crossing survives when B1 is small (the quote's condition) and the crossing fast. How small is computed for the actual machine - the beam-dynamics laboratory's imperfection tools do it; pole tilt and off-center coils are the usual B1 sources.
Cited in: Beam Dynamics: An Interactive Laboratory
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Avoid running the beam long near the Walkinshaw resonance Qr - 2Qz = 0 (n = 0.2 in a classical machine): mean-field nonlinearity there pumps radial into axial oscillation with the axial amplitude reaching twice the radial amplitude.
Qr - 2Qz = 0; classical cyclotron: sqrt(1-n) = 2*sqrt(n) -> n = 0.2Source quote & editorial note
When transferring the energy of radial betatron oscillations into axial oscillations, the amplitude of the latter turns out to be twice the amplitude of radial oscillations.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 39
Editorial note, tabletop extrapolation: Very concrete for the reference machine: if the edge-field falloff pushes n through 0.2 near the last turns, dwelling ions grow vertically as far as the coupling perturbation drives them - into the dee aperture if allowed. Keep n below ~0.2 out to the extraction radius, or cross the resonance fast (dg-152, dg-694).
Cited in: Beam Dynamics: An Interactive Laboratory
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To hold the field index n roughly constant over radius, profile the pole (shim) axial gap as g(r) = g0*(r/r0)^n.
g(r) = g0*(r/r0)^n (equivalently g0*(r0/r)^-n), eq. 5.9Source quote & editorial note
If the task is to obtain an average field with a value of the field decay index n close to constant for all radii, then the axial gap g can vary in accordance with the expression
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 49
Editorial note, tabletop extrapolation: A one-line pole-taper recipe for the builder tool: pick n (e.g. 0.02-0.2), machine the gap to this power law, verify in FEMM.
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Expect orbit separation from energy gain of dR = R*(dW/W)*(gamma/(gamma+1))/Qr^2 per turn; if that is too small for a septum, add a controlled first-harmonic bump (a few gauss suffices at the Qr = 1 crossing) to drive precession and enlarge turn spacing.
dR = R*(dW/W)*(gamma/(gamma+1))/Qr^2 per turn - W kinetic energy, dW the gain per FULL turn, Qr the local radial tune; the source's precession expression x_c = pi*R*(b1/B0)*n_eff uses its own n_eff definition (scan re-read queued for it)Source quote & editorial note
The presence of the resonance makes it possible to use the first harmonic of the field with a small amplitude (usually a few gauss) to obtain a significant increase in radial amplitudes.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 64-65
Editorial note, tabletop extrapolation: The dR formula tells the builder exactly what turn spacing a ~kV energy gain buys at 4-inch radius (fractions of a mm), i.e. whether a septum/foil extraction is geometrically feasible for a next machine.
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Size water-cooled copper main coils around the source's practically achievable engineering current density of ~5 A/mm^2 - defined there as ampere-turns over winding cross-section (superconducting NbTi windings reach 120-150 A/mm^2).
j_eng(Cu, water-cooled) ~ 5 A/mm^2; j_eng(NbTi SC winding) ~ 120-150 A/mm^2Source quote & editorial note
The practically achievable engineering current density (the ratio of the value of the ampere-turns in the winding to the cross section of the conductor) is of the order of 5 A/mm2.
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 15-16
Editorial note, tabletop extrapolation: First-cut sizing for a next machine's coil pack: NI / 5 A/mm^2 estimates the winding cross-section with water cooling - a starting point that still owes fill factor, cooling channels and insulation their space, and the thermal calculation is the real gate (magnet-power calculator). Air-cooled magnet wire derates well below this (dg-092).
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For maximum energy gain per turn, make the dee's RF angular size (geometric angle times harmonic h) 180 degrees or an odd multiple - where the |sin| factor peaks; energy gain per turn is dE = 2*N*q*U*|sin(h*dphi/2)|.
dE_turn = 2*N*q*U*|sin(h*dphi/2)|; |sin| = 1 at h*dphi = 180, 540, 900 deg (the sign alternation is a phase convention, absorbed into the synchronous phase); transit-time effects ride on topSource quote & editorial note
the maximum energy gain corresponds to a system in which the RF size of the dee is close to 180 degrees or is a multiple of 180 degrees with a factor of 3, 5, 7
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 11
Editorial note, tabletop extrapolation: The reference machine's single ~180-degree dee on h=1 is already the optimum; the formula lets the builder tool compute turns-to-energy for any future dee angle or harmonic choice.
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With a single dee at 60-70 kV, protons can reach 9-10 MeV in a decreasing-field classical cyclotron; energy scales with achievable energy gain per turn, so more turns cannot compensate a phase budget already spent.
1 dee, U = 60-70 kV -> E_final ~ 9-10 MeV (protons, decreasing field)Source quote & editorial note
in the presence of one accelerating dee and a voltage of 60-70 kV, protons can be accelerated in a decreasing magnetic field to an energy of 9-10 MeV
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 51
Editorial note, tabletop extrapolation: Sets the scale, not a law: the quoted machine class pairs 60-70 kV with 9-10 MeV, and the reference machine's ~1.3 kV dee at ~150 keV sits consistently below that line. Final energy in a classical machine is phase-budget-limited (the summed slip, dg-273), which dee voltage relieves nonlinearly - compute the budget rather than scaling proportionally.
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With an internal ion source and cosine RF, the central region's phase acceptance is roughly the starting-phase window (-90, +20) degrees; phase slits can then select bunches down to a few RF degrees.
phase acceptance ~ (-90 deg, +20 deg) relative to peak-voltage phase = 0Source quote & editorial note
the phase acceptance of the center, as a rule, contains the particles, the initial RF phases of which do not go beyond the range of (-90; 20)
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 56
Editorial note, tabletop extrapolation: Explains why a large fraction of source output never accelerates: only starting phases inside a ~110-degree window of the full 360 are candidates at all - a uniform-emission estimate makes that a ~30% ceiling, before radial and axial acceptance cut further; it is not a measured capture efficiency. The builder tool should launch macroparticles across this window rather than a single reference phase.
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For shielding design, fast-neutron production on complex nuclei is roughly one neutron per 10-15 MeV of proton energy (below 50-60 MeV); the source's permissible-flux figure is 30-60 n/cm^2/s (a dated, era-specific limit - modern limits are dose-based), and it gives the neutron relaxation length in ordinary concrete as 16 cm (1-2 m walls typical).
~1 neutron per 10-15 MeV proton energy on target; source's era limit 30-60 n/cm^2/s (dose-based limits govern today); concrete relaxation length 16 cmSource quote & editorial note
mainly fast neutrons are generated, and the permissible flux is 30-60 neutrons/cm2 s
Smirnov, The Cyclotron and Its Modeling — Phys. Part. Nuclei 52 (2021) — p. 16
Editorial note, tabletop extrapolation: At <=1 MeV protons the reference machine is below the (p,n) thresholds of its structural metals (the first structural channel, 55Mn(p,n)55Fe, opens at 1.03 MeV) and of the light targets: 7Li 1.88 MeV, 9Be 2.06 MeV, 11B 3.02 MeV, and even deuterium 3.34 MeV (NNDC QCalc, retrieved 2026-08-23) - so these neutron numbers do not set its shielding scale. They start to as soon as the machine accelerates deuterons, because D-D and Be(d,n) are exoenergetic with no threshold at all (dg-1047), or pushes protons past ~1.9 MeV on lithium; dg-1041 and dg-1047 carry the residual channels that keep a neutron survey honest below that. Read this as a scale for the case that applies, not as a clearance for the case that does not. [Corrected 2026-08-22: previously said neutron shielding is "a non-issue" for the machine; the exception clause was there, but the headline was an absolute.] [Corrected 2026-08-23: the exception clause itself was imprecise - it said the neutron channels "open far lower" for Li, Be, B or a deuterated material, but every one of those (p,n) thresholds is above 1 MeV as well; the genuinely thresholdless route is deuterons, per dg-1047. Raised by an upstream review of the source dataset.] [Corrected 2026-09-13: previously claimed 'below every (p,n) threshold'; thresholds are properties of nuclides, not of matter, and mid- and heavy-Z nuclei can sit far lower - 115In(p,n)115Sn is open at 287 keV, Coulomb-suppressed (NNDC QCalc; see the safety page's activation section) - so the claim is now scoped to the structural metals and light targets actually checked. Raised by an external site review.]
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Turn separation from acceleration alone is dr = R*(dE/turn)/(2E), so at fixed radius doubling the dee voltage doubles the turn spacing.
dr0/r0 = (1/2)*(dE0/E0); more exactly dR/dn = R*(dE/dn)/E * gamma/(gamma+1) * 1/nu_r^2Source quote & editorial note
the relative radial increase is only half the relative energy increase. However, for a given cyclotron, the turn separation dr0 will double when the dee voltage is doubled.
Kleeven & Zaremba, Cyclotrons: Magnetic Design and Beam Dynamics — CAS 2015, arXiv:1804.08961 (2018) — p. 44
Editorial note, tabletop extrapolation: The reference machine (~150 keV, 2.6 keV/turn, r ~ 9.6 cm) gets ~0.8 mm/turn. A 10 kV dee at the same radius scales it by the ratio of per-turn energy gains - computed from the actual voltage convention and gap count: 10 kV peak with two crossings at good phase is ~20 keV/turn, ~6 mm; one effective crossing or poor phase halves it or worse.
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Professional-scale reality check: 30 MeV with 100 keV/turn at R=0.5 m yields only 0.83 mm turn separation, versus a typical 4 mm radial beam width - acceleration alone rarely separates turns.
dr = R*dT/(2T)Source quote & editorial note
for a final energy of T = 30 MeV, dT = 100 keV, and an extraction radius of 0.5 m, we find dr = 0.83 mm. This is a rather small number, e.g. when compared with a radial beam width of for instance 4 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 6
Editorial note, tabletop extrapolation: Small machines fare better because dr/R scales as dT/T: a 350 keV next machine at 10-20 keV per turn carries a fractional turn separation 9-17x this 30 MeV machine's. Its beam width does not shrink in proportion, though - so the separation-vs-width comparison still needs the machine's own numbers (dg-495).
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Maximum extra turn separation from precession is 2*pi*(1-nu_r)*x; a 3 mm coherent amplitude accelerated to nu_r=0.8 buys 3.8 mm, added on top of the acceleration term.
dr_precession(max) ~ 2*pi*|1 - nu_r|*x near integer tune (the exact sinusoidal maximum is 2*x*|sin(pi*nu_r)| - 3.53 mm for the quoted 3 mm, nu_r = 0.8 case)Source quote & editorial note
when a coherent oscillation amplitude x of 3 mm has been built up ... and acceleration takes place until vr = 0.8, the maximum turn separation due to precession is 3.8 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 7
Editorial note, tabletop extrapolation: A deliberate few-mm coherent amplitude (source off-centering is one way to seed it), plus letting nu_r fall toward 0.8 in the fringe, can multiply turn spacing severalfold - IF the precession phase is arranged so the separation appears at the septum azimuth. It is a designed, tracked orbit-dynamics move, not a free effect.
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A first-harmonic field bump displaces the equilibrium orbit by dx = eps1*R/(nu_r^2-1); eps1=1e-4 (about 0.6 G in a 0.59 T field) at R=1 m and nu_r-1=0.01 already gives 5 mm.
dx = eps1*R/(nu_r^2 - 1), eps1 = B1/B0Source quote & editorial note
taking eps1 = 10-4, R = 1 m and vr - 1 = 0.01, one finds an orbit centre shift, i.e. a radial oscillation amplitude, of dx = 5 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 9
Editorial note, tabletop extrapolation: Gauss-level azimuthal asymmetry matters at 0.59-0.89 T NEAR nu_r = 1: the (nu_r^2 - 1) denominator is what turns the quoted 0.6 G into 5 mm, and the sensitivity falls away from the resonance and shrinks with radius. It is both the knob (a deliberate shim or coil bump) and the hazard (uncontrolled bumps de-center the beam) - dg-562's tolerance computation is the same physics from the defensive side.
Cited in: Beam Dynamics: An Interactive Laboratory
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Electrostatic deflector design point: give the beam a 50-100 mrad kick; septum entrance a few tenths of a mm (0.1 mm in modern IBA practice) thickening to several mm at exit, with a V-slit entrance to spread heat.
theta = E_gap*L/(2T/q) for nonrelativistic protons (pv = 2T)Source quote & editorial note
An angle kick of typically 50 to 100 mrad is provided. The inner electrode, septum, is at earth potential. At the entrance it has a thickness of a few tenths of a mm, increasing to several mm at the exit.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 14
Editorial note, tabletop extrapolation: At 350 keV a 100 mrad kick over 10 cm of arc needs E = theta*(2T/q)/L = 7 kV/cm - about 3.5 kV across a 5 mm gap. At nanoamp beams the septum's heat load is negligible whatever fraction it intercepts: 1 nA of 350 keV beam carries only 0.35 mW in total.
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Deflector discharge limit (Smith-Grunder): keep V*E < 1.5e4 kV^2/cm, and derate the holdable voltage another 20-30% because the deflector sits in a magnetic field.
V[kV] * E[kV/cm] < 1.5e4Source quote & editorial note
a criterion for the product of electric field E and potential V for a cyclotron deflector in order to avoid electric discharges: VE < 1.5 104 (kV)2/cm. The maximum sustainable voltage in a magnetic field is 20-30% lower.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 14
Editorial note, tabletop extrapolation: A 3-5 kV, 5-10 kV/cm tabletop deflector sits orders of magnitude below this bulk-discharge criterion - so at tabletop scale the practical ceiling comes from feedthrough, surface and edge-radius engineering (dg-353, dg-297, dg-295), not from the Smith-Grunder product.
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Round every HV electrode edge: peak field at an edge of radius r facing a gap a is Emax = 0.9*V/(r*ln(a/r)); Rutgers chose 3/16-inch edge radii to keep peaks at 170 kV/inch (67 kV/cm) against aluminum's ~290 kV/inch limit.
Emax = 0.9*V/(r*ln(a/r))Source quote & editorial note
At HV edges, electric field lines become so dense that breakdown becomes a major concern. Aluminum=290 kV/inch ... We settled on a minimum radius of R=.1875 inches ... Emax=170 kV/inch
Editorial note, tabletop extrapolation: Direct amateur precedent: a 1 T / 472 keV university tabletop deflector ran at 28-32 kV. A lower-energy machine needs proportionally less deflector voltage (scaling roughly with beam energy at similar geometry - a 150 keV-class machine perhaps a third, not a tenth), and the edge-field formula stays the design check: generous radii reduce peak field, they do not make sparking impossible - finish and conditioning still rule (dg-295, dg-353).
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Classical-cyclotron deflector sizing (MIT 42-inch practice): peel to DR = 0.1R-0.2R (0.15R typical); for 16 MeV deuterons at R=18.75 in with 0.3 in gap that meant 47-87 kV, with the channel tapered from ~1/8 in at entry to ~1/2 in at exit.
Vd = (2T/q)*d*DR/(R*(R+DR)) (uniform-field estimate)Source quote & editorial note
For DR = 0.1R: Va = 47,000 volts ... A typical figure, used in the MIT cyclotron, is a DR of 0.15R. ... The deflector gap is usually tapered.
Livingston & Blewett, Particle Accelerators (1962) — p. 163-166
Editorial note, tabletop extrapolation: Scaling by 2T: a next machine at 350 keV needs about 1/45 of MIT's voltage at the same normalized geometry - roughly 1-2 kV across a proportionally scaled entry gap - rising if a faster peel (larger DR) or a larger gap is wanted. Compute with the formula for the actual geometry (dg-590's worked example).
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The efficiency ladder for extraction, rung by rung and source by source: ~10% for early synchrocyclotron precessional extraction (Botman), up to 25% of internal beam for a well-tuned classical-cyclotron deflector under optimum conditions (the quoted machine), 75-80% for IBA self-extraction and >90% for modern well-centred precessional methods (Jongen, CYC2004).
Source quote & editorial note
Emergent beam intensities up to 25 per cent of the resonant beam intensity have been obtained under optimum conditions; ... practical operating intensities would in this case be limited to 80 or 100 [micro]a.
Livingston & Blewett, Particle Accelerators (1962) — p. 166
Editorial note, tabletop extrapolation: Plan a next machine's deflector attempt around the classical rungs - tens of percent at best, and that under optimum tuning: with nA internal beam, 0.1-0.25 nA external is still a countable, PIXE-usable beam. The upper rungs belong to machine classes a tabletop deflector does not reach.
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Multi-turn extraction energy spread is of order the per-turn gain, ~2*q*Vdee in the simple picture; single-turn extraction requires RF phase width |phi| < sqrt(2/N) - a few degrees for hundreds of turns - and correspondingly tight field stability.
|phi| < arccos(N/(N+1)) ~ sqrt(2/N)Source quote & editorial note
This results in a phase acceptance of only a few degrees for the typical case of a few hundred turns.
Baartman, Cyclotrons: Why/How Are Their Dynamics Different? — JINST 18 T03005 (2023) — p. 10
Editorial note, tabletop extrapolation: Do not chase single-turn extraction on a small machine: accept multi-turn with spread of order the turn energy gain (~20 keV at a 10 kV dee - the simple-picture floor; turn overlap and precession can widen it), which PIXE tolerates. (Spread and dB/B detail: botman pp.11-14.)
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Extraction purely by acceleration (no deflector) is possible only if turn count Nt <= (R/g)^2/(pi*Nh*gamma*(gamma+1)) - i.e. the pole half-gap g at extraction must be tiny compared to radius R.
Nt <= (1/(pi*Nh*gamma*(gamma+1))) * (R/g)^2Source quote & editorial note
it is mostly the squared ratio of extraction radius and pole gap at extraction which determines the maximal number of turns or the minimal energy gain
Baumgarten, Cyclotron Beam Extraction by Acceleration — arXiv:2205.04124 (2022) — p. 5-6
Editorial note, tabletop extrapolation: A next machine with R ~ 10 cm and half-gap 1.27 cm allows at most ~9 turns by the bound (needing ~18 keV per turn); shrinking the edge half-gap to 6-7 mm allows ~32-44 turns - a few keV per turn, reachable for a 5-10 kV LDMOS dee.
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H- stripping extraction converts nearly all intercepted ions with a simple device - a carbon foil of 50-200 ug/cm2, lifetimes above 2e4 uAh - and makes extracted energy variable by foil radius, at the price of an H- source, stringent vacuum, and the residual losses stripping keeps: interception geometry, scattering, straggling, foil heating and finite life.
dT/T = 2*dr/r sets extracted energy spread from radial beam widthSource quote & editorial note
the negative hydrogen ion beam simply passes a thin carbon foil (e.g. pyrolytic graphite, typically 50 to 200 ug/cm2), which strips off the electrons.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 3-4
Editorial note, tabletop extrapolation: At sub-MeV a 50 ug/cm2 foil costs ~10 keV of energy and some scattering. The septum, HV and turn-separation problems genuinely disappear - replaced by the H- problems: an internal H- source, and the 1e-6 Torr-class vacuum that gas stripping of the fragile H- demands (dg-599).
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H- gas-stripping cross-section is maximal exactly in the 0.1-300 keV range; the compact AMIT design (8.5 MeV, 4 T) loses (14.6 +/- 1.5)% at ~1e-4 hPa central pressure, while a 70 MeV machine at ~1.5e-6 mbar transmits ~87%.
T = exp(-n*sigma*L), n[cm^-3] = 3.3e16 * P[Torr], L = total spiral pathSource quote & editorial note
the cross section of H- interactions with the gas molecules is maximal for the energy range (0.1 - 300) keV of the beam in the central region.
Calvo et al., Beam Stripping Interactions in Compact Cyclotrons — PRAB 24, 090101 (2021) — p. 14
Editorial note, tabletop extrapolation: A next machine's H- variant spends its whole life at the cross-section peak. Run the loss arithmetic explicitly through T = exp(-n*sigma*L) with measured H- detachment cross-sections - the 1e-15 cm2 class near the peak; fetch sigma(E) for the actual gas mix when designing. At that scale ~25 m of spiral at 1e-6 Torr loses of order 5-10%, and 1e-5 Torr costs most of the beam: vacuum, not physics, decides this option. (70 MeV data: cyclotron_vacuum_model p.3.)
Cited in: The Vacuum Budget of a Cyclotron
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PIG discharges split into two families: cold-cathode (secondary-emission) arcs run above ~1 kV at 0.5-5 A, hot-cathode (self-heated thermionic) arcs run below ~1 kV at 1-50 A. The cold mode has positive incremental impedance, the hot mode negative — plan the supply accordingly.
cold cathode U_arc > 1 kV, I = 0.5-5 A; hot cathode U_arc < 1 kV, I = 1-50 ASource quote & editorial note
the cold cathode PIG source with arc voltages above 1 kV and currents between 0.5 and 5 A, and the hot cathode PIG source with arc voltages below 1 kV and currents between 1 and 50 A
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82
Editorial note, tabletop extrapolation: The reference machine's source at tens-to-hundreds of mA sits BELOW the handbook's canonical cold-cathode band, which starts at 0.5 A - closer to a glow regime than the tabulated arcs. The design consequence stands regardless: if the discharge crosses into a self-heated, negative-slope mode (AMIT reported a transition near 250 mA on their source), only a stiff current source holds it - so build the arc supply as a current source from the start.
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Above a minimum magnetic field of roughly 0.1 T the discharge parameters barely depend on B; ignition is easier at higher field. Ordinary internal PIGs run 0.1-1 T homogeneous.
B_min ~ 0.1 T; typical 0.1-1 T; little d(V,I)/dB above thresholdSource quote & editorial note
There is little influence of the magnetic field on the discharge parameters as long as it reaches a certain minimum of roughly 0.1 T.
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82
Editorial note, tabletop extrapolation: The reference machine's 0.59 T and a ~0.9 T successor both clear the handbook's 0.1 T minimum, so field-level effects on the ARC parameters should be small per the quote. Ignition and stable running still ride on pressure, geometry and surfaces (dg-372's ignition margins) - after a large field retune, a quick arc-parameter check beats an assumption.
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Ion current density at the cathodes is 5-10x that at the anode wall; total extracted current is proportional to arc current, roughly 10-100 (mA/cm^2) per ampere of arc for radial extraction through the anode slit.
j_cathode = (5-10) x j_anode; I_extracted/area ~ 10-100 (mA/cm^2)/A_arcSource quote & editorial note
the ion current density at the cathodes is five to ten times the density at the anode surface ... The total extracted current of a PIG ion source is proportional to the arc current (Figure 5.6), and for extraction through the anode, about 10 to 100 (mA/cm2)/A
Wolf (ed.), Handbook of Ion Sources (1995) — p. 82-83
Editorial note, tabletop extrapolation: Sizing arithmetic for the chimney slit: a 0.5 x 5 mm slit (0.025 cm^2) at 100 mA arc predicts ~25-250 uA available at the slit — consistent with Forringer's measured 230-590 uA at 50-150 mA through a 0.5 mm slit.
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Wolf Table 5.5's cold-cathode column, as extracted (the quote line verifies the gas row against the page image): arc 1-5 kV at 1-5 A, ignition 5 kV, duty <=25%, B >= 0.4 T, source gas pressure 1-10 Pa, gas consumption 0.2 sccm, ion current <=5 mA, anode aperture 1.5 x 25 mm, anode canal 6 mm dia, cathode 9 mm dia, cathode spacing 6.5 cm.
see rule; gas consumption 0.2-0.6 sccm across all PIG types in the tableSource quote & editorial note
Gas consumption (sccm) 0.2 [hot cath.] / 0.2 [cold cath.] / 0.2-0.6 [heated cath.] (Table 5.5; verified against page image)
Wolf (ed.), Handbook of Ion Sources (1995) — p. 101
Editorial note, tabletop extrapolation: The headline for the reference machine is the gas line - full-size accelerator PIGs run on 0.2-0.6 sccm, and its own hydrogen feed is a 1-sccm-full-scale mass-flow controller, so what the chimney buys is not less gas but gas confined where the ionization happens. Dimensions scale down for a 36 mm pole gap (its chimney will be shorter than the 6.5-10 cm cathode spacings listed, which are for big-gap machines).
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Cold-start ignition per Clark's account: raise the arc voltage to about 3 kV and increase gas pressure; the struck arc is then stabilized by the supply's current regulator or ballast resistor, with dc arc currents of 1-15 A (the quote). Corroborating machines carry their own figures: AMIT (to -3 kV with a gas boost near 10 sccm, striking in seconds, sustaining under 1 kV) and Forringer's 3 kV current-limited supply (dg-415).
V_ignite ~ 3 kV (Wolf table gives 3-5 kV); V_run = 0.3-2 kV; gas boost then reduceSource quote & editorial note
An arc is struck by raising the arc voltage to about 3 kV and increasing the gas pressure ... is stabilized by the arc supply current regulator or ballast series resistor ... Arc currents are 1-15 amps for dc sources and higher for pulsed sources. Arc voltages are 300-2000 volts.
Clark, Ion Sources for Cyclotrons — Cyclotrons '81, Caen (1981) — p. 3
Editorial note, tabletop extrapolation: Spec the arc supply for ~3 kV compliance even though running voltage is ~0.3-2 kV, and automate the sequence - gas up, strike, gas down, current-regulate - with the boost magnitude and timing tuned on the machine rather than copied.
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Internal-source extraction in Clark's survey: the anode/chimney is grounded and the dee's RF does the extraction via a puller or feeler, at 30-100 kV of RF on the full-size machines; his external sources run 10-30 kV DC with the anode biased positive.
internal PIG anode at ground; extraction field = dee RF via puller; 30-100 kV RF (big machines)Source quote & editorial note
Source extraction voltage is 10-30 kV dc for external sources, with the anode being biased positive. For internal sources, the anode is usually grounded and 30-100 kV of rf voltage is used for extraction
Clark, Ion Sources for Cyclotrons — Cyclotrons '81, Caen (1981) — p. PDF p.3 (printed p.233 of the 9th Int. Conf. on Cyclotrons proceedings)
Editorial note, tabletop extrapolation: The reference machine extracts with its few-kV dee - far below the surveyed machines. Compensating with a small source-puller gap follows Child-Langmuir-like scaling (I ~ V^1.5/d^2 in the planar model - a guide in this geometry, not a law): documented small gaps run 2.3-2.9 mm (Siemens, K100 - dg-624), and expect proportionally lower current than published microamp figures until measured.
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Cathode-anode gap in the NSCL/ACCEL cold-cathode source was anywhere from 1.9 to 3.8 mm and 'is not a critical parameter'; the thesis's practice pairs that with 100-grit cathode sanding (early screwdriver-scratching proved unnecessary) and the essential water cooling of cathode rod and anode base (dg-416's melted-copper lesson).
cathode-anode gap 1.9-3.8 mm, non-criticalSource quote & editorial note
The cathode anode gap was between 0.075" (1.9 mm) and 0.150" (3.8 mm), and is not a critical parameter for the source's operation.
Editorial note, tabletop extrapolation: Generous tolerance on the AXIAL gap - that part of the chimney stack-up doesn't need precision. Concentricity and slit alignment are separate tolerances with their own tighter demands, and the cooling warning stands at any arc power: provide a conduction path sized for continuous arc wattage, or plumb water.
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This cold-cathode source family has run at 4.5 T in the Harper Medical Cyclotron and at 0.5 T in NSCL test-stand low-field checks; the thesis's test-stand practice: base vacuum in the 1e-6 Torr range (gas off) for consistent starts, with 2.5 sccm of H2 putting the chamber at 4e-5 Torr under 600-800 L/s of turbo pumping.
B operating range 0.5-4.5 T demonstrated; base vacuum ~1e-6 Torr for reliable startsSource quote & editorial note
there needs to be a base vacuum (with the ion source gas supply turned off) in the 10−6 Torr range ... Various turbo pumps ranging from 600 to 800 liters/second were used ... With a gas flow rate of 2.5 cc/min of hydrogen, the pressure in the main vacuum chamber is around 4 × 10−5 Torr.
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. PDF p. 39 (printed p. 29) for the vacuum/flow practice; PDF p. 27 (printed p. 17) for the 4.5 T / 0.5 T endpoints
Editorial note, tabletop extrapolation: The reference machine's 0.59 T sits just inside the demonstrated field range - demonstrated at the endpoints, not characterized as uniform performance across it - and its existing turbo and 1e-6-class base pressure match the thesis's start conditions as-is.
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Puller geometry from the same source family: test-stand puller radius 12.7 mm with 5.0 mm minimum chimney-puller gap at 50 kV design voltage; the K100 medical cyclotron puller runs a 2.9 mm minimum gap (at ~20-40 kV RF), with the puller center deliberately offset 0.5 mm from the chimney center.
gap 5.0 mm at 50 kV; 2.9 mm (K100); offset 0.021" between chimney and puller centerlinesSource quote & editorial note
The chimney is centered at (0.000,0.000) and the puller is centered at (0.021,0.000). The minimum gap between the chimney and the puller is 2.9 mm while the gap at the source opening is 3.0 mm, meaning that the beam does not see the peak electric field. [K100 geometry]
Forringer, Phase Space Characterization of an Internal Ion Source for Cyclotrons — MSU dissertation (2004) — p. 78, 85
Editorial note, tabletop extrapolation: Gap sets extraction field at fixed voltage, so at a few kV on the dee the chimney-puller gap must shrink below these machines' values to recover useful gradient - but there is no constant-kV-per-mm law to size it by (dg-419): pick a gap, then verify holdoff on the bench with the actual electrodes, finish and RF. The K100's deliberate 0.5 mm center offset - trading peak field at the beam for extraction optics - is the transferable design idea.
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Alignment sensitivities: an off-center cathode (relative to anode bore and B axis) produces dramatically fewer secondary electrons with shorter confinement lifetimes; extraction is optimized over a mere -0.2 to -1.5 deg of anode (slit) rotation relative to the puller (>50% extraction inside that window), with the puller 2.2 mm from the anode aperture.
cathode-anode-B coaxiality critical; slit-to-puller rotational alignment ~1 deg classSource quote & editorial note
the properly aligned configuration produces significantly more secondary emission electrons ... with the anode rotation angles from -0.2 to -1.5 degree, more than 50% H- beam can be extracted through pullers
Mu et al., Simulation of Electron Behavior in PIG Ion Source for 9 MeV Cyclotron (2015) — p. 4-6
Editorial note, tabletop extrapolation: Two different tolerance classes: build the chimney concentric (pin the cathode discs to the bore, machine in one setup), and provide an external rotational adjustment of the source stalk with sub-degree feel for slit-to-puller aiming. The KIRAMS optimum spanned about a degree, so an adjustment range of a few degrees around nominal is the class to design for - the actual optimum is found on the machine, not inherited.
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A chimney over a filament converts an open e-bombardment source into a column source: thermionic electrons travel the full chimney to the median plane, ions form in the whole column, and a small aperture (1/16", 1.6 mm) facing the dee releases them into the gap with field lines naturally matched to the first orbit.
chimney aperture 1/16" (1.6 mm) toward dee (Rutgers 12-inch)Source quote & editorial note
The inclusion of a chimney placed on top of the existing design will permit the thermionic electrons to travel to the median plane, thereby generating ions in the entire column. A small aperture, 1/16 of an inch in diameter, opening towards the DEE permits ions to be drawn into the accelerating field.
Koeth, Rutgers 12 Inch Cyclotron Ion Source Studies: Part I (2006) — p. 2-3
Editorial note, tabletop extrapolation: The half-step option: chimney-over-filament keeps the reference machine's existing filament supply and adds gas confinement plus a defined 1.6 mm emission aperture. Injection matching to the first orbit remains its own design question (aperture position, puller, phase - dg-348), not an automatic property; a PIG chimney gets the same geometry benefits and deletes the filament, at the price of a new arc supply (dg-383).
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Before freezing a magnet design, survey parameters on a cheap small-scale model magnet (CIT used 2-inch poles for wide surveys, then 6", 9", and final-geometry models) rather than computing everything.
Source quote & editorial note
A series of studies were made on a model magnet with poles 2 inches in diameter. This could be changed quickly and cheaply to give rough data over a wide range of parameters.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 7
Editorial note, tabletop extrapolation: General magnet practice, transferable with its limits: a small bolt-together model surveys geometry cheaply (CIT's 2-inch scans were 'rough data over a wide range'), while saturation and B-H behavior do not scale - same-steel-same-B is what made scaled prediction land elsewhere (dg-1322). The model surveys shape; full-size verification still happens, or FEMM plays the model's role (dg-1089).
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Optimize coil height (and yoke/pole area ratio) by minimizing combined steel + copper + power cost; the cost minimum is flat, so deviating for mechanical convenience costs little.
minimize cost(steel) + cost(Cu) + cost(power) vs coil height and A_yoke/A_poleSource quote & editorial note
The coil height giving the minimum cost was found for a field of 20,000 gauss. Since the cost curve had a flat minimum this resulted in little increase in cost.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 8
Editorial note, tabletop extrapolation: General magnet economics in FORM: minimize steel + copper + power cost for your own prices and expect a flattish minimum near the optimum - CIT's flatness belonged to a 20-kilogauss design at 1950s prices, so re-run the small optimization with today's numbers before leaning on the flatness for convenience deviations.
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Do not count on holding the field up beyond about 90% of the pole-face radius: the source's shim studies hit that limit because the pole cross-section was too small just below the face - thickening the pole there is the lever they identify.
Source quote & editorial note
Shim studies showed it would be very difficult to hold up the field out to a radius greater than 90 percent of the pole face radius. This was due to the pole cross-section being too small just below the pole face.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 9
Editorial note, tabletop extrapolation: Directly applicable planning figure: budget usable beam radius near 90% of the 8-inch pole (~3.6 in) - and let the machine's own field map set the real number (dg-098's fringe accounting).
-
Design the vacuum chamber to split and withdraw without disturbing the shimmed magnet pole tips, so chamber service never invalidates the field map.
Source quote & editorial note
The chamber parts into two halves in a vertical plane through the center of the magnet, permitting the removal of the chamber without disturbing the magnet pole tips.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 15
Editorial note, tabletop extrapolation: Directly applicable packaging rule: make the next machine's chamber removable or serviceable in place without unbolting pole tips or shims - and still re-verify the field after any reassembly that could have moved iron. Undisturbed tips make the recheck quick, not unnecessary.
-
Support the dee on insulating columns 'making it possible to provide a DC bias' - CIT's design summary planned 1000-2000 V (NYO-780 p.75).
dee DC bias 1000-2000 V (NYO-780 summary, p.75)Source quote & editorial note
It is supported on insulating columns, making it possible to provide a DC bias.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 15
Editorial note, tabletop extrapolation: A DC-isolated dee mount costs little at design time and provides the discharge-control knob the era's reports repeatedly reach for (dg-320, dg-680, dg-805). A kilovolt-class bias means the mount and its feed are HV-insulated by design, not as an afterthought.
-
Stack removable radiation shielding in two staggered layers so no straight-through cracks remain [the source prints 'stacked in two vertical layers to that no straight-through cracks remained' - 'to' is an original typo for 'so']; where density matters the report's magnetite concrete reached ~200 lb/ft3 with 3000 psi crush strength and ~10% water (commercial magnetite + Portland cement, per Creutz & Downes 1949).
magnetite concrete ~200 lb/ft3, 3000 psi at 28 days, ~10% waterSource quote & editorial note
A density of 200 pounds per cubic foot was obtained with a 28 day crushing strength of 3,000 pounds per square inch and a water content of 10 percent. ... All removable shielding blocks were stacked in two vertical layers to that no straight-through cracks remained.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. PDF 43 (printed p. 38), Section VIII - SHIELDING
Editorial note, tabletop extrapolation: Transferable - stagger any shielding blocks on a next machine (concrete, water, borated PE) so seams never line up with the beam plane.
Cited in: Shielding a Small Cyclotron
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Interlock access doors and enclosures so they cannot open without turning off the cyclotron oscillator or moving the magnetic field off its resonance value.
Source quote & editorial note
they cannot be opened without turning off the cyclotron oscillator or reducing the magnetic field from its resonance value.
Creutz, Design and Construction of Synchro-Cyclotron — NYO-780 (1950) — p. 44
Editorial note, tabletop extrapolation: Directly applicable: interlocking RF-enable to the enclosure door is the cheap, classic scheme. Prefer the oscillator-off condition as the gate - an off-resonance field reduces acceleration but leaves RF and high voltage energized, so field detuning alone is not a conservative personnel interlock.
Cited in: Shielding a Small Cyclotron
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Budget vacuum RF gaps from bench data, then derate for surface roughening: an 0.080-inch polished copper gap held 50 kV at 13 Mc and 5e-6 mm on the bench (625 kV/in; 40 kV was the design value), while the discharge-roughened operating unit held ~30 kV over its 0.060-inch gap - 500 kV/in, about 20% lower in average field.
bench: 50 kV / 0.080 in = 625 kV/in (polished Cu, 5e-6 mm, 13 Mc); design ~80% of bench; roughened unit: 30 kV / 0.060 in = 500 kV/in (~20% field derate)Source quote & editorial note
a .080" gap between copper or copper-plated surfaces having a reasonable polish would hold a maximum of 50 kilovolts at 13 mc at a pressure of about 5 x 10-6 mm.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 13
Editorial note, tabletop extrapolation: Directly applicable breakdown data for setting a next machine's dee-to-liner and puller gaps at 5-13 kV - with the derate compared in FIELD, not voltage (the two units had different gaps), and remembering vacuum RF hold-off does not scale as fixed kV-per-gap: bench-verify the actual geometry (dg-419).
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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 — as the report's stated consequences of that scaling choice, not measured model results — power x2 and Q x 1/2 for equal voltage. The measured comparison is effective dee capacitance well below static: 500 vs 1600 uuF. [2026-09-06 erratum, scan re-read: the static capacitance is 1600 uuF, not 1000 pF, and the power/Q figures are scaling consequences, not measurements.]
1/n scale -> f x n, L and C / n; stated consequences: power x2, Q x 1/2 for equal voltage; measured: effective 500 uuF vs 1600 uuF staticSource quote & editorial note
For reasons of convenience, a quarter scale was chosen. The resonant frequency is then increased fourfold and all inductances and capacitances are reduced by a factor of four.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 14
Editorial note, tabletop extrapolation: Transferable method: prototype a next machine's resonator at reduced scale with a VNA - remembering effective dee capacitance is not the static value, which is exactly what the model run is for.
-
Expect small dimensional errors in RF models and layouts to accumulate - the quoted case: about two inches of cumulative model error produced a transmission-line-length discrepancy, with consequences the report details (scan re-read queued); build in adjustment range.
Source quote & editorial note
The evident discrepancy in transmission line length was eventually traced to a cumulative error of about two inches in various small errors in model dimensions.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 22
Editorial note, tabletop extrapolation: Directly applicable: give a next machine's resonant line or tank a deliberate tuning range - trombone section, tuning vane, trimmer capacitor - instead of trusting calculated dimensions to land the frequency.
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Cure resonant-electron/multipactor discharges in large volumes around the dee by cutting down the free volume with perforated grounded shields, adding a grounded dummy dee, and applying negative DC bias to the dee.
Source quote & editorial note
All discharges were eliminated by cutting down the available volume by means of perforated shields around the sides of the dee, by adding a grounded dummy dee and by applying a negative bias to the dee.
MacKenzie et al., Design of the Radio-Frequency System for the 184-inch Cyclotron — UCRL-64 (1948) — p. 23
Editorial note, tabletop extrapolation: Directly applicable - the 1948 combination that cleared THAT machine's discharges: reduced free volume (perforated shields preserve pumping speed), a grounded dummy dee, and negative dee bias. On a new machine, apply the elements as diagnosis suggests (dg-1273's discrimination between multipactor and gas discharge) rather than as one obligatory bundle - though all three are cheap to design in from the start.
-
Calibrate dee-voltage-per-watt expectations from this report's machine: its oscillator produced 15 kV peak on the dee at 10 Mc (9 kV at 20 Mc) for 6 kW input at ~70% average efficiency; the report elsewhere identifies the machine and tube complement (scan re-read queued for those details).
15 kV dee at 10 Mc for ~6 kW input, ~70% efficiency (37-inch dee, C ~ 300 pF)Source quote & editorial note
It would produce 15 kv peak volts on the dee at 10 me and 9 kv at 20 me with 6 kw input. It averages around 70%.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 4
Editorial note, tabletop extrapolation: A benchmark near the reference machine's 9 MHz - and transferring it runs through the resonator parameters: scale by the actual dee capacitance and Q via dg-313's formula, not by watts-per-kV alone.
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Provide a tuning vane - a movable copper sheet with flexible end connections facing the resonant line - to trim the resonant frequency without rebuilding the line; on the source machine the vane's range was about 6%.
vane travel -> ~6% frequency trim of the resonant lineSource quote & editorial note
The upper and lower frequency limits can be varied together about 6% by a tuning vane which varies the impedance of the transmission line. It is a movable copper sheet with flexible end connections.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 5
Editorial note, tabletop extrapolation: Directly applicable to a fixed-frequency machine: a vane gives few-percent trim to land the dee resonance on the magnet's cyclotron frequency. The range you get depends on your line's geometry - size the vane by calculation and keep a fallback adjustment (dg-665's trombone/trimmer).
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Expect an electron-oscillation discharge that lives only below an extinction voltage near 500 V RF and blocks voltage build-up even at 1e-5 mm Hg; the 37-inch eliminated it with a sweeping field - biasing the dee, transmission line and condenser stator a few hundred volts POSITIVE - and the bias, unexplained, roughly doubled their beam.
discharge sustained only below ~500 V RF (the source's extinction neighborhood); any sweeping field kills it - the 37-inch used a few hundred volts positive biasSource quote & editorial note
Above this voltage, which is in the neighborhood of 500 volts, the discharge is rapidly extinguished as electrons can no longer oscillate. However, the discharge is usually intense enough, even at 10-5 mm of Hg to prevent the voltage from building up to this extinction value. Such a discharge can be eliminated by a sweeping field obtained in any manner. The sweeping field was obtained on the 37-inch cyclotron by biasing the dee, transmission line, and condenser stator parts a few hundred volts positive.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: The single most relevant discharge fact for the reference machine: its ~1.3 kV dee lives just above this regime, and the 5-13 kV upgrade must punch through it during every start - plan for a bias supply on the dee from day one, and note the source's polarity (positive on the 37-inch; dg-320's machine used negative - both worked, because any sweeping field defeats the resonance).
-
Keep RF-exposed electrode spacings along the magnetic field short: at 20 Mc an electron gains ~30 eV over a 5 cm path, so paths of ~20 cm sustain ionizing oscillation discharges while the short dee-region paths gave no trouble.
at 20 Mc, ~30 eV in 5 cm; danger paths ~20 cm; safe paths < ~5 cm (worse at lower f)Source quote & editorial note
At 20 megacycles the space between electrodes which will allow an electron to reach an energy around 30 volts in 5 cm. There are very few paths, along the magnetic field, in the neighborhood of the dee that are greater than this, so no trouble has occurred in this region. In the rotary condenser however, most of the paths are of the order of 20 cm. Electrons oscillating in this space can reach efficient ionizing energies long before their amplitude becomes equal to the distance between electrodes.
MacKenzie & Waithman, R.F. System for Frequency Modulated Cyclotron — MDDC-1045 (1946) — p. 12
Editorial note, tabletop extrapolation: Directly applicable geometry rule - at 9 MHz electron oscillation amplitudes are larger still, so keep open RF-exposed volumes and along-field gaps in the next machine's chamber small or shielded.
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Do not fight the n = 0.2 resonance for the last few percent: Berkeley POSTPONED accelerating past that radius because the available ion energy there was already within 5 percent of the system maximum (the specific radii and the n = 1 identification are the report's: scan re-read queued).
E_max at radius where n = 1; usable beam ends near n = 0.2Source quote & editorial note
accelerating particles past the radius where n = 0.2 in the 184-inch cyclotron has been postponed, since the available energy of the ions at this radius is within 5 per cent of the maximum of the system
Editorial note, tabletop extrapolation: Budget a next machine's energy at the n = 0.2 radius, not the pole edge - and where shims can push the n = 0.2 contour outward, that buys usable energy more surely than chasing radius into the fringe (dg-152's taper rule is the design form of the same point).
Cited in: Beam Dynamics: An Interactive Laboratory
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At n = 0.2 the coupling resonance omega_z = omega_r/2 converts radial oscillation energy into vertical oscillation at up to double the amplitude - and machines with low accelerating voltage (many turns per inch) build it up rapidly.
omega_r = sqrt(1-n)*omega_0, omega_z = sqrt(n)*omega_0; at n = 0.2, omega_z = omega_r/2 (the coupling resonance); the amplitude transferred depends on coupling strength and crossing speed - the doubling figure is the report's estimate for its machineSource quote & editorial note
It must be kept in mind for systems having low accelerating voltages similar to the 184-inch cyclotron, that the ions will rapidly increase the amplitude of their vertical oscillations at the point where n = 0.2.
Editorial note, tabletop extrapolation: The reference machine's few-kV dee means many turns near any resonance radius - the slow-crossing regime the quote warns about. Keep n below 0.2 over the whole usable radius (the mapped check, dg-138), and give the dee aperture real margin over the expected radial oscillation amplitude.
Cited in: Beam Dynamics: An Interactive Laboratory
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Working small classical cyclotrons in the 1958 census ran as-run center fields of 12.3-19 kG (ISSP 16-in: 14-19; BNL 18-in: 13.1; Stanford 27-in: 12.3 as-run — its 12.5 was the design-sheet maximum; ANU 31-in: 12.6; Purdue 37-in: 16.2; Copenhagen 90-cm: 17.5) - none below ~12 kG in the tabulated set; iron near saturation was the cheapest energy. [2026-09-06 erratum, scan re-read: Stanford corrected 12.5 -> 12.3 kG per its X-882A ACTUAL PERFORMANCE DATA sheet; the census pairs design sheets (X-882) with actual-performance sheets (X-882A), and this band is the as-run one.]
K_p[MeV] ~ 48.2*(B[T]*r[m])^2; K_d ~ 24.1*(B*r)^2Source quote & editorial note
Mag. field, k-gauss 14 - 19
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: the reference machine's 0.59 T is a factor 2-3 below this tabulated population; pushing a next machine toward 1.2-1.5 T multiplies energy 4-6x at fixed pole radius - the route every tabulated machine took. The Stanford correction is the design-vs-operating-point lesson in miniature: the census itself splits design and as-run onto separate sheets, and the two differ.
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Dee-to-dee voltage in the census tracks energy loosely: ISSP's 16-inch ran 10-18 kV and still held 100 uA internal beam; larger 1-4 MeV machines ran to ~30 kV (Stanford 20, Tokyo 27), and 7-11 MeV machines 40-90 kV.
Source quote & editorial note
Dee-to-dee, kv 10 - 18 ... Internal Beam, Stable, ua 100
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Editorial note, tabletop extrapolation: Proof that low dee voltage works at small radius: ISSP is the existence proof for a sub-MeV goal on a ~10 kV-class dee. Dee voltage buys turn count, phase budget and survival - the energy ceiling stays with B*r (dg-026) - and the field profile must keep the extra turns focused.
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Oscillator budgets for the census's 16-31 inch machines ran 10-50 kW, dominated by self-excited single-tube circuits (ISSP: one 8T11R, 10 kW in / 6 kW out; Stanford: one RCA 899A, 12 kW; BNL: one 5771, 35 kW in / 20 kW out; ANU: 50 kW out).
Source quote & editorial note
Oscillator tube one 8T11R ... Osc. input, max 10 kw ... Osc. output, max 6 kw ... Oscillator tube one, RCA 899A ... Osc. input, max 12 kw ... Oscillator tube 3Q 260E (S.T.C.) ... Osc. output, max 50 kw
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. PDF 106 (printed -99-) as cited for BNL; ISSP on PDF 60 (printed -53-), Stanford on PDF 166 (printed -161-), ANU on PDF 26 (printed -19-)
Editorial note, tabletop extrapolation: Those kilowatts bought tens-of-kV dees at high Q, not beam power. A few-kV tabletop dee's budget comes from the resonator formula instead (dg-313: tens of watts dissipated, so a 100 W-1 kW amplifier class with margin) - and the census's plain self-excited oscillators show that sophisticated drive chains are not a prerequisite for running a cyclotron.
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Magnet iron grows steeply with pole diameter across the census: 16-in -> 6 tons Fe, 18-in -> 6, 27-in -> 10, 28-in -> 17, 31-in -> 31, Copenhagen 90-cm -> 35, Washington 54-in-core -> 70; copper or aluminum windings add 1-12 tons.
census tonnage vs pole diameter: growth is steep but not a clean power law - gap, yoke geometry and field vary across the setSource quote & editorial note
Weight, Fe 6 ; Cu 4 tons. Winding 3/4 in x 1/16 in strip.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 106
Editorial note, tabletop extrapolation: Extrapolating down the census, an 8-in-pole machine sits in the fraction-of-a-ton class - hobby-crane scale, and the reference machine's 757 lb H-frame agrees - while every inch of added pole diameter on a next machine is bought with steeply growing steel.
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Census geometry ratios - the quoted 31-inch row computes to: pole gap 17.7% of pole diameter, dee aperture 59% of the gap, dee diameter 93.5% of pole diameter, maximum beam radius 81% of pole radius; the census's smaller machines bracket similar ratios (full tabulation: scan re-read queued).
Source quote & editorial note
Pole tip dia. 31 in. Beam radius, max 12.6 in. Field gap, center 5.5 in. ... Dee dia. 29 in. Dee aperture 3 1/4 in.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 26
Editorial note, tabletop extrapolation: Sanity template for a next machine on 8-inch poles: ratios of this class suggest a 1-1.4 in gap, a 0.5-0.8 in dee aperture, and energy planned at a 3.2-3.6 in beam radius rather than the pole edge - starting proportions to check against the machine's own field map and stability analysis, not expected dimensions.
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Shim for a 2-4% total field drop-off from center to maximum beam radius - the census machines cluster tightly there as tabulated (Copenhagen 1.75%, ANU 2%, ISSP 2.5%, BNL 3%, Tokyo 25-in 3%, Rochester 3.4%). [2026-09-06 erratum, scan re-read: the Rochester sheet prints 'Field drop-off 3. 4 %' - a decimal 3.4%, not a 3-4% range, verified at 600 dpi against the sheet's other decimals; the tabulated cluster is 1.75-3.4%.]
total dB/B (center to r_max) ~ 0.02-0.04; tabulated census cluster 1.75-3.4%Source quote & editorial note
Field drop-off 3-4 %
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 164
Editorial note, tabletop extrapolation: Directly transferable as a SHAPE target for the reference machine's field: the fixed-frequency population converged on a smooth, monotonic few-percent total drop. The total constrains the average only - the stability check remains the local n(r) map (n > 0 throughout, staying clear of 0.2; dg-003, dg-138), which the same total drop can satisfy or violate depending on where the fall concentrates.
Cited in: Beam Dynamics: An Interactive Laboratory
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Internal beams of 100-3000 uA were routine on the census's small machines (ISSP 16-in: 100 uA deuterons; BNL 18-in: 1-2 mA protons; ANU: 3 mA); external beams ran far lower on most (Copenhagen 2%, ANU 8% of internal), with BNL's tabulated pairing - 800 uA external against 1000-2000 uA internal, nominally 40-80% - the outlier, and the table's values not necessarily simultaneous.
Source quote & editorial note
Internal Beam, Stable, ua 1000-2000 ... External Beam, Stable, 800 ua; 100 ua focused on target 15 ft from machine
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 107
Editorial note, tabletop extrapolation: If the reference machine sees nA, the gap to the historical uA-mA norm lives in source output and center-region transmission, not physics limits - and extraction cost most census machines most of their beam, so budget a next machine's external current pessimistically.
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Hooded low-voltage arc sources with hot filaments dominated the census's small machines as tabulated: ANU hooded arc with tungsten filament, BNL hot cathode in a copper arc house, Stanford hooded arc, ISSP hooded low-voltage.
Source quote & editorial note
Ion source, type hooded arc, tungsten filament
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 26
Editorial note, tabletop extrapolation: Population-level evidence that the hooded filament arc is the proven route to 100 uA-class internal beams at this scale - evidence of practice, not proof a cold-cathode PIG cannot compete (PIGs run cyclotrons too, dg-383): the choice trades filament fragility against arc-supply simplicity and delivered current.
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A variable-energy small cyclotron can hold its field profile over a range: ISSP varied 14 to 18 kG by coil current alone, keeping 1-2.5% drop-off at the 16-cm exit radius, with a variable-frequency self-excited oscillator following.
Source quote & editorial note
Magnetic field variable, by only changing the coil current, from 14 to 18 kg with 1 to 2.5% field drop-off at the exit (r = 16 cm).
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 61
Editorial note, tabletop extrapolation: The builder can trim B to match a fixed RF (or vice versa) and expect the shim profile to survive over a modest range - PROVIDED the iron is not driven into locally different saturation, which reshapes the profile. Measure n(r) at both ends of the intended current range before trusting it.
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Air-cooled magnet windings sufficed on documented small machines: the survey lists Stanford's 27-in (12.5 kG, 10 t Fe) and Howard's 16-in (15-16 kG) with air-cooled coils.
Source quote & editorial note
Air-cooled coils. Iron ore blocks for shielding
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 127
Editorial note, tabletop extrapolation: Precedent that air cooling can work at this scale - two real machines did - not proof that a given coil can: adequacy is set by I^2R dissipation, winding geometry, insulation rating, duty cycle and airflow. Do the dissipation arithmetic (magnet-power calculator) and monitor winding temperature (dg-220) instead of citing precedent.
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Whole working cyclotrons were built for $5k-$110k and about two years, per the census: Stanford 27-in cost $5000 plus $5000 in improvements (1940 to first beam July 1941); ISSP 16-in $40k with first beam 26 months after start; BNL 18-in $110k.
Source quote & editorial note
Construction started 1940. Completion date July 1941 ... Total cost $5000 initial, $5000 improvements.
Howard, Cyclotrons and High-Energy Accelerators, 1958 — ORNL-2644 (1958) — p. 166
Editorial note, tabletop extrapolation: Scope calibration: small teams on small budgets built working 2-4 MeV, 16-27 inch machines in this era. A next machine at the few-hundred-keV scale on 8-in-class iron - dg-697's K ~ 48*(B*r)^2 gives about 0.35 MeV at 1 T on an 8-in pole's usable radius - is historically a modest, well-precedented project.
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Keep DC supply voltage off RF conductors that run through the magnetic field in vacuum: a DC-biased line in the field can sustain a Phillips-ion-gauge-type discharge - the quote's warning; the discharge-to-window damage sequence is the report's incident account (scan re-read queued).
Source quote & editorial note
a Phillips-Ion-Gauge-type discharge can start in the magnetic field inside the vacuum tank near the positive transmission line
Editorial note, tabletop extrapolation: Very relevant at higher dee voltage on the reference machine or a next machine: crossed E and B in vacuum is exactly a PIG geometry - it is how the gauge and the source work - so route DC-carrying feedlines, bias leads and probe wires out of the field region or shield them. This failure mode is designed out at layout time.
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The dee must be a high-Q energy-storage resonator, never a switched load: brute-force reversing a 100 pF dee-to-liner capacitance at 100 kV and 10 Mc/s would demand 20 MW, versus watts-to-kilowatts to sustain the same voltage in a resonant system.
P_switched ~ 2*C*V^2*f for hard +V/-V reversals - each reversal moves the stored charge through 2V, so the source's 20 MW = 2 x 1e-10 F x (1e5 V)^2 x 1e7 Hz checksSource quote & editorial note
If this is done at the rate of 10 megacycles per second, the power requirement would be 20 megawatts!
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 13
Editorial note, tabletop extrapolation: The cleanest back-of-envelope argument in this collection for why dee voltage is bought with Q, not amplifier watts - scale it to a next machine (7-9.5 kV on tens of pF at 6.78 MHz) to show why a few hundred LDMOS watts suffice only through a good resonator.
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Multi-frequency drive pushed the source toward separate control: getting the third harmonic's phase and amplitude right was 'somewhat difficult' - and the report notes no serious self-excited driving system was attempted, so the comparison there is undeveloped, not decided.
Source quote & editorial note
It was somewhat difficult to get both the phase and the amplitude of the third harmonic adjusted correctly; however no serious attempt was made to develop a good self-excited driving system.
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 25
Editorial note, tabletop extrapolation: Mirrors the next machine's decision already leaning MOPA: independent control of each degree of freedom is the argument, and a DDS + LDMOS chain is the modern form - while the self-excited literature (dg-1367, dg-254) holds the other seat. This source records a difficulty, not a verdict.
Cited in: Driving the Dee: RF Coupling
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Size deflector gaps by the VE relationship: for equal sparking probability with given materials, gap voltage times cathode gradient is constant - the quoted relation (the experimentally tested gap range is the report's: scan re-read queued).
V(kV) * E(kV/cm) = const; equivalently V ~ K*d^0.5Source quote & editorial note
for equal probability of sparking with given materials, the product of gap voltage and cathode gradient is a constant.
Editorial note, tabletop extrapolation: For a next machine's deflector the trade falls out of a chosen VE number: a 3-mm gap at VE = 1.5e4 (kV)^2/cm predicts ~67 kV at ~220 kV/cm - far beyond tabletop needs (dg-590's few kV), which is the real point: tabletop deflectors sit deep inside the bulk-breakdown envelope, and surface/edge engineering rules instead (dg-591).
-
Derate the deflector to VE = 1.5e4 (kV)^2/cm for day-to-day operation even though 2.25e4 was held in tests: a one-third margin below best-demonstrated holding.
VE_design = 1.5e4 (kV)^2/cm vs 2.25e4 achieved (Fig. 10 design chart)Source quote & editorial note
In order to provide an adequate margin for day-to-day operation, a design value of 1.5 X 10^4 should be used.
Editorial note, tabletop extrapolation: The most quotable deflector design number in the collection: design to VE = 1.5e4 (kV)^2/cm and treat the tested 2.25e4 as commissioning margin - as the source machine practiced. Transfer it as a starting point under the usual conditions (electrode material, finish, conditioning - dg-353, dg-295), and verify on the actual electrodes.
-
Design the deflector supply to limit the energy delivered per spark, not to prevent sparks: the 88-Inch supply stores only 2.5 J at 120 kV (distributed across 1200 diodes), sparked virtually every second for 24 h/day for many days without damage, and its spark will not puncture 5-mil aluminum foil.
E_stored = 2.5 J at 120 kV; survives ~1 spark/s continuousSource quote & editorial note
it stores only 2-1/2 joules and, at most, this is distributed among 1200 diodes. ... There is so little energy in a spark from this rectifier that it will not puncture even a piece of 5-mil aluminum foil.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 28
Editorial note, tabletop extrapolation: The governing philosophy for a next machine's deflector supply: limit the energy delivered per spark rather than trying to prevent sparks - low stored energy is an equipment-survival property, and a sub-joule store at 50-100 kV is achievable. It is not a personnel-safety property: such a supply remains dangerous to people, and in human contact the supply's follow-on current adds to the stored energy. Personnel protection stays with enclosure, interlocks, grounding and discharge practice (dg-522, dg-654).
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Precessional/regenerative extraction must satisfy the quoted three requirements: (a) arrest the precession so the radial-oscillation maximum recurs at one azimuth, (b) obtain sufficient gain per turn - enough to step over the septum wall WITH entrance margin, and (c) minimize losses from axial blowup.
requirements: precession arrested; gain/turn > septum wall + entrance margin; axial losses boundedSource quote & editorial note
The extraction requirements, simply stated, are: (a) The precession must be arrested (b) Sufficient gain per turn must be obtained (c) Losses owing to axial blowup must be minimized.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 7
Editorial note, tabletop extrapolation: The cleanest checklist in this collection for what a next machine's precessional-assist extraction must accomplish - phase-lock the precession to place orbit maxima at the septum azimuth, then count gain-per-turn against septum thickness. Machine-class independent.
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The variable-energy argument for electrical extraction elements: the source's system - with tunable frequency AND gradient - eliminates the difficulties fixed magnetic extraction systems have on variable-energy machines, where static perturbations set into the pole geometry cannot follow a changing energy and field.
tunable (f, E) replaces fixed (B-bump geometry) for variable-energy operationSource quote & editorial note
The possibility of changing the electrical frequency and gradient to match operating conditions eliminates difficulties arising in magnetic extraction systems for variable-energy machines.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 4
Editorial note, tabletop extrapolation: Supports the next machine's plan-of-record (electrostatic deflector, no fixed magnetic channel) in spirit: an educational machine running several field/energy points wants extraction strength on a knob. A plain electrostatic deflector carries the voltage knob - not the source system's frequency knob - and that adjustability is exactly what a fixed B-bump lacks.
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Make ion-source position adjustable from outside the vacuum: the 63-inch found source-to-field alignment 'extremely critical', necessitating external adjustments - the 86-inch's Selsyn-driven rotator is the report's example implementation (scan re-read queued).
Source quote & editorial note
The alignment of the source with the magnetic field is extremely critical, as was expected, and makes it necessary to provide for external adjustments of the ion source.
Editorial note, tabletop extrapolation: Strong design input for a next machine: budget at least one externally accessible source degree of freedom (rotation or z) - both ORNL machines provided it after finding the optimum unreachable blind. Adjustment under beam is the convenient form; adjust-then-pump iterations reach the same optimum, slower.
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Apply a small negative DC bias (1-2 kV on the 63-inch) to the dees while RF oscillation is being established, to sweep out ions formed during startup and prevent them loading or destabilizing the rising RF.
dee bias -1 to -2 kV on the 63-inch's ~50 kV dees (2-4% of dee voltage) during RF establishmentSource quote & editorial note
A negative voltage bias, 1 to 2 kv, is applied to the dees in order to sweep out any ions that may be formed while oscillation is being established.
Editorial note, tabletop extrapolation: Transferable as a startup practice: a bias supply that sweeps ions out during RF ramp-up is the classical cure for start-up loading (dg-320, dg-680 - polarity differs by machine and both worked). What voltage a small machine needs is found at the machine; the 63-inch's 2-4% of dee voltage is the documented anchor, not a scaling law.
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Bench-test an ion source on a 180-degree beam path in the magnet before installing it: the 63-inch source was tested dc by collecting after a half-turn, measuring the species mix - 8 mA N+, 2 mA N++, 2 mA N+++ (the quoted result; the report's fuller qualification detail: scan re-read queued).
Source quote & editorial note
In dc tests the output of the source, measured after the beam had passed through a 180 deg path in the magnetic field, was: 8 ma of N+, 2 ma of N++, and 2 ma of N+++.
Editorial note, tabletop extrapolation: The 180-degree bend uses the cyclotron's own field as a mass spectrometer with the RF off — on the reference machine this is precisely the source-species test geometry: source + static field + offset collector measures the H+/H2+/H3+ mix directly before any acceleration studies.
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Central-region orbit centering couples source radial position to dee voltage: with the Davis axial source confined to r < 2.5 in, the machine is forced to comparatively low dee voltages (20-30 kV) so the first-turn radius matches the available source position and the orbits stay centered — dee voltage is set by geometry, not by available RF power.
first-gap geometry couples V_dee to source/puller radius: r_1 = sqrt(2*m*q*V_gap)/(q*B) for acceleration from rest through the gap potential - initial energy and RF phase correct it furtherSource quote & editorial note
the ion source position is limited to a maximum radius of 2.5 inches. This forces operation at comparatively low dee voltages (20-30 kv) in order to center the orbits.
Editorial note, tabletop extrapolation: The design logic transfers directly to a next machine's central-region layout: pick dee voltage and source-puller radius TOGETHER from the first-orbit geometry. It also cuts the other way for the reference machine's 5-13 kV upgrade: raising dee voltage moves the optimum source position outward — re-scan source position after the RF upgrade.
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Distrust scale-model magnet studies at excitation extremes: the Davis model magnet could not be operated at the extremely low planned field level (3.5 kilogauss) - the quoted limitation; the full-scale consequences and iron rework are the report's account (scan re-read queued).
Source quote & editorial note
it was not possible to operate the model magnet at the extremely low (3.5 kilogauss) field levels at which we might like to operate the full scale machine.
Editorial note, tabletop extrapolation: Modern translation for the FEMM pipeline: a model (physical or FEM) validated at one excitation does not certify another — iron saturation state changes the profile shape, so re-run the field solution at every planned operating point, especially the lowest, and verify the real magnet across its full excitation range.
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A computed field map validated by orbit code can produce first beam without empirical shimming iteration: Davis obtained a 21-MeV H2+ internal beam on the first attempt using the computed field, taken as confirmation of both the magnetic measurements and the orbit calculations.
Source quote & editorial note
the validity of the calculations and magnetic field data is supported by the fact that we obtained an internal beam of 21 MeV H2+ ions using the computed field on the first attempt.
Editorial note, tabletop extrapolation: The 1966 encouragement for a next machine's compute-first pipeline (field map -> tracker -> build): careful measurement plus an honest tracker produced first beam on the computed field, first attempt, on that machine. One result is precedent, not promise - keep shim stock on hand, and let the pipeline earn trust machine by machine.
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Design the magnet around the report's four field premises: a steel- and copper-free cylindrical 'gap' whose diameter is about nine times its axial height (the quoted ratio); mid-plane symmetry; no azimuthal dependence; and a field falling with radius gently enough that n = -(R/H)(dH/dR) stays well below 1/5 at all used radii - the report's working condition.
gap diameter ~ 9x gap height; n = -(R/H)(dH/dR) << 1/5 inside the used radius; field decreases linearly with radius to the gap edgeSource quote & editorial note
This region, called the "gap," should have a diameter about nine times as great as its axial dimension. ... n = - (R/H)(dH/dR) << 1/5 ... The desired field is one which decreases linearly with increasing radius to the outside "edge" of the gap.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. PDF p.6 = printed p.6 (TID-454, Technical Report No. 1, Sec. 1.1 Pole Tips, 'Introduction')
Editorial note, tabletop extrapolation: CORROBORATING, not new - the same premises underlie Livingston-Blewett and Wouters (corpus already carries 0<n<1 stability). TID-454's working condition is the stricter n<<1/5; note its own 130-in/14-in example is 9.3x. The reference machine's 8-in poles over a wide gap fall far short of 9x, which is exactly why usable radius is scarce; a next machine's gap choice should respect this proportion.
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Keep magnet coils as small as a reasonable power budget allows: coil resistance grows with mean circumference (the quote), and the steel circuit that must wrap around the coil grows with it - the report's steel-scaling expression accompanies the quoted argument (scan re-read queued).
R_coil ~ mean circumference; steel volume ~ (2*coil height + radial width); achieve small coils via high average conductivity (material, low temperature, high space factor)Source quote & editorial note
1. The resistance of the coil is proportional to its mean circumference. 2. An amount of steel approximately proportional to two times the height of one coil, plus the radial width of the coils, is required to complete the magnetic circuit.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. PDF p.25 = printed p.25 (TID-454, Sec. 1.2 Magnet Coils, 'Introduction')
Editorial note, tabletop extrapolation: The compounding is the point - on any H-frame rebuild, fat coils cost twice (copper AND the longer steel circuit around them), so invest in space factor and cooling before adding turns.
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In the report's practice, a high-current low-voltage magnet coil needs insulation only to maintain mechanical separation of the conductors; the report pairs this with direct cooling through a few large channels in large conductors rather than many small ones.
Source quote & editorial note
In a high-current low-voltage coil, insulation is required only to maintain mechanical separation of the conductors.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 25
Editorial note, tabletop extrapolation: What transfers is the architecture - few turns of heavy conductor at high current, direct cooling through generous passages - which beats many-turn fine-wire coils on space factor and pumping pressure. The bare-minimum insulation standard does not transfer: a modern coil wants verified turn-to-turn and ground insulation against inductive transients (dg-218's dump events), abrasion, thermal aging and coolant exposure, cheap as modern materials make it.
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When no large winding machine is available (winding on site), build the coil as a flat-wound helix of conductor pieces fabricated as annulus sectors and joined into a continuous helix, cooled by water tubes on the inner and/or outer circumference.
Source quote & editorial note
A second type of coil which is more attractive, when the coil must be wound at the cyclotron site, is a flat-wound helix.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 26
Editorial note, tabletop extrapolation: Directly a garage-scale construction technique: cut flat copper sectors, stack into a helix, join into a continuous conductor - no winding mandrel needed. The joints are the engineering: braze for permanent low-resistance splices, bolt only with designed contact pressure and area (the report's joint-sizing criterion: scan re-read queued for the number), and place cooling per the report's tube arrangement.
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Match the DC supply to the magnet coil so that (maximum voltage)/(maximum current) equals the coil resistance; otherwise part of the supply's capability can never be delivered.
V_max/I_max = R_coil for full utilization of the supplySource quote & editorial note
The generator should match the coil in the sense that the quotient of the maximum voltage output and the maximum current should be equal to the resistance of the coil.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33
Editorial note, tabletop extrapolation: When sizing a surplus supply for the next machine's coil - or the turn count for a given supply - pick turns so the coil's HOT resistance sits at the supply's V_max/I_max corner: copper rises 20-40% in resistance from cold, so a cold-matched coil starves at temperature. And confirm the supply can actually hold its corner continuously; not every surplus unit can.
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Keep the magnetic circuit short with wide, thin yoke sections, and proportion coils so that (coil OD - coil ID) over the sum of both coil heights is about 1 - both statements 'useful only as guides' per the source's own caution.
(OD - ID)/(h_coil1 + h_coil2) ~ 1, i.e. 2*(r_out - r_in)/(h1 + h2) ~ 1 in radial terms; yoke sections wide and thin (guides, not optimization results)Source quote & editorial note
Both the above statements need qualification and are useful only as guides.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33
Editorial note, tabletop extrapolation: Quick shape checks for an H-frame rebuild - square-ish coil cross section and flat wide return yokes - with the author's own warning not to treat them as optimization results.
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Put the magnetically good steel where it counts: the pole base is flux-critical and its optimum cross-section 'rather critical' - found from B/(dB/dH) equal to a cost ratio, landing near B ~ 21,000 gauss for low-carbon steel in the worked case - while the yoke's steel QUALITY matters much less.
solve B_B/(dB_B/dH_B) = cost ratio (Eq. 123); worked case gives 8.3e3 Oe -> B ~ 21 kG pole base (p.35), ~18 kG horizontal yoke (p.36), low-carbon steelSource quote & editorial note
it should be made of magnetically good steel, and the optimum size is rather critical ... the quality of steel used in this part of the magnet [the yoke] is less important.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33-36
Editorial note, tabletop extrapolation: For a next machine's steel shopping: spend on clean low-carbon (1006/1008) pole and pole-base stock and size the pole base deliberately - it is the critical dimension - while the return yoke tolerates lower-grade steel. Lower-grade still means characterized enough to size its area with margin (dg-132's measure-or-assume-conservatively), not mystery plate on faith.
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There is an optimum operating field for a given beam energy (bigger magnet at low field vs smaller at high field); it follows from balancing the marginal cost of scale (C = C3*S^3 + C2*S^2 + C1*S + C0, with E ~ S^2) against the marginal cost of excitation - and it cannot be pinned down without a model magnet close to final form.
C = C3*S^3 + C2*S^2 + C1*S + C0; E = E'*S^2; optimum where d(cost)/d(energy) via scale equals d(cost)/d(energy) via field (Eqs. 137-145)Source quote & editorial note
This field strength depends on the design and the size of the magnet and cannot be determined without a model magnet.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 33-38
Editorial note, tabletop extrapolation: The steel-vs-power tradeoff behind "how hard to push B" - for a fixed 757-lb-class magnet the answer comes off the real excitation curve, not theory; FEMM plays the role of the model magnet for first passes.
Cited in: Choosing Your Machine
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Compute free-molecular conductance of long ducts of ANY cross section from S = 400*A^2/(O*L) liters/sec with A in in.2, O (perimeter) in inches, L in inches (air, ~300 K; exact constant 403). Circular-duct equivalent: S = 6.3e4*sqrt(T/273M)*D^3/L cm3/s.
S = 400*A^2/(O*L) l/s (A in in.2, O in., L in.; air 300 K; exact 403); S = 6.3e4* sqrt(T/(273*M))*D^3/L cm3/s for circular ducts (Eq. 40-41)Source quote & editorial note
S = 400 A^2/OL liters/sec ... For convenience of calculation the value 400 is used rather than 403; the results are hardly affected since the formula is only an approximation.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 144-145
Editorial note, tabletop extrapolation: The workhorse formula for long, odd-shaped passages in a cyclotron - annular gaps around the dee, slots, duct runs - where circular-tube handbook formulas fail. Its own conditions ride along: LONG ducts in molecular flow, and 'only an approximation' by the source's own words; short apertures, bends and abrupt area changes take end corrections or the orifice forms (dg-839), and a complex dee cavity is a network of elements, not one duct.
Cited in: The Vacuum Budget of a Cyclotron
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For molecular-flow orifices use S = 75*A liters/sec (A in in.2) when the orifice is small relative to its surroundings, and S = 75*A*Abar/(Abar - A) when it is large (Abar = total duct area containing the orifice); combine elements as an electrical network, 1/S_tot = sum(1/S_i) in series, S_tot = sum(S_i) in parallel.
S_orifice = 75*A l/s (A in in.2, ~11.6 l/s/cm2 air); large orifice S = 75*A*Abar/(Abar-A) (Eq. 43-44); series 1/S = sum 1/S_i, parallel S = sum S_i (Eq. 45-46)Source quote & editorial note
For an orifice small relative to the area surrounding it, S = 75A. For an orifice large relative to the area surrounding it, S = 75A Abar/(Abar - A).
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 145
Editorial note, tabletop extrapolation: With the duct rule this covers most of a chamber conductance budget: baffle holes, dee mouths and constrictions become orifice or short-duct elements in a network. Finite-thickness holes transmit less than the zero-thickness 75A form - they are short ducts; interpolate or use transmission-probability tables - and series elements combine only approximately, so the budget is an estimate the pumpdown curve then checks.
Cited in: The Vacuum Budget of a Cyclotron
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Model the whole vacuum system as an electrical equivalent circuit - every duct, orifice and perforation a conductance (resistance = 1/S), combined in series/parallel down to a single effective speed AT THE LOCATION THAT MATTERS (inside the dee, where the beam and source live), not at the pump flange.
Source quote & editorial note
the term "resistance" is used there to indicate the reciprocal of the conductance. The use of resistance presents perhaps a clearer picture through the use of an electrical analog.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 132
Editorial note, tabletop extrapolation: The report's method in one sentence - their 32-in pumps' 13,700 l/s collapsed to 8,300 l/s effective inside the dee (air; the report's own worked numbers). The size of that collapse is the reason to budget from the source outward, not the pump inward - compute the conductance chain for the actual geometry rather than assuming any fixed fraction survives.
Cited in: The Vacuum Budget of a Cyclotron
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Size high-vacuum pumps by THROUGHPUT at the operating chamber pressure, not by rated speed: tabulate Q = P_B * S_PB for each candidate against the system's effective conductance, and require margin over the known gas load for outgassing (virtual leaks) plus some real inleakage. Their comparison: 32-in pumps swallow ~2x the gas of 20-in at the same 1.15e-5 mm Hg chamber pressure.
Q = P_B*2S_PB = S_EL*(P - P_B) = S_net*P (Eq. 24); compare pumps by Q at equal chamber PSource quote & editorial note
Thus the 32-in. pumps will handle almost twice as much gas as the 20-in. pumps, and the decision to use 32-in. pumps is an obvious one.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 135-137
Editorial note, tabletop extrapolation: The right way to evaluate a diff-pump upgrade for a next machine - work in throughput (torr-l/s) at the pressure the source needs, with the MFC's known gas feed as the load, instead of comparing nameplate l/s.
Cited in: The Vacuum Budget of a Cyclotron
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Anchor the vacuum design to the ion-source gas load: their 200 ml/hr (NTP) maximum injection = 0.042 liter-mm/sec (~0.04 torr-l/s), which against the effective pumping speed set the achievable operating pressure of ~4e-6 mm Hg.
200 ml/hr NTP = 0.042 liter-mm/sec; P_operating = Q_source/S_effective + P_pumpSource quote & editorial note
If 200 ml/hr is considered as a maximum rate of gas injection, this results in ... 0.042 liter-mm/sec.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 136
Editorial note, tabletop extrapolation: The same arithmetic the builder runs with the MFC: a 0.1-1 sccm hydrogen feed is 1.3e-3 to 1.3e-2 torr-l/s; divide by the honest effective speed FOR HYDROGEN at the chamber, then add the pump ultimate and the outgassing floor, to predict running pressure before touching hardware. The formula assumes the source feed dominates the incremental load - the flow-on/off test verifies that (dg-370).
Cited in: The Vacuum Budget of a Cyclotron
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Build and run a scale model of the RF system before committing to the full assembly: the report's 3/4-scale oscillator program delivered the dee-voltage-vs-frequency curve, the tuning-capacity range and drive-power data, and the quoted 27% efficiency measurement that changed the final design to six type-880 tubes while power-supply capacity allowed it.
model resonant frequencies ~ 1/scale (their 3/4-scale limits were 5% high for the scale factor used)Source quote & editorial note
Fig. 6.3-Typical characteristics of three-fourths scale model ... 150-kw input, 27.5-kw plate dissipation per tube ... The fairly low efficiency, 27 per cent, indicates that it would be desirable to go to six type-880 tubes in the final model
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. PDF p.162 (unnumbered chapter opener, Technical Report No. 6) for the quoted text; the figure is on PDF p.167 = printed p.167
Editorial note, tabletop extrapolation: The transferable method rule - prototype the next machine's dee/stem/liner as a cheap scale model (or full-scale mockup, given the small size) and measure resonance, Q and parasitics before final fabrication; NYO-780 p.29ff records the same practice. Cite both.
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Treat construction-material choice as a radiological design decision made at the drawing board, not a retrofit; where activation channels are open, prefer aluminum for in-beam and near-beam structures and minimize stainless steel.
Source quote & editorial note
a careful choice of materials of construction, for example, using as much aluminum as possible and very little stainless steel, should reduce the radiation problem significantly.
Boom, Toth & Zucker, Residual Radiation of the LRL 184-inch Cyclotron — ORNL-3158 (1961) — p. 18
Editorial note, tabletop extrapolation: ENERGY SCOPE: a 730-MeV machine's recommendation. At the reference machine's sub-MeV proton operation the spallation and (p,xn) channels behind it are closed, so bulk structural activation does not drive material choice at that scale - with the standing exceptions: thresholdless capture on some nuclides, light-element targets, and any deuteron operation. The drawing-board principle bites the moment a machine crosses into open-channel territory.
Cited in: Shielding a Small Cyclotron
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Expect the internal, in-vacuum components that the beam actually strikes to be the hottest objects in the report's accounting - a probe target may emit more than 10,000 r/hr, against the report's ~500 r/hr for the deflector and 100-500 r/hr for external targets at 5 minutes - and design their removal paths and storage shielding first.
internal probe target and exit strip: ~10,000 r/hr; deflector: ~500 r/hr; external targets 100-500 r/hr at 5 minSource quote & editorial note
Targets and their assemblies normally emit about 100 to 500 r/hr 5 minutes after bombardment ... The intensity of radiation by the exit strip averages about 10,000 r/hr, and the deflector about 500 r/hr.
McWalters et al., Radiation Exposures of Personnel at the 60-inch Cyclotron — UCRL-8276 (1958) — p. internal-target and external-target figures on PDF p. 10 as cited; deflector/exit-strip figures on PDF p. 15 (section 'Maintenance')
Editorial note, tabletop extrapolation: ENERGY SCOPE: these are 10-24 MeV activation levels. The design ordering survives: whatever intercepts full beam (probe tip, Faraday cup, target holder) concentrates the consequences. On a sub-MeV machine that is heat and sputtering today - and activation joins the list via thresholdless capture on some materials, light-element targets, or any deuteron operation, growing first at these same components if energy climbs.
Cited in: Shielding a Small Cyclotron
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State the hard requirements first (for a magnet: isochronous average field, adequate focusing, achievable power), then weigh remaining configurations against soft criteria like cost, ease of extraction, and maintenance.
Source quote & editorial note
Beyond these requirements the advantages and disadvantages of various magnet configurations that might be used become more subtle and must be weighed against such factors as the cost, ease of beam extraction, and maintenance requirements.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 162
Editorial note, tabletop extrapolation: Scale-free requirements-hierarchy discipline - with the hard-requirements LIST being machine-specific: for a classical weak-focusing machine it is the field law (falling field, n inside its stable band), focusing, and achievable power; isochronism is the AVF machine's version, and a synchrocyclotron's differs again. State yours first, then trade the soft criteria as the source does.
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A risk-retiring model's charter, in the source's words: examine practicability, reveal any unexpected phenomena, and demonstrate the feasibility of the riskiest subsystem - the purposes their electron analogue was conceived for.
Source quote & editorial note
conceived as an experimental device to examine the practicability of isochronous acceleration ... to reveal any unexpected phenomena ... and finally, to demonstrate the feasibility of a high efficiency beam extraction system.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 263
Editorial note, tabletop extrapolation: The three-purpose charter is scale-free for any model or prototype a program chooses to build; whether to build one at all is a cost-versus-risk call - FEMM plus the tracker is the tabletop program's cheap analogue. The keV-electron stand-in trick itself needs more than matched T/mc^2 to be faithful (rigidity and geometry must scale together).
Cited in: Choosing Your Machine
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When rejecting alternatives in a trade study, name each one's defects - the source's own practice in the quoted line: 'all suffer from one or more of the following defects', followed by the list.
Source quote & editorial note
All suffer from one or more of the following defects: excessive space requirements, lack of terminal space, lack of terminal auxiliary power, and lack of flexibility for future uses.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 149
Editorial note, tabletop extrapolation: Their injector shoot-out (tandem vs open-terminal vs pressurized vs Van de Graaff) models the documentation style for any subsystem selection in mark2_design_notes open decisions.
Cited in: Choosing Your Machine
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Choose sector number from the essential-resonance structure of the tune range you must traverse, then break ties with RF symmetry (how many accelerating gaps the geometry naturally supports).
systematic (structure) resonances: a*vr + b*vz = p*N for integer p (p = 1 is the fundamental sector harmonic), subject to order and symmetry selection rulesSource quote & editorial note
Six- and eight-sector machines are free from strong essential resonances ... also, the symmetry easily permits four accelerating gaps per revolution, a situation well suited to rf cavities.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 266-267
Editorial note, tabletop extrapolation: 810-MeV specifics (vr climbing to 2, spiral sectors) do not scale down; the method — list resonances crossed by your vr/vz trajectory before fixing N, then let RF layout break ties — applies to any AVF design.
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Consult fabricators about producible sizes and processes before finalizing magnet geometry, and let fabricability (available forging/plate sizes, machining method) drive the construction concept.
Source quote & editorial note
Representatives of the steel industry were consulted to determine the size of forging of the required shapes that could be practicably produced.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 136
Editorial note, tabletop extrapolation: Scale-free: for a next machine this reads 'call the waterjet/plate supplier before freezing the pole drawing' — same move as TID-454's cost-driven magnet design.
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Put the field-critical dimensions on iron geometry rather than on coil placement - the quoted design principle - and plan from the outset to shim the finished magnet: post-construction shimming is 'reasonable to expect'.
Source quote & editorial note
A magnet of this design places all the critical dimensions on the iron geometry and minimizes the sensitivity to errors in coil placement. It is reasonable to expect that the final magnet would have to be shimmed after construction
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 172
Editorial note, tabletop extrapolation: Directly scale-free: machined iron holds its dimensions in a way wound copper cannot, and 'shim after construction' is a scheduled step rather than a failure mode. Trim coils, where fitted, are a separate adjustability decision with their own warm-magnet limits (dg-160).
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Stage the model-magnet program: carry competing configurations through deliberately crude models to settle gross characteristics, then build one accurate model whose field maps are good enough for orbit computation.
Source quote & editorial note
The model tests to date have been directed at determining the gross characteristics of various configurations ... Future models will include one very accurate version on which measurements suitable for orbit calculation can be made.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 172
Editorial note, tabletop extrapolation: Maps onto the FEMM-first pipeline: cheap comparative FEMM runs play the role of crude models; only the chosen geometry earns a high-fidelity field map for the Python tracker.
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Match power-supply regulation to each coil's fractional contribution to the field: the source used transistor-regulated supplies of 1-part-in-1e4 stability for every coil contributing more than 1% of the field.
regulation stability ~ (field tolerance)/(coil's fractional field contribution)Source quote & editorial note
Transistor-regulated power supplies with 1 part in 10^4 stability are used to energize coils which contribute more than 1% to the magnetic field.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 274
Editorial note, tabletop extrapolation: Scale-free budgeting instinct (from a 42-gauss analogue machine): spend regulation money in proportion to field contribution. The 1% line and any source-sharing arrangements are that design's choices; the general form is regulation ~ field tolerance / coil contribution, applied against your own stability budget (dg-027).
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Choose the accelerating-structure topology by total-machine cost: if a dee-sized magnet gap prices the magnet unreasonably, move the resonator out of the gap (cavities between sectors) rather than paying for gap in iron and amp-turns.
Source quote & editorial note
The cost of the magnet would be increased unreasonably if a gap suitably large for conventional dees were provided. For this reason, a system for acceleration with vertically oriented resonant cavities was adopted.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 145
Editorial note, tabletop extrapolation: The specific topology (vertical TEM cavities) is 810-MeV-only; the transfer is the coupling: every inch of dee clearance is bought with magnet cost, so dee-gap and magnet-gap must be traded as one system, as in a next machine's gap decision.
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Prefer the RF configuration you can analyze - the source chose the ordinary coaxial cavity as 'more amenable to design' - and set its free dimensions as documented compromises, theirs being voltage-holding ability against transit-time effects.
Source quote & editorial note
chosen for the final design since this is the ordinary coaxial cavity and is more amenable to design ... was chosen as a compromise between voltage-holding ability and transit-time effects.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 174-176
Editorial note, tabletop extrapolation: Scale-free method: a dee-stem system is likewise a transmission line with machine-fixed dimensions and a few free ones - when sizing the planned higher-voltage dee (the 5-13 kV upgrade), name each free spacing's compromise pair in the design notes the way the source names theirs.
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Build a scale model of the resonator to validate the design method: theirs certified the calculation - 151.3 Mc/s predicted, within 4% of measurement - and caught a several-percent construction error in the spacing near the median plane; both are the quoted outcomes.
Source quote & editorial note
Checking of the model dimensions revealed a construction error of several percent in the spacing near the median plane ... a resonant frequency of 151.3 Mc/s was calculated for the model; this is within 4% of the measured value.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 177
Editorial note, tabletop extrapolation: Scale-free double duty: a bench mock-up of a next machine's dee/stem before the LDMOS amplifier arrives certifies the calculation and catches build errors - and while it sits on the bench, sweeping for higher-order modes and measuring Q are nearly free additions (dg-664).
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Budget RF power in explicit named lines - the source's budget: computed cavity loss 500 kW + beam power 160 kW + contingency 200 kW (about 30% on top of the computed lines) = 860 kW total.
P_total = P_cavity + P_beam + P_contingency (source: 500 + 160 + 200 kW; contingency ~30% of the computed lines)Source quote & editorial note
Computed power loss in cavity 500 kW; Beam power 160 kW; Contingency 200 kW; total 860 kW
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 180
Editorial note, tabletop extrapolation: The kilowatts are 810-MeV numbers; the structure sizes the planned 100-500 W LDMOS chain honestly - compute the resonator loss (dg-313), add beam and coupling loads, then carry contingency as a NAMED line of the source's ~30% class instead of hiding margin inside each estimate.
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Select the amplifier-to-resonator coupling by its behavior during a spark: the source's scheme reflected a large resistive load to the amplifier plates when the cavity sparked, DECREASING tube plate current - prefer arrangements with that property.
Source quote & editorial note
Thus, when a spark occurs in the cavity a large resistive load is reflected to the plates of the power amplifier and the tube plate current would decrease.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 182-183
Editorial note, tabletop extrapolation: Scale-free fault-mode-first design: dees spark at every scale, so choose a next machine's amplifier coupling for arc behavior, not just matched-condition efficiency - establish what YOUR coupling does to the device when the load arcs (some couplings raise device stress instead), then layer the protection accordingly (dg-338, dg-679). Directly relevant to protecting an LDMOS pallet.
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Size the pumping system from the outgassing load rather than the volume: the source ASSUMED net pump speed at 25% of mouth speed for its baffles and valves, and found published outgassing data high against measurement by ~20x at 1 hour and ~2x at 20 hours.
S_net ~ 0.25 * S_mouth; Blears data vs measured: ~20x high at 1 hr, ~2x at 20 hrSource quote & editorial note
The net speed of these pumps was assumed to be 25% of the speed at the mouth of the pump, because of the usual losses in baffles and valves.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 158
Editorial note, tabletop extrapolation: Scale-free in structure, not numbers: size from the outgassing load, compute the actual duct and baffle conductances (1/S_eff = 1/S_mouth + 1/C - the vacuum deep dive's budget method), and treat handbook outgassing rates as early-time bounds. The 25% is what THEIR plumbing cost them; the reference machine's SI100 stack has its own conductance chain to compute.
Cited in: The Vacuum Budget of a Cyclotron
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Check whether electrostatic or magnetic deflection wins at your particle velocity before designing an extractor: the equivalent magnetic field for a given force shrinks as B = E/v, so E-fields lose effectiveness as velocity rises.
B_equiv = E/v; their case: 4.4 kV/cm on the Analogue scales to 700 kV/cm at 810 MeV vs only 2,800 gauss magneticSource quote & editorial note
electric fields are relatively ineffective at high particle velocities, but the force on an ion due to a magnetic field is proportional to velocity.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 151
Editorial note, tabletop extrapolation: At 150 keV protons (v ~ 5.4e6 m/s) the comparison runs strongly toward electrostatic: modest septum fields equal coil fields that are awkward to engineer at that scale, which is why documented small machines extract electrostatically. Run the B = E/v arithmetic before copying any big-machine magnetic-channel scheme - the crossover is a computation, not a law.
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Assume the shielding estimate will prove low and the experiment space too small - the quoted history: shielding initially provided 'has later proved to be inadequate' and experiment areas are 'now too small in almost every installation'. Design margin and expansion room in from the start.
Source quote & editorial note
Historically, the shielding initially provided for high-energy accelerators has later proved to be inadequate ... The experiment areas are now too small in almost every installation.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 184
Editorial note, tabletop extrapolation: Scale-free planning doctrine, and this collection's first design-stage statement of it: leave physical room (and structural capacity) to add shielding around a next machine before the first neutron is made.
Cited in: Shielding a Small Cyclotron
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Design shielding so the stricter general-population dose limit is met in all regularly occupied adjacent areas, even where regulations would allow worker limits - the source's practice, under their era's limits (5 rem/yr occupational, 0.5 rem/yr public).
design limit = public limit in inhabited adjoining areas (their era: 5 / 0.5 rem/yr; current US: 5 rem/yr occupational vs 0.1 rem/yr public - a factor of 50)Source quote & editorial note
we have designed the shielding so that the limits for general population are observed in the regularly inhabited work areas adjoining the accelerator and experiment rooms.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 186
Editorial note, tabletop extrapolation: Directly transferable posture for a residential-basement machine: the family upstairs is 'general population', so design to the CURRENT public limit at occupied locations - in the US today 1 mSv (0.1 rem) per year, fifty times below occupational and five times stricter than the source's era ratio - and take the numbers from the jurisdiction's own regulations (/legal/), not from a 1965 report.
Cited in: Shielding a Small Cyclotron
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Build the shield estimate as an explicit chain - dose limit, source term, attenuation, secondary buildup - recording at each approximation which direction the error runs; the source's own example neglected secondary production and target attenuation together because the net stayed conservative, and only to within the precision of the other data.
Source quote & editorial note
we have neglected both the secondary production and target attenuation; this results in a conservative estimate still within the precision of other data.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 189
Editorial note, tabletop extrapolation: Scale-free methodology (their 810-MeV cascade physics is not): carry the same per-step bookkeeping on a next machine's estimate. The quote's specific lesson: omissions can run in opposite directions and partially cancel, so direction is tracked per step, never assumed - and the net conservatism is only as good as the input data's precision.
Cited in: Shielding a Small Cyclotron
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Separate the radiation components by the question each answers: the penetrating high-energy component sets shield thickness, while the soft/evaporation component sets activation and the dose at surfaces — do not size one problem with the other's source term.
Source quote & editorial note
The thickness of shielding required for a high energy accelerator is established chiefly by the cascade nucleons ... The evaporation particles must be taken into account, however, in determining the activation of materials
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 186-188
Editorial note, tabletop extrapolation: The sort-by-question habit is the transferable part: identify which radiation component sets shield thickness and which sets activation and surface dose for YOUR source term. For a D-D-capable machine that is fast-neutron moderation for thickness, with capture gammas and nuclide-specific activation as separate questions carrying their own data - not a clean analogue of the source's cascade/evaporation split, which is high-energy physics.
Cited in: Shielding a Small Cyclotron
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Sanity-check derived unit prices against what was actually paid for the nearest precedent - the quoted practice: their $0.35/lb finished-magnet estimate judged reasonable against $0.26/lb actually paid for another large magnet; the report's appendix ties its cost lines to suppliers (scan re-read queued).
Source quote & editorial note
The estimate of $0.35 per pound for the finished magnet appears reasonable when compared with the unit price of $0.26 per pound paid for another large magnet at the Laboratory.
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 245
Editorial note, tabletop extrapolation: Scale-free estimating hygiene: their App. F traces $11.5M to named suppliers; a next machine's BOM should likewise tie each line to a quote, a catalog page, or a reference machine receipt — and explain deltas ('more complex machining, more waste metal').
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Provision probable future additions now and keep their cost out of the baseline - the quoted split: 'provisions have been made in all plans to make the addition of the medical facility as simple and as economical as possible' while 'the cost of the medical facility is not included in the initial cost of the project'.
Source quote & editorial note
Provisions have been made in all plans to make the addition of the medical facility as simple and as economical as possible ... The cost of the medical facility is not included in the initial cost of the project
Oak Ridge National Laboratory, A Proposal for the Mc² Isochronous Cyclotron — ORNL-3540 (1963) — p. 22
Editorial note, tabletop extrapolation: Scale-free scoping discipline for the business plan: design the educational-machine baseline with hooks for upgrades (extraction port, shielding growth, second station) without loading their cost onto gate-one.
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Make the deflector adjustable and expect a minority fraction: the 22-inch development deflector, with full adjustability, extracted 38% of a 1000-uA internal beam under the BEST conditions — treat tens of percent as a good small-machine electrostatic extraction efficiency, reached by tuning, not by drawing.
extraction efficiency ~38% at best on a 22-in-orbit machineSource quote & editorial note
A very effective adjustable beam deflector has been developed; under the best conditions, 38% of a 1000 ua internal beam has been deflected.
Editorial note, tabletop extrapolation: Sets expectations for any future extraction gate: design the septum/deflector with in-vacuum adjustability - the quoted 'very effective' unit was fully adjustable and even so extracted 38% at BEST. Tens of percent is the documented ballpark for classical deflectors (dg-496, dg-595); define success for your machine before the attempt, and account for where the undeflected majority goes (dg-260).
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On the experimental unit, with dees limited to 10 kV, injection potentials over 10 kV decelerated ions in the gap between the accelerating electrode and the dee; their fix was raising the dee-side capability - a redesign for at least 20 kV dee-to-ground.
first gap accelerates only while the signed electrode-to-dee potential difference is favorable (their case: V_inject > V_dee ran it backward)Source quote & editorial note
Since the dee voltage in the experimental unit was limited to 10 kv, application of injection potentials of over 10 kv resulted in deceleration of ions between the accelerating electrode and the dee.
Editorial note, tabletop extrapolation: Any source-bias or puller experiment must check the same ordering in ITS geometry: a dc extraction potential that overtops what the RF gap can supply runs the first gap backward. The check is signed potentials and timing at the actual gap - the source's inequality is that machine's instance of it, not a universal bound.
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The pole iron is the durable identity: ORNL's 1949 test cyclotron was the '22-inch' by maximum orbit, and after the rework it was 'more appropriately identified as the 44-in. cyclotron' - renamed for its equivalent pole diameter, the report's own naming logic.
Source quote & editorial note
Inasmuch as the equivalent diameter of the pole pieces is 44 in., the machine is more appropriately identified as the 44-in. cyclotron.
Editorial note, tabletop extrapolation: The reference machine's H-frame is the analogous asset: energy upgrades - gap, shims, dees, RF power - can stage around the same 757-lb iron for years. The platform reading is the editorial lesson drawn from ORNL's staged reuse of one magnet line (1.5 MeV, then 5 MeV, then proposed heavy ions); the quote itself carries the renaming.
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Material choice for beam-intercepting hardware must include activation: a thin-wall stainless septum mockup handled 190 W per inch of water-cooled tube, but type 304's extreme induced radioactivity disqualified it and drove a switch to aluminum alloy — thermal adequacy is not the whole selection (86-inch deflector development).
bench test - 0.025-in.-OD, 0.003-in.-wall SS tube, 7.7 in.3/min water, ~190 W/in.Source quote & editorial note
The extreme radioactivity induced in type 304 stainless steel makes its use undesirable, the use of an aluminum alloy is now being investigated.
Editorial note, tabletop extrapolation: At sub-MeV energies on ordinary structural metals activation is small where it occurs at all - thresholdless capture and deuteron operation are the exceptions - and the selection logic transfers whole: thermal adequacy is not the whole selection. Prefer aluminum or graphite for probes, septa and slits anywhere protons above a few MeV are contemplated, and let the licensing story inherit the same reasoning.
Cited in: Shielding a Small Cyclotron
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A variable-energy cyclotron is a credible Van de Graaff alternative in the 5-10 MeV band: ORNL's study concluded feasibility, with energy definition better than +/-10 keV achieved by collimation plus magnetic analysis of the deflected beam - selection, not correction: the analyzer transmits a narrow band and discards the rest, trading current for resolution - and 1-10 uA deflected.
energy definition < +/-10 keV via deflected-beam collimation + magnetic analysisSource quote & editorial note
such a cyclotron is feasible, that an energy definition of less than +/-10 kev could be achieved, and that deflected beams would be in the range of 1 to 10 ua
Editorial note, tabletop extrapolation: Direct prior art for the plan's educational variable-energy concept: vary energy with field/frequency plus a movable target (cf. the 44-inch spacer), and buy energy DEFINITION with a simple analyzed beamline - accepting the current it costs - rather than machine perfection.
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Sequence rf design around measurement: ORNL designed every component of the 44-inch rf system EXCEPT the filament-coupling circuit, deliberately, because that circuit depends on the resonant dee system's electrical characteristics and "cannot be designed until these characteristics are determined" — leave the coupling stage undesigned until the tank/dee resonator is built and measured.
Source quote & editorial note
Since this circuit depends upon the electrical characteristics of the resonant dee system, it cannot be designed until these characteristics are determined.
Editorial note, tabletop extrapolation: The template for the reference machine's LDMOS upgrade - freeze the amplifier and dee-resonator designs, but specify the matching/coupling network only after measuring the real dee system's f0, Q, and shunt impedance on the bench. Ordering the coupling parts first is the classic mistake this rule prevents.
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Insulate the entire dee system from ground so a dc bias can be applied to control ion loading — designed into the rebuilt 44-inch from the start (and already proven on the 22-inch: ornl-1339 measured accelerated-beam gains from dee bias; ornl-1269's Fig. 12 ran 600 V bias).
Source quote & editorial note
The whole dee system is insulated from ground so that a bias potential may be applied to control ion loading.
Editorial note, tabletop extrapolation: The reference machine already uses dee bias; the design rule for a next machine is to make bias a first-class requirement - insulate the dee-stem support (see the ornl-1884 cantilever-on-insulators execution) rather than retrofitting isolation later.
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High dee voltage buys its clearance out of the magnet gap: to run 100 kV, ORNL removed the flat shims from the tank, accepting a wider 13.5-in. gap (and the field cost that implies) — dee-voltage ambition, aperture, and gap trade against each other and must be budgeted together (44-inch cyclotron).
Source quote & editorial note
The removal of the flat shims from the tank increased the magnet gap to 13 1/2 in. and provides sufficient clearance to permit operation of the dees at a potential of 100 kv.
Editorial note, tabletop extrapolation: For a next machine the same ledger applies at 5-13 kV: dee-to-liner spark distance plus dee aperture plus liner clearances must fit inside the gap, and gap given to voltage clearance is field taken from energy - in the gap-dominated, fixed-ampere-turn regime (dg-021's measured caveat on the ideal scaling). Decide voltage and gap together (dg-181).
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Develop cyclotron RF on an electrical model: the variable-energy oscillator test used an 8-ft section of the 63-inch dee-stem electrical model as its resonant system - the quoted practice; the dee-simulating capacitors and circuit-selection details are the report's own (scan re-read queued).
Source quote & editorial note
Dees were simulated by a capacitor connected from the end of each dee stem to ground... Other circuit components were selected to have approximately the same values as those in a full-scale operation.
Howard (ed.), Electronuclear Research Division Semiannual, period ending 20 September 1953 — ORNL-1663 (1954) — p. PDF p. 19 as cited (printed p. 10, section 'VARIABLE-ENERGY HEAVY-PARTICLE CYCLOTRON')
Editorial note, tabletop extrapolation: A bench-scale dee-stem mockup (pipe sections plus padding capacitors) lets the next machine's oscillator/coupling scheme be raced against alternatives for pocket change - the same measure-on-model philosophy as the deferred filament-coupling rule, one report earlier in hardware form.
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Divide fabrication deliberately: ORNL contracted the liner, dees and dee-stem housing to an outside shop while making faceplates, dee stems, ion source, target probe and vacuum system locally - the quoted split; the contractor difficulties that followed are the succeeding reports' account (the 1670 -> 1795 -> 1884 arc).
Source quote & editorial note
The liner, dees, and dee-stem housing are being fabricated by an outside contractor. The faceplates, dee stems, ion source, target probe, and vacuum system were fabricated locally
Editorial note, tabletop extrapolation: The three-report arc remains this collection's cleanest outsourcing story: the contracted brazed, water-cooled vacuum parts were where the delays landed - one program's experience, and a fair prior. For a next machine: buy simple machining, keep leak-integrity parts in-house or design them repairable.
Cited in: The Vacuum Budget of a Cyclotron
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Design subsystems as a reusable kit: the proposed 44-to-48-inch conversion needed only a new magnet and vacuum tank because the oscillator, dee system, vacuum system, ion source, target probe, and power supplies were all judged reusable — subsystem modularity is what makes a machine upgradable into a different machine (44-inch cyclotron).
Source quote & editorial note
All other components of the present 44-in. cyclotron, oscillator, dee system, vacuum system, ion source, target-probe, and power supplies, would be utilized.
Editorial note, tabletop extrapolation: A strong argument for clean interfaces between a next machine's subsystems: ORNL could contemplate a new machine class for the price of iron and a tank because everything else was JUDGED reusable - the judgment is the quote's; the adaptation cost of the reuse is not on this card. Design interfaces so the same judgment could be true of your machine.
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The 48-inch conversion spec set design dee-to-dee voltage at 200 kV against a 110-kV threshold for N5+ - a factor of about 1.8 over threshold.
V_design / V_threshold ~ 200/110 ~ 1.8Source quote & editorial note
Dee-to-dee r-f voltage (design), kv 200; Threshold voltage for N5+, kv 110 (Table 3, condensed)
Editorial note, tabletop extrapolation: Margin philosophy consistent with the 63-inch's 75-vs-60 kV acceptance hold (ornl-1339): documented machines bought well over threshold. For the LDMOS upgrade, compute the threshold dee voltage for the intended turn count and buy real headroom - documented precedents cluster around 1.3-2x. What the margin purchases (orbit count, loading headroom, species reach) is the editorial reading, not the table's statement.
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Site an accelerator below grade and the earth is your shield: the 48-inch room was planned "mostly below ground level" explicitly because it "will be easy to shield", at basement floor level for heavy-equipment transfer, adjacent to the existing building so utilities barely extend and the existing control station works without moving.
Source quote & editorial note
Being mostly below ground level, the room will be easy to shield. Placing the room at the basement floor level will make it convenient to transfer heavy equipment.
Editorial note, tabletop extrapolation: Directly relevant to the facility question for any MeV-class educational machine: below-grade siting was the study's shielding strategy, and siting beside existing utilities and controls was a cost line they weighed as seriously as the magnet. Earth shields in the directions it actually covers, by its actual thickness, density and moisture - it does not blanket-replace engineered shielding, and the uncovered directions, the roof, and every penetration still get the full design treatment (see the shielding deep dive).
Cited in: Choosing Your Machine · Shielding a Small Cyclotron
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Retire beam-dynamics risk deliberately: ORNL PLANNED an electron-model accelerator 'to be used in assessing the importance of imperfection resonances and the feasibility of their penetration' before committing to the 1-BeV proton machine - the plan is what the quote records.
Source quote & editorial note
Plans are being made for an electron-model accelerator to be used in assessing the importance of imperfection resonances and the feasibility of their penetration.
Editorial note, tabletop extrapolation: A historical instance of risk-ordered development: when the open question is orbit dynamics, a cheap electron model is one way to attack it before proton iron is bought - scaled properly (dg-892's rigidity caveat). The tabletop program's equivalent instruments are the tracker and measured field maps.
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A major rebuild of even a small, staffed machine runs about two years decision-to-tested-assembly: 44-inch revision design underway Mar 1953 (ORNL-1531), design essentially complete Mar 1954 (ORNL-1670), assembly approaching completion Sep 1954 with contractor rework (ORNL-1795), assembled and vacuum-tested but NOT yet on beam Mar 1955 — with ion source, oscillator auxiliaries, and shimming still open.
timeline: design start +12 mo = design done; +6 mo = assembly (blocked on contractor); +6 mo = assembled/vacuum-tested, beam still pendingSource quote & editorial note
The major components have been assembled and vacuum-tested (see Fig. 5).
Editorial note, tabletop extrapolation: Schedule realism, one datapoint thick: a professional division with machine shops took about two years from revision concept to vacuum-tested assembly, with outsourced fabrication the long pole (dg-951). A home program's periods stretch and compress differently; the census's one-to-six-year first-beam spread is the wider base rate.
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Architect an external beamline as condenser -> shielded slit -> analyzer: the cyclotron's apparent source is too fuzzy to analyze directly, so first focus as much beam as possible onto a precision slit, then use that slit as the sharply defined object for the analyzing magnet.
Source quote & editorial note
in order to produce a suitable object for the analyzing magnet, we introduce a second magnet whose sole function is to focus as much of the beam as possible on a precision slit.
Editorial note, tabletop extrapolation: DIRECT for any ANALYZED external line on a next machine - the canonical two-stage architecture: a condenser focuses as much beam as possible onto a precision slit, and that illuminated slit becomes the analyzer's cleanly defined object. Lines that only transport or irradiate skip the apparatus; the slit's shielding is the companion rule (dg-966).
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Put the beam-defining slit inside the shield wall, because the fraction of beam intercepted by the slit system is itself a strong radiation source; put the condenser as close to the beam exit port as fringe fields allow (minimizes horizontal spread), and give the analyzer a long image distance to reduce angular spread at the image.
Source quote & editorial note
A considerable amount of undesirable radiation will be produced by that part of the beam intercepted by the slit system. ... it is also desirable that the analyzer image distance be large, in order to reduce the angular spread of the beam at the image point. ... [placing the condenser farther from] the cyclotron port ... required larger condenser pole pieces in order to accommodate the horizontally spreading beam.
Editorial note, tabletop extrapolation: DIRECT and cheap to honor at layout time, nearly impossible later: treat every defining aperture as a place where beam power - and therefore radiation - concentrates. At 150-170 keV the intercepted beam makes mostly heat plus thick-target bremsstrahlung whose X-ray yield climbs steeply with voltage, so the slit belongs with the shielded, surveyed components, wherever the survey ranks it that day.
Cited in: Shielding a Small Cyclotron
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Prefer a strong-focusing quadrupole pair over a sector magnet for the condenser role: the study's comparison gave at least tenfold less weight and power (the quoted factor), a straight-pipe vacuum, and - because the beam is undeflected - field and lens tunability without geometry changes; the as-built pairing was 355 lb of doublet against an estimated 3 tons of sector magnet (p.32).
Source quote & editorial note
the weight and power requirements would each be less than the corresponding sector-magnet requirements by at least a factor of ten.
Editorial note, tabletop extrapolation: DIRECT - the as-built comparison (p.32) was 355 lb for the doublet pair vs an estimated 3 tons for a sector condenser. At a next machine's rigidity (~7x lower than Rochester's 4e5 G-cm) a doublet becomes a benchtop object; the no-deflection tunability argument is the one to remember when laying out the line.
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Size quadrupole aperture from the measured extracted-beam envelope with explicit margins - the report's arithmetic: the measured beam box gave semi-axis a = 3 cm, they applied 'an extra factor of safety' and took c = 1.5, hence poles at xy = +/-2.25 cm^2.
hyperbolic poles xy = +/-c^2; an inscribed ellipse of semi-axes A, B is tangent when c^2 = A*B/2; the report: a = 3, c = 1.5 -> xy = +/-2.25 cm^2Source quote & editorial note
With this as a guide we apply an extra factor of safety and take a = 3, c = 1.5, hence the magnet poles are given by xy = +/- 2.25 cm^2
Editorial note, tabletop extrapolation: DIRECT method, not numbers: measure the real beam first, then stack explicit margins on the way to the pole constant. A next machine's envelope comes from its own extraction simulation or measurement; margin-then-round-up is what prevents discovering an undersized bore after the coils are wound.
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Use effective (not physical) magnetic length for quadrupole optics: measurements on these magnets showed effective length up to ~20% greater than physical - their design treated 18.1 cm physical as 20 cm effective, a 10% correction.
l_eff ~ up to 1.2 x l_phys for these small-bore quads; all lens equations use l_effSource quote & editorial note
Measurements have shown that the effective length of the magnets is as much as 20% greater than the physical length.
Editorial note, tabletop extrapolation: DIRECT: for short quads the fringe extension is a first-order effect, not a correction - and it scales with aperture, which is why short, fat quads see the largest effect. Get l_eff per magnet from the FEMM/tracker pipeline; ignoring it produces significant focal errors.
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Run beam-transport quads at deliberately low field (~1 kG): avoids iron saturation, keeps excitation power low enough to skip water cooling entirely, and leaves headroom; since lens strength parameter lambda scales as B^1/2 for a given particle and energy, excitation current is a smooth tuning knob.
B = (lambda/l)^2 * (a/2) * B_rho ~ 1 kilogauss at design point; lambda proportional to B^1/2Source quote & editorial note
This low field avoids saturation difficulties in the magnet iron and high excitation power requirements. Furthermore, it enables us to dispense with water cooling in the windings.
Editorial note, tabletop extrapolation: DIRECT: at a next machine's rigidity, transport-quad pole-tip fields of a few hundred gauss are plausible - compute the actual requirement from aperture, length and focal geometry (the formula) - and where field and current density land as low as the source's, unsaturated iron with air-cooled random-wound coils is exactly the regime they describe. Confirm with the dissipation arithmetic before skipping water (dg-708). OCR trap - the text layer renders the B^1/2 exponent as B^2; page image verified B^1/2.
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Connect all four coils of a quadrupole strictly in series on one supply: paralleling (or individual supplies) brings 'extreme difficulty in maintaining uniform gradients' - the quoted reason. The report's winding specification, page-image verified: #22 heavy Formex magnet wire, ~3000 turns per coil in the 2.67 cm2 window (12,000 per unit), convenient maximum 500 mA and safe 625 mA at their 1000-circular-mil-per-ampere allowance, 72.5 ohms per coil at 20 C; ampere-turns sized by a path integral over the magnetic circuit (sum of l_i/mu_i terms) with margin - 5000 A-turns needed for 1 kG, designed for 6000.
series connection forces equal current through all four poles. NI by path integral over l_i/mu_i [the formula is handwritten in the source; its exact typography is partly illegible even at 600 dpi, but the prose defines l_i and mu_i, so the path-integral character is certain]; 1 kG needs NI = 5000, designed 6000; 3000 turns/coil #22, 72.5 ohm, 500-625 mASource quote & editorial note
A field of 1 kilogauss requires NI = 5000 ampere turns. As a safety factor, we have designed for 6000 ampere turns. ... Each coil will have exactly 3000 turns and the coils in each unit are connected in series
Bromley & Bruner, The Design of a Focusing and Analyzing System for the 27-inch Cyclotron Beam — NYO-3823 (1954) — p. PDF p.31 (printed page 28)
Editorial note, tabletop extrapolation: DIRECT wiring doctrine for any home-built multipole: gradient symmetry comes from forced equal current, not matched resistances - which is also why surplus-wire coil construction works, since the series circuit forgives resistance mismatch between coils.
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Keep analyzing-magnet field below the onset of pole-edge saturation (here ~8 kG for a 4 cm gap C-magnet): above it the field grows less uniform near the pole boundaries, which is exactly where a wedge analyzer's focusing happens. This sets a minimum bend radius for the top energy (rho >= 47 cm for 7 MeV protons, B-rho = 3.8e5 G-cm).
rho_min = B_rho(E_max) / B_max(uniformity-limited); their case: ~3.83e5 G-cm at 7 MeV over 8 kG -> rho ~ 48 cmSource quote & editorial note
For fields above about 8 kilogauss, saturation effects begin to set in, and the field becomes less uniform near the pole boundaries.
Editorial note, tabletop extrapolation: DIRECT sizing rule with scale caveat: the 8 kG threshold is geometry- and steel-specific, but the logic (uniformity budget, not raw B_sat, sets the working field; bend radius follows) applies to any analyzer dipole on a next machine. At ~170 keV protons rho is a few cm even at modest fields - the analyzer becomes a bench magnet.
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Match model order to input-data quality: Rochester declined to base the magnet design on second-order calculations because the fringe-field corrections were 'not sufficiently precise to warrant' it - the quoted judgment; the wedge-design context and the clearance check they did run are the report's detail (scan re-read queued).
Source quote & editorial note
the methods for correcting for the fringe fields effects ... are not sufficiently precise to warrant basing the magnet design on the second-order calculations.
Editorial note, tabletop extrapolation: DIRECT design-philosophy rule for the whole next-machine campaign - match model order to input-data quality. Also note the companion check they DID run (pp.49-50), that the bent beam clears the back of the magnet with ~5 cm margin for the full 6 cm beam - a 30-second calculation that catches a catastrophic layout error.
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Relax instrument specs to the actual measurement: relaxing the original requirement for 'extremely high field uniformity' collapsed the Browne-Buechner-derived design to a simple C-shaped yoke - the quote; the specific relaxations (the uniformity figure, deferred pole-tip spacers, the rationale) are the report's detail (scan re-read queued).
Source quote & editorial note
By relaxing the original requirements for extremely high field uniformity, a considerable simplification of the Browne-Buechner design was achieved in reducing the magnet yoke structure to a simple C-shape.
Editorial note, tabletop extrapolation: DIRECT and very relevant to a next machine - the whole report is a case study in not copying the flagship instrument (Browne-Buechner at MIT) but re-deriving requirements from the local physics program. Compact C-yokes, deferred correction hardware ("add spacers only if needed" - they never were), and unconventional yoke placement are all fair game once the real spec is known.
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A conventional cyclotron usually needs no beam sweeper for pulsed work - the source's point: the beam is already naturally bunched into RF-phase packets, so timing structure comes built in, unlike a Van de Graaff's DC beam, which must be swept or bunched.
Source quote & editorial note
the problem of obtaining a pulsed beam usually does not arise, because the beam of a conventional cyclotron is already naturally bunched.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 6
Editorial note, tabletop extrapolation: DIRECT and foundational for the experiment catalog: the reference machine at 9 MHz delivers phase-bunched beam at the RF period - a measurable, teachable property and the enabling fact for gated counting. 'Usually' is operative: time-of-flight at fine resolution, or experiments needing low repetition rate, can still require pulse selection or extra bunching - check bunch width and period against the experiment's timing demands.
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Derive the timing reference from the cyclotron oscillator itself, not from a beam-intercepting pickup: RF-derived reference pulses are insensitive to beam-current changes and are all smooth and identical in shape; the residual phase shift between beam bunches and oscillator when the magnet tuning changes is small enough in practice to ignore.
Source quote & editorial note
the pulses are obtained in a way which makes them insensitive to beam current changes, and b) all reference pulses are smooth and identical in shape.
Fulbright et al., A Fast Neutron Time of Flight System for Use with Cyclotrons — NYO-9360 (1962) — p. 6
Editorial note, tabletop extrapolation: The most directly transferable finding here: the machine's RF is a free, stable timing fiducial at any scale - clock gated counting and TOF off a capacitive sniff of the dee. A fiducial is not a beam-arrival timestamp: beam phase relative to the RF moves with field tuning, loading and cable delays, so calibrate the offset against a real beam signal - and re-calibrate after retuning - before treating RF zero-crossings as beam time.
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Retire RF-system risk with a scaled electrical model before cutting full-size metal: build the complete RF circuit at reduced scale (frequency scales inversely with size), verify tuning range, voltage distribution, and power on the bench, then commit to full-scale construction on the model dimensions. The 184-inch followed a three-stage chain: calculation (MacKenzie BP-140), half-scale model (this report), full-size bench test before installation.
half-scale resonates at ~2x full-scale frequency, and characteristic impedance is scale-invariant - for geometrically similar structures in the same mode with the same dielectric; lumped parts, couplers, losses and joints break exact similarity, so the model verifies the geometry-dominated partSource quote & editorial note
Performance of the model is considered sufficiently satisfactory to proceed with the full scale design and construction based on the model dimensions.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 16
Editorial note, tabletop extrapolation: A next machine's dee/stem/tank is already benchtop-sized, so the transferable form is the mockup itself — a cheap RF-only copy (no vacuum) of the dee-liner geometry, swept with a VNA before the vacuum parts are machined. Same lineage as UCRL-64 and MDDC-1045 already in this collection.
Cited in: Choosing Your Machine
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Three parasitics set a dee system's resonant range and deserve first attention: the capacity presented to the dee by the dummy dee, the minimum capacity of the tuning element, and the inductance at the dee throat (stem junction). Reducing any one raises the frequency.
Source quote & editorial note
These were the capacity presented to the dee by the dummy dee, the minimum capacity of the rotor, and the inductance at the throat of the dee.
Anderson, Half-Scale Model Tests on the Three Quarter Wave R.F. System — UCRL-31 (1947) — p. 10
Editorial note, tabletop extrapolation: Direct checklist for why a tank on the reference machine or a next machine does not resonate where the lumped-element estimate says — dummy-dee proximity, feedthrough/trimmer minimum C, and stem-to-dee transition inductance are the three knobs.
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Energy gain per turn strongly conditions resonant extraction quality: the report concludes that volts-per-turn substantially below the designed 280 keV/turn 'would result in sharp reduction of both extraction efficiency and optical quality' (its comparative runs at half (140), design (280), and double (560) kV per turn found the high-voltage case notably well behaved) [2026-08-28: the queued scan re-read was delivered upstream; the placeholder is replaced with the report's comparative values.]
turn separation achieved: 0.006 cyc units between the 14th and 15th turns (hand-corrected figures) for a 0.002 cyc-unit beam at 280 kV/turnSource quote & editorial note
volts per turn substantially lower than the designed 280 kev/turn would result in sharp reduction of both extraction efficiency and optical quality.
Editorial note, tabletop extrapolation: The quantitative ancestor of 'dee volts buy extraction': the reference machine's uncalibrated ~1.3 kV dee is one reason it is internal-beam-only, and a next machine's 5-13 kV target is what would make an extraction scheme thinkable - thinkable, not feasible, until the turn separation (delta_r ~ r*delta_E/2E), phase width, septum clearance, tune and bump design are actually computed.
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Let the computation overrule the folklore: the study found beams entering the extraction region approximately centered on the equilibrium orbit 'behave as well or better' than beams entering with substantial displacement - the computational basis and the earlier proposal this revised are the report's context (scan re-read queued).
Source quote & editorial note
beams entering the extraction region approximately centered on the equilibrium orbit behave as well or better than beams entering with substantial displacement.
Editorial note, tabletop extrapolation: The project-level lesson for a next machine — run the cheap simulation before committing hardware to any orbit-dynamics intuition, including intuitions published by people as good as Blosser and Gordon.
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The peak accelerating field at the gap center - the median-plane centerline value in this idealized geometry - saturates at V0/h, set by the APERTURE, not the gap: E(0) = (V0/h)/(1+alpha) = 0.994, 0.948, 0.870, 0.654, 0.489, 0.378, 0.306, 0.253, 0.216 times V0/h for k/h = 0.1 through 3.5. Narrowing the gap below the aperture height buys almost nothing.
E(0) = (V0/h)/(1+alpha), exact from eq. 6; k->0 limit E_x = (V0/h)*sech(pi*x/(2h))Source quote & editorial note
Table 1. k/h = 0.1: at x/h = 0, E/(V0/h) = 0.99388 [values verified against page image]
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 11
Editorial note, tabletop extrapolation: Sets the ceiling on CENTERLINE gap field for a dee redesign: with a 1-inch aperture (h = 0.5 in) and 2.5 kV dee-to-dummy, the median-plane peak cannot exceed ~2 kV/cm however tight the gap. Two cautions: local surface fields at electrode edges run above the centerline value - breakdown cares about those (dg-353) - and widening the aperture trades centerline field for beam height by the table's factors, not one-for-one at every k/h.
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Do not use the parallel-plate V/d estimate for dee-gap fields: for wide gaps (k/h >= 2) the mid-gap field sits ~25% below 2V0/(2k) because flux escapes through the aperture (k/h = 2.0: 0.378 vs 0.5 naive; 3.5: 0.216 vs 0.286), and the field maximum moves off-center to just inside the dee tips (x/h ~ k/h - 0.7); for narrow gaps the uniform-field picture fails entirely and V/d wildly overestimates the peak.
wide-gap plateau E ~ 0.75*(V0/k); max off-center for k/h >= 2: E_max at x/h = 1.2, 1.6, 2.2, 2.8 for k/h = 2.0, 2.5, 3.0, 3.5 [from Table 1]Source quote & editorial note
Table 1, k/h = 2.0: E/(V0/h) = 0.37823 at x/h = 0, maximum 0.38966 at x/h = 1.2 [verified against page image]
Beal, Computation of Electric Field and Potential of an Idealized Dee Geometry — MSUCP-12 (1961) — p. 16
Editorial note, tabletop extrapolation: Kills the tempting E = V_dee/gap for FIELD estimates on a next machine's geometry, where gap and aperture are the same order (k/h ~ 1) and neither limiting approximation holds - use the formulas or tables for the profile. Energy gain is a different question: absent transit-time effects the work across the gap is q*V0 whatever the profile; the profile changes transit-time factors and where field concentrates - and the surface fields at electrode edges, which the breakdown margin actually cares about (dg-353, dg-1028).
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Direct bremsstrahlung from a heavy projectile scales as ~1/M^2 of its mass and is usually insignificant; the X-ray sources that matter on a positive-ion machine are instead - the manual's list - characteristic X-rays from inner-shell vacancies, nuclear deexcitation, and bremsstrahlung from stray electrons.
bremsstrahlung ~ 1/M^2 -> proton bremsstrahlung negligible; hazard = characteristic X-rays + stray-electron bremsstrahlungSource quote & editorial note
The bremsstrahlung is approximately inversally proportional to the M2 where M is the mass of the incident particle. It is therefore usually insignificant for heavy particles.
Editorial note, tabletop extrapolation: Supports the program's standing model that dee-voltage electrons, not the proton beam's own bremsstrahlung, dominate the X-ray hazard on a sub-MeV proton cyclotron. Dominant is not sole: characteristic X-rays and any nuclear gammas from targets keep their own lines in the survey plan.
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Lacking design detail, the Army manual estimates the stray-electron X-ray source term of a positive-ion accelerator by assuming a reverse-directed electron current of 0.2*I (I = ion current) accelerated through 1/3 of the terminal voltage - an assumption the authors themselves label unreliable, offered to show that even a rough guess predicts "very considerable" X-ray production, not as a bounding figure. [Corrected 2026-08-23: an earlier version and its note presented the 0.2*I / V/3 pair as a bounding recipe. The source presents it as the opposite - an unreliable assumption that nonetheless gives a large number - and using it as a ceiling is under-conservative.]
I_e(back-streaming) ~ 0.2 * I_ion at E ~ V_terminal/3 - a rough historical source-term ASSUMPTION, not a boundSource quote & editorial note
If we assume that the ion current "I" results in a reverse directed electron current of magnitude 0.2*I that is accelerated through 1/3 the terminal voltage we would usually get a very considerable x-ray production.
Editorial note, tabletop extrapolation: Use this only as the lesson that stray-electron X-rays exist wherever there is RF voltage and vacuum, never as a ceiling. For a next machine's hazard analysis, plan around at least the peak-to-peak dee voltage as the electron impact energy - a planning floor, not a physical ceiling, since multi-transit RF processes can exceed single-gap figures - and let the measured X-ray endpoint from the survey be the authority the analysis answers to.
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As a rough shielding estimate for a heavy-ion accelerator's stray-electron X-rays, provide the shielding that would be required at 90 degrees from the beam axis of an ELECTRON accelerator of the same beam current and energy; ion-machine shielding "may not be so much less" than the electron case.
shield(ion machine) ~ shield(electron machine, 90 degrees, same I and E)Source quote & editorial note
As a rough estimate we offer that shielding which is required at 90 deg from the beam axis of an electron accelerator, with the same beam current and energy.
Editorial note, tabletop extrapolation: The conservative sizing pattern for a product-machine enclosure: bound the ion machine by an equivalent electron accelerator at the same current and at the maximum electron energy credible in the machine (at least peak dee-to-ground; dg-1036), then read the required thickness from electron-accelerator shielding data at that energy and verify by survey. The reference machine's chamber walls stopping its soft X-rays is a measured fact about ~10 kV operation, not a rule to inherit.
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Proton cross sections for nuclear interaction fall steeply below about 0.1 MeV because of the Coulomb barrier — but the light-nuclei exceptions the source waves off are exactly the targets amateurs use: 7Li(p,alpha) and 11B(p,alpha) run at measurable rates well below 100 keV. Evaluate the actual target isotopes before making radiation assumptions. [Corrected 2026-08-20: an earlier version endorsed the source's "nuclear-reaction-free" conclusion; nuclear data contradict it for light targets.]
sigma(p,nuclear) ~ 0 below ~0.1 MeV; barrier penetration grows sharply with E thereafterSource quote & editorial note
Because of the Coulomb barrier, proton cross sections for nuclear interaction are negligible below about 0.1 MeV. In light nuclei there are some exceptions which are of little interest here.
Editorial note, tabletop extrapolation: Closes the neutron question for the reference machine at ~150 keV-class energies EXCEPT via the light-nuclei exceptions the chapter waves off - and the exceptions differ in kind: the deliberate 11B(p,alpha) target yields charged alphas and gammas, not neutrons directly (the indirect path to check is secondary (alpha,n) on nearby low-Z materials); deuterium contamination is the direct neutron path, D(d,n) being thresholdless (see Ch. IV rule).
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(p,n) reactions are threshold-gated: the n-p mass difference (0.78 MeV) sets a floor, thresholds are of the order of an MeV for light and low-intermediate nuclei, and neutron emission becomes the dominant channel about 1 MeV above threshold - the manual's rough generalization; resonances and channel competition make real cases isotope-specific.
E_thr(p,n) > 0.78 MeV (stable targets), ~MeV for light nuclei; n-channel dominant at E > E_thr + ~1 MeVSource quote & editorial note
For light and low-intermediate nuclei, (p,n) thresholds are of the order of an MeV. Neutron emission becomes the dominant reaction when the incident particle energy exceeds the threshold by about 1 MeV.
Editorial note, tabletop extrapolation: The threshold-audit pattern for every machine energy bump: list materials the beam can strike, look up (p,n) thresholds, and confirm E_beam sits below them. At 170 keV (a next machine) every (p,n) channel on stable nuclei is closed, but the margin is not uniform: the lowest known stable-target threshold, 115In(p,n)115Sn at ~287 keV, leaves only ~120 keV, while the common structural metals and light targets sit >600 keV away (first structural channel 55Mn(p,n)55Fe at 1.03 MeV; 7Li(p,n) at 1.88 MeV). The audit must be redone on any energy bump, against the materials actually present, not a generic list. [Corrected 2026-09-13: previously claimed every stable-nucleus channel closed 'by >600 keV of margin'; that figure held for the structural metals and light targets but not for mid-Z nuclides like 115In (NNDC QCalc; see the safety page's activation section). Raised by an external site review alongside the dg-581 correction.]
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Neutron shielding is slow-down-then-capture in the manual's account - light nuclei (hydrogen) dominate energy loss, so hydrogenous concrete outperforms lead for neutrons - and the quoted rule of thumb: a facility shielded in concrete for X-rays 'generally contains adequate neutron shielding in the process', with the serious problem arising where the neutron hazard exceeds the photon hazard: proton and deuteron machines, the quote's own caveat.
concrete X-ray shield ~ adequate neutron shield (rule of thumb, <30 MeV); capture gammas must be shielded in turnSource quote & editorial note
it is a fairly accurate rule of thumb that for energies of interest here, the facility generally contains adequate neutron shielding in the process. The more serious neutron shielding problem occurs when the X- and gamma ray hazard is exceeded by the neutron hazard. Proton and deuteron accelerators are cases in point.
Editorial note, tabletop extrapolation: For any future neutron-capable operation (a deuterium species test, or a >1.9 MeV machine) the caveat is the operative part: an X-ray shield does not automatically cover the neutron hazard, and the source names proton and deuteron machines as exactly the case where neutrons dominate. The source's physics points to hydrogenous material (concrete, HDPE) rather than lead for the neutron component, but sizing it is a separate design problem - worked from the actual source term and verified by survey - not settled in advance by this rule of thumb.
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For first-pass neutron shield sizing the chapter uses the reactor-derived removal-cross-section method: penetration as exp(-Sigma_r*x), with removal cross-sections roughly three-quarters of the total at 8 MeV (somewhat larger for hydrogen), and its concrete coefficient Sigma_r ~ 0.094 cm^-1.
phi(x) = phi_0 exp(-Sigma_r x); sigma_removal ~ 0.75*sigma_total @8 MeV; Sigma_r(concrete) ~ 0.0942-0.0945 /cmSource quote & editorial note
Experimental removal cross sections are roughly three-quarters of the total cross section for 8 MeV neutrons. For hydrogen this fraction is somewhat larger. [Table III-7B] Ordinary Concrete 0.0942 ... Barytes Concrete 0.0945
Martin (ed.), Accelerator Radiation Protection — AD-755510 / USA-NLABS-TR-73-7, US Army Natick Laboratories (1972) — p. PDF 58 (printed 49) for the quote; PDF 57 (printed 48) for the exponential/reactor framing; PDF 60 (printed 51) for the concrete coefficient in Table III-7B
Editorial note, tabletop extrapolation: The one-line neutron shield ESTIMATOR for contingency planning - a D-D source term attenuates ~10x per 24 cm of concrete at the chapter's coefficient - used with its conditions: the coefficient is energy-derived (8 MeV; 2.45 MeV D-D neutrons remove differently), hydrogen content matters, and the chapter's own safety factors ride along. An estimate to verify by survey, never a design allowable.
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The 1972 occupational limits - accumulated whole-body dose <= 5 rem x (age-18) and <= 3 rem per calendar quarter (the quoted pair), with companion prose prescriptions for skin and extremities, and the manual's general-population limit set 'lower by a factor of ten' than occupational, not to exceed 0.17 rem/yr - are SUPERSEDED; extract only the structure: occupational vs public tiers, quarterly pacing, organ-specific limits. [2026-09-06 erratum, scan re-read: an earlier audit fix restated the public tier as '~30x below the occupational 5 rem/yr'; the manual's own framing is a factor of TEN, taken against the ~1.7 rem/yr average that 5(N-18) implies, and the companion values are numbered prose prescriptions (a)/(b), not a table. Reverted to the source's framing.]
HISTORICAL (1972 manual, prose prescriptions): 5(N-18) rem accumulated; 3 rem/qtr; public 'lower by a factor of ten', <= 0.17 rem/yr. MODERN: 10 CFR 20 / NCRP 116 - 5 rem/yr occupational, 0.1 rem/yr public, age-proration abolishedSource quote & editorial note
shall not exceed 5 rems multiplied by the number of years beyond 18. The dose in per calendar quarter shall not exceed 3 rems.
Editorial note, tabletop extrapolation: CAUTION — HISTORICAL NUMBERS, superseded by 10 CFR 20 / NCRP 116 (5 rem/yr occupational, 100 mrem/yr public, age-proration abolished). Keep for reading-era context and for the still-valid design pattern: public-tier limits ~10-50x below occupational drive product-machine enclosure design, since customers are "general population."
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Accelerator radiation differs from isotope-source radiation in ways that defeat isotope-calibrated instruments - the chapter's trio: PULSED time structure (the quoted cyclotron line: 50-200 us macropulses with microstructure at RF frequencies), ANISOTROPY, and MIXED neutron/gamma fields; the quote itself carries the pulse row.
cyclotron pulse structure: 50-200 us macropulse + microstructure at RF frequency (Table VI-1)Source quote & editorial note
Cyclotron positive ions 50-200 usec ... Microstructure at RF frequencies
Editorial note, tabletop extrapolation: The reference machine runs CW-RF but a beam bunched at 9 MHz; any future pulsed-RF operation (LDMOS duty-cycling) puts the machine squarely in this table — recheck every survey instrument's pulse response before trusting it.
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When counting radiation from a pulsed machine whose pulse length is shorter than the detector dead time (GM: 200-600 us; ion chamber 5-10 us; organic scintillator 0.01-0.1 us), the measured rate saturates at the pulse rate - provided each pulse registers at least one count and the detector recovers between pulses - no matter how intense the field.
for rho > pulse length, n'_max = pi (pulses/s); GM dead time 200-600 us (Table VI-2, Eq. VI-9)Source quote & editorial note
the second term in the equation above becomes zero and the number of counts per second, as is expected, becomes the radiation source pulse rate.
Editorial note, tabletop extrapolation: THE classic accelerator-survey trap, and the reason the program's survey doctrine prefers current-mode ion chambers over GM counters for any pulsed operation: a counter reading 60 cps at a 60 Hz pulse rate is reporting its saturation value, not a dose rate. The saturation reading appears when the field is strong; a weak pulsed field reads below the pulse rate, so equality with the pulse rate is the alarm signature.
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Dose-equivalent-proportional neutron instruments exist and work: an Anderson-Braun BF3 counter in polyethylene/boron cylinders read dose equivalent to +-10% from 0.04 to 10 MeV in the cited tests, and a properly made moderated-sphere rem counter held similar accuracy at intermediate energies - a rem counter beats converting raw flux by hand.
Anderson-Braun rem counter +-10% over 0.04-10 MeV; moderated thermal detector rem-proportional +-10%Source quote & editorial note
They obtained an accuracy of +-10% in measuring dose equivalent of neutrons over the range 0.04 to 10 MeV.
Editorial note, tabletop extrapolation: Justifies planning on one moderated rem meter as the primary neutron instrument for a D-D-class source term (2.45 MeV sits mid-band). Its band is not everything: moderated and scattered fields extend below 40 keV where response rolls off, so corners and maze mouths get checked against the instrument's stated energy response - and the calibration must be current.
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The most common cause of serious accelerator radiation exposure is entry — accidental or intentional — into the shielded target cell during operation; shielding quality is irrelevant if access during beam-on is possible, so access limitation (physical barriers + interlocks, generally both) is a first-class design requirement, from "a small shielded box with an interlocked lid" up.
access control = physical barrier + electrical interlock, both, sized to the hazardSource quote & editorial note
The most common cause of serious radiation exposures associated with accelerators, has been accidental (and sometimes intentional) entrance into the normally shielded target cell.
Editorial note, tabletop extrapolation: The product-machine posture in one line: an educational cyclotron IS the 'small shielded box with an interlocked lid' (Ch. I's phrase). Lid switch + beam-off interlock + machine-on light is the historically identified starting set for this machine class - not a sufficiency proof: fail-safe wiring (opening kills beam; no automatic restart on re-closing), periodic interlock function tests, and the access and bypass rules (dg-654, dg-1074) complete the design.
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Permit NO line-of-sight path for radiation through any access route or penetration, and then still evaluate the scatter path through the maze - the chapter's paired requirements.
no line-of-sight through any penetration; scatter path evaluated per the 0.05/sr ruleSource quote & editorial note
Naturally no "line of sight" path for radiation would be permitted yet it is also necessary that the scatter path through the maze be considered.
Editorial note, tabletop extrapolation: The audit rule for every feedthrough, window and joint in an enclosure: check sight-lines from the X-ray source point (the dee gap) outward, then bound the one-bounce leakage with the albedo rules (dg-1068). Geometry creates the streaming problem; material still sets what each bounce and wall costs, so both enter the estimate.
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Interlock philosophy, the quoted requirement: it should NEVER be convenient to remake an open interlock without someone physically going to the point of the break and, if the hazard no longer exists, re-establishing it there; the chapter pairs this with keeping systems simple and low-friction so operators are not tempted to defeat them (that passage: scan re-read queued).
simple + low-friction + no remote remake of a broken interlock (reset at the point of break)Source quote & editorial note
it should never be convenient for an operator or an experimentor to remake an open interlock without someone actually going to the position of the break and, if the hazard no longer exists, reestablishing the interlock.
Editorial note, tabletop extrapolation: Design requirement for the product controller: a tripped lid/door input must latch and require a local (at-the-lid) action plus console reset — a firmware-only "clear fault" button recreates the exact failure mode this rule exists to prevent.
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Fail-safe circuit logic, per the manual: require a complete path or presence of a signal to PERMIT accelerator operation, and let any open circuit or loss of signal disable it - so the commonest failures (broken wires, unplugged connectors, lost power) land in the safe state.
permissive = continuously energized circuit; any open / loss of signal -> beam offSource quote & editorial note
a fail-safe design may typically use a complete path or presence of a signal to permit accelerator operation and an open circuit or loss of signal to disable operation.
Editorial note, tabletop extrapolation: The normally-energized interlock-loop architecture: a series loop holding the RF/HV enable relay closed puts breaks, unplugs and power loss on the safe side. One loop is the architecture, not the whole chain - channels that must be independent stay independent (dg-1074), the loop gets exercised periodically (dg-1110), and any trip thresholds (a beam-current ceiling included) come from the machine's own hazard analysis.
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Prefer loss of operating time to loss of safety - the quoted principle: design so anticipated malfunctions trip the interlocked function to its safe state, accepting false trips as the price (the chapter's illustrative failure list - power loss, broken wires, sticky relays: scan re-read queued).
enumerate failure modes -> all anticipated failures trip safe; latching event memory + manual reset; downtime > riskSource quote & editorial note
For interlocks, however, the loss of operating time must be preferred to the loss of safety.
Editorial note, tabletop extrapolation: Two concrete requirements: (1) an FMEA-style enumeration of interlock failure modes with each shown to land safe; (2) latched annunciation: the controller must remember a mid-run lid opening even if reclosed, until deliberately reset.
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A person overlooked during the search before lockup must be able to POSITIVELY defeat the beam - not merely shut down some unassociated apparatus: the quoted requirement (the chapter's e-stop identification guidance sits alongside: scan re-read queued).
e-stops obvious to visitors, positively beam-defeating, hesitation-free cultureSource quote & editorial note
A person overlooked during the search before lockup must be able to positively defeat the beam instead of ineffectively shutting down some unassociated apparatus.
Editorial note, tabletop extrapolation: In-enclosure e-stop requirement for any walk-in product installation; even for benchtop machines the classroom master kill must cut the actual hazard (RF+HV+source), not merely the controller, and the no-blame-for-pressing norm belongs in the curriculum.
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Two quoted Morse principles anchor protection-system design: human safety should not be entrusted to one or more persons following a written routine; and even mechanized systems become routine after a time and hence may lose their effectiveness.
no safety-by-checklist-alone; counter habituation deliberately (the site's translation: vary the interlock-test scenario)Source quote & editorial note
Human safety should not be entrusted to one or more persons following a written routine. ... Even mechanized systems become routine after a time and hence may lose their effectiveness.
Editorial note, tabletop extrapolation: The strongest possible source endorsement for the program's hardware-interlock- over-procedure stance (procedures complement, never replace, the interlock chain), plus a curriculum idea: occasionally rotate the interlock test scenario so student operators never go through the motions.
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There is no substitute for the vigilance of personnel — automatic devices, interlocks, and remote area monitoring are ESSENTIAL BUT INSUFFICIENT without personnel training; engineering and administration are complements, not alternatives.
protection = engineered systems AND trained vigilant people; neither alone sufficesSource quote & editorial note
There can be no substitute for the vigilance of personnel. Automatic devices, interlocks and remote area monitoring systems are essential but insufficient to do the job without personnel training.
Editorial note, tabletop extrapolation: The counterweight to over-trusting the product machines' interlock chains — the curriculum's radiation-safety module is a safety SYSTEM component, not documentation overhead.
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Small organizations frequently cannot field a separate health-physics staff, so the operations staff acts as its own HP staff — a workable "way of life" ONLY if responsibilities and priorities are explicitly defined; in larger setups, keep HP advisory and leave radiation-safety responsibility with the operational supervisor.
small org -> operator doubles as HP; must write down who owns which safety decisionSource quote & editorial note
it may be necessary for the operations staff to act as the health physics staff as well. Though less then ideal, this condition will frequently be a "way of life". Under these conditions it is of paramount importance to define responsibilities and priorities.
Editorial note, tabletop extrapolation: A 1972 acknowledgement, with conditions, of the small-facility reality in which one person wears both the operator and radiation-safety hats. The conditions transfer to any teaching installation - the documentation names the RSO-equivalent role and its decision rights - and the arrangement itself must clear the jurisdiction's requirements: registered machines commonly require a named, qualified RSO (/legal/), which written role definitions support but do not replace.
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Air-activation species (13N, 15O) from (gamma,n) are 'of concern only to electron accelerators of energies in excess of 15-20 MeV' - the manual's practical judgment. The underlying thresholds sit lower (14N(gamma,n) ~10.6 MeV, 16O(gamma,n) ~15.7 MeV); yield, not kinematics, sets the manual's concern line. 16N (7.1 s) matters inside recirculating ducting.
thresholds: 14N(gamma,n)13N ~10.55 MeV, 16O(gamma,n)15O ~15.66 MeV; the manual's practical concern line: >15-20 MeV electron machinesSource quote & editorial note
The threshold for (gamma,n) reactions are of sufficient magnitude to make the production of 13N and 15O of concern only to electron accelerators of energies in excess of 15-20 MeV.
Editorial note, tabletop extrapolation: Scopes air activation out of every current and planned program machine - all far below even the 10.6 MeV threshold - so the air-handling design concentrates on ozone (dg-1085). When a reviewer asks, cite the actual thresholds alongside the manual's concern line rather than conflating them.
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Shape sector iron by formula-guided empirical iteration, not a priori specification: pick "reasonable" <B>(r) choices, observe the flutter F(r) that results, and test the combination against tune formulae rather than demanding the iron fit pre-selected profiles exactly.
iterate {<B>(r), F(r), tan(spiral)} -> Smith-Garren vz^2, vr -> accept/reject; do not fix profiles a prioriSource quote & editorial note
The process is a trial and error search, with general guidelines and test criteria for success.
Editorial note, tabletop extrapolation: Directly transferable design-process pattern for any pole or shim work on a next machine: let FEMM play the role of the Nevis model magnets, with analytic tune formulae as the accept/reject criteria - within FEMM's 2-D limits (azimuthal structure needs a 3-D model or the measured map; the playbook's tracker closes that loop). The final accept/reject is the measured field, exactly as it was at Nevis.
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Evaluate axial and radial tunes first with analytic formulae (Smith-Garren), then verify at critical places — especially large radius where derivative terms grow — by exact orbit-integration computer solutions.
analytic vz,vr everywhere; exact orbit codes at critical radii (large r, extraction)Source quote & editorial note
first evaluated using the Smith-Garren formula, checked at critical places, especially at larger r, by exact orbit motion computer solutions.
Editorial note, tabletop extrapolation: Exactly the field-solver-plus-orbit-tracker pipeline an amateur design can run. The Nevis precedent: spend the expensive tracking where the cheap formulae are least trustworthy - large radius and the extraction region on their machine - and anywhere else the smooth approximation visibly strains.
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Build adjustability into pole and sector iron: Nevis planned final 'touch up' machining of these pieces with the final iron in place, driven by magnetic field-mapping studies - the quote; bolt-on, pin-located implementation details are the site's editorial translation of what makes such iteration cheap.
removable edges + removable center tips + slotted repositioning + locating pinsSource quote & editorial note
a final "touch up" machining of these pieces, with the final iron in place on the basis of magnetic field mapping studies.
Editorial note, tabletop extrapolation: Fully transferable at any scale — design a next machine's shims and center plugs as bolt-on, pin-located pieces so field-map-driven iteration does not mean remaking the poles.
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Harvest resonance lines to avoid from other machines' documented beam-loss experience: Nevis, alerted by ORNL's observed losses in ORIC, designed its tune trajectory to avoid specific coupling lines - the report names them (scan re-read queued for the identifications).
keep (vr,vz) trajectory clear of (3vr-vz)=3 and (vr+3vz)=2 (plus the standard low-order lines)Source quote & editorial note
alerted by the ORNL studies of observed beam loss in the ORIC cyclotron to try to avoid
Editorial note, tabletop extrapolation: Method transfers directly — a tune plot should carry resonance lines sourced from operating-experience literature, not just textbook theory; a weak-focusing tabletop crosses fewer lines but the audit habit is the point.
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Choose the resonator mode and geometry so tuning elements sit outside the main vacuum chamber: the half-wave resonator 'permits the rotating capacitors to be located outside... for good shielding from both the magnetic field and radiation' - the quote; the iron tuner housings are the report's detail (scan re-read queued).
half-wave resonator puts voltage node / tuner outside chamber; 2-in. Fe housing shields rotorsSource quote & editorial note
a half-wave resonator permits the rotating capacitors to be located outside the main vacuum chamber for good shielding from both the magnetic field and radiation
Editorial note, tabletop extrapolation: The placement principle transfers: keep variable capacitors, trimmers and drive mechanisms of a next machine's tank outside the pole gap and chamber, where field, beam spray and pumpdown cannot reach them - where the geometry allows it.
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Establish the RF system's variable parameters on a reduced-scale model plus computation before full-scale construction: the design 'used a 1/2 scale model, in conjunction with detailed computer calculations, to establish all parameters which can be varied' - which parameters, and the mode-clearance criteria, are the report's enumeration (scan re-read queued).
1/2-scale RF model + computation -> full-scale build; cross mode kept well below 2x main mode over tuning rangeSource quote & editorial note
The design has used a 1/2 scale model, in conjunction with detailed computer calculations, to establish all parameters which can be varied
Editorial note, tabletop extrapolation: At tabletop size the "scale model" is the full-size mockup on the bench — cold-test a next machine's dee/stem with a VNA before power exists; the mode-spectrum audit transfers verbatim.
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DC-float the dee/resonator so that a negative bias 'of amount sufficient to control multipacting' can be applied - the Nevis provision, with their planning value at -500 to -2000 V (Part II).
Nevis planning value: dee DC bias -500 to -2000 V (Part II, p.48)Source quote & editorial note
The dee resonator will be dc floating so a negative bias of amount sufficient to control multipacting can be applied.
Editorial note, tabletop extrapolation: Directly relevant at a next machine's planned 5-13 kV dees, where multipactor bands are widest: a 1971 operating-lab remedy with a concrete magnitude to scale from. Bias works by breaking the multipactor resonance condition; what trajectories do in detail depends on the local fields, so 'sufficient to control' is found empirically - exactly as Nevis wrote it.
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Buy shielding with geometry before mass, as the Nevis layout does: the underground beam stop aims away from occupied areas - which the report says greatly eases shielding and background - with secondary beams taken off at large angles and bends between production targets and experimenters.
beam stop aimed away from people; large-angle takeoff; bends between target and experimenters (the report's layout choices)Source quote & editorial note
Since the underground beam stop is aimed away from the experimental areas, this greatly eases shielding, and subsequent background problems
Editorial note, tabletop extrapolation: Direction-dependence of secondary radiation is universal even though the 550-MeV numbers are not: orient any future target station and Faraday-cup dump so the forward cone points at mass, not people. The specific takeoff angles and bend counts are per-facility physics rather than constants - lay out first, then let the survey confirm the geometry did what was expected.
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Build accelerator safety interlocks to the 1974-era trend or better: fail-safe circuitry with self-checking - the properties the era's designs pursued as they moved to solid state - so that component failures and stuck states reveal themselves instead of silently defeating the interlock.
fail-safe + self-checking logic; solid state preferred over relays (NBS Handbook 107 lists general requirements)Source quote & editorial note
The trend seems to be toward more elaborate systems which utilize solid state devices, fail-safe circuitry and self-checking circuits.
Editorial note, tabletop extrapolation: Directly actionable for the next machine and the tiny controls spec: an amateur interlock chain (door, HV, RF-enable, radiation monitor) should be fail-safe and self-testing. Those properties come from the circuit design, not the device family - solid-state parts can fail shorted - so the design proves de-energize-to-safe behavior and exercises each channel periodically. What was state of practice in 1974 is trivially cheap in 2026.
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Take the fast-neutron half-value thickness of ordinary concrete for cyclotron-target neutrons as approximately 10 cm (ORNL measurement over thick C, Al, Cu, Ta targets under proton, deuteron, alpha, and carbon beams).
HVT(ordinary concrete, cyclotron-target fast neutrons) ~ 10 cmSource quote & editorial note
fixes the half-value thicknesses of ordinary concrete for neutrons from cyclotron targets at approximately 10 cm
Editorial note, tabletop extrapolation: The corpus's first literal shielding number for MeV-class cyclotron neutrons. The reference machine's proton operation sits below its (p,n) thresholds and makes none - deuteron operation is the standing exception (D-D is thresholdless) - and this ~10 cm HVT is the sizing constant the moment any machine or D-beam work crosses into neutron production; it was measured for cyclotron-target spectra, so re-check it for a materially different spectrum.
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Adopt the exposure design philosophy the source's era called ALAP (As Low As Practicable) - not merely staying under limits, but reducing further wherever technology and economics permit - and recognize it works only as a standing management commitment. Modern regulation's successor term is ALARA, As Low As REASONABLY ACHIEVABLE, with its own regulatory definition.
design target: exposures as far below limits as practicable/reasonably achievable (era: ALAP, AEC Reg. Guides 8.8/8.10; modern: ALARA, 10 CFR 20)Source quote & editorial note
the As Low As Practicable philosophy can be adopted and put into practice only where there is a firm commitment by management to do so
Editorial note, tabletop extrapolation: The governing philosophy any licensing narrative must speak fluently - in its modern wording (ALARA), since the terms are not interchangeable in a regulatory context. For the home program it means shielding and interlock decisions justified as 'as low as reasonably achievable', not 'under the limit'.
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Choose fast-neutron shielding for high density combined with LOW atomic number; the attenuation cross section per nucleon falls as Z rises (nucleons shadow each other inside a large nucleus), which is why ordinary concrete outperforms lead per unit weight against neutrons.
sigma per nucleon decreases with Z (shadow effect); merit ~ density x (hydrogen + light-element fraction)Source quote & editorial note
one should seek substances which combine high density with low atomic number. Among convenient and practical materials none would seem better than concrete.
Editorial note, tabletop extrapolation: The shadow-effect argument is a >100 MeV argument. At low energy the conclusion usually still favors hydrogenous materials - elastic scattering on hydrogen dominates moderation - but merit depends on the objective: moderation, capture, dose, or secondary-gamma control (hydrogenous shields buy moderation with 2.2 MeV capture photons, dg-1329). Concrete, water and polyethylene win per dollar for neutron MODERATION, with the gamma bill accounted separately.
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Shield for machine-generated loss points, not just the target: besides the forward cone from the probe, Moyer found 'a general spray of neutrons due to the deuteron beam grazing the interior of the dee' - his report characterizes its intensity and azimuthal extent (scan re-read queued for those figures).
Source quote & editorial note
Besides the neutron beam cone from the probe there was found to be a general spray of neutrons due to the deuteron beam grazing the interior of the dee.
Editorial note, tabletop extrapolation: Wherever beam is lost - dee edges, septum, probe stalk, chamber wall - is a candidate source, and a survey plan that only looks downstream of the target can miss most of the emission solid angle. Moyer's spray was found by surveying: that is the lesson.
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Where geometry is complicated, trust model tests over calculation: MacKenzie preferred a mechanically awkward layout that could only be settled empirically, noting that dimensions calculable "fairly exactly" were the sole advantage of the calculable variant.
Source quote & editorial note
dimensions can be calculated fairly exactly whereas in the system shown in Figure 5 one must depend on model tests (which are safer anyway).
Editorial note, tabletop extrapolation: Transmission-line formulas ignore end effects, bends, and support hardware; for any resonator whose geometry is not a textbook line, a cheap model measurement outranks the calculation it checks.
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Predict full-scale RF power from model measurements and state both numbers: 400 W (48 Mc) and 600 W (18 Mc) of model input for 1500 V on the dee scaled - via V-squared and the sqrt(2) Q correction - to 28 and 42 kW for 15 kV; MacKenzie also flags that the model's bad joints and brass surfaces bias it pessimistic against the copper full-scale build.
P scales as V^2 x (Q_full/Q_model)^-1; model bad joints/brass make prediction conservativeSource quote & editorial note
The 1/2 scale model uses about 400 watts input to the oscillator at 48 megacycles and 600 watts input at 18 megacycles to produce 1500 volts on the dee.
Editorial note, tabletop extrapolation: Dee power scales as voltage squared: measure watts-per-volt-squared on the bench and the amplifier requirement for any target voltage falls out. Mind the quantity - the model figures are OSCILLATOR INPUT, so the scaled 28-42 kW carries the model oscillator's efficiency inside it: separate wall loss from drive-chain overhead when budgeting a modern amplifier (dg-313, dg-316), and budget for joint quality and surface material shifting Q.
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Start every target heat-load estimate from the deposited beam power P = I x dE (current times energy lost in the target). Corwin's worked example: 100 nA losing 43 keV in a 380 ug/cm2 PbCl2 target gives P = 0.0043 W into a 1 mm x 3 mm (0.03 cm2) beam spot. For a target thick enough to stop the beam, dE is the full beam energy.
P[W] = I[A] x dE[eV] / z (z = charge state; z = 1 for protons). Corwin's example: 1e-7 A x 4.3e4 eV = 4.3e-3 W over A = 0.03 cm2Source quote & editorial note
In a typical charged particle experiment 100 na of beam loses 43 keV in a W = 380 ugm/cm2 PbCl2 salt target
Editorial note, tabletop extrapolation: A 1 uA, 170 keV proton beam fully stopped in an internal target deposits 0.17 W — forty times Corwin's example — into whatever spot the beam makes; the entire current limit of a thin uncooled target follows from this one number and the two removal channels (radiation, conduction) he works out next.
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Radiation limit (Corwin): a thin foil radiates from both faces, so shedding power P to surroundings at T0 follows P = e*sigma*2A*(T^4 - T0^4). For his 0.0043 W / 0.03 cm2 example, emissivity 1.0 needs about 106 C - and a realistic e = 0.1 needs about 330 C.
P = e*sigma*2A*(T^4 - T0^4), sigma = 5.67e-8 W/m2K4, factor 2A = both faces; e ~ 0.1 realistic for thin films, possibly lowerSource quote & editorial note
the target appears transparent and all of the radiating surface of a solid may not be present in a thin film.
Editorial note, tabletop extrapolation: Radiation is the only cooling channel a self-supporting foil in vacuum really has at the spot: solving Corwin's equation for a stopped 0.17 W beam on a 0.03 cm2 spot with e = 0.1 gives roughly 1200 C equilibrium - above most evaporated films' damage points and hot enough to anneal or evaporate many (boron itself melts higher, but its substrate and adhesion rarely survive) - which is why the spot is enlarged or the film backed (dg-1160).
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Conduction limit (Corwin): heat conducted radially from a beam spot of radius r_b to a frame at r_t obeys P = 2*pi*k*h*dT / (1/2 + ln(r_t/r_b)) - thickness h enters linearly. His example (h = 0.65 um, r_b = 0.1 cm, r_t = 0.64 cm, P = 0.0043 W): an insulator with k = 2 W/mK runs a ~1240 K rise - it fails - while a metal with k ~ 200 W/mK holds the quoted ~12 C rise.
P = 2*pi*k*h*dT * (1/2 + ln(r_t/r_b))^-1; k(salts) ~ 1-10 W/mC, k(metals) ~ 200 W/mCSource quote & editorial note
so a metal target could conduct the heat away with a 12 C rise in temperature.
Editorial note, tabletop extrapolation: The 100x conductivity gap between salts/insulating compounds and metals is the single biggest lever on target survival: a boron film on a thick copper or silver backing is conduction-cooled through the backing, while the same film self-supported is radiation-only (dg-1159). Thickness enters linearly, so doubling film thickness halves the rise at fixed power.
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Process-selection ladder (Adair & Kobisk, ORNL): rolling is by far the most material-conserving route to thin metal foils - the quoted superlative; the paper's Table 1 assigns per-element routes (its boron row: evaporation, 20-250 ug/cm2 self-supporting or 10-1000 on a metal backing) and its text records the low material efficiency of evaporation (exact figures: scan re-read queued).
Table 1 legend: a = evaporation, b = rolling, c = electrolytic, d = casting or pressing; backing 1 = self-supporting, 2 = metal backing, 3 = thin carbonSource quote & editorial note
Rolling is by far the most conservative process with regard to material loss in preparing thin targets. ... The vacuum evaporation process is very inefficient and frequently evaporation efficiencies of only 1% are obtained.
Thomas & Karasek (eds.), Proceedings of the Fourth Annual Conference of the Nuclear Target Development Society — ANL/PHY/MSD-76-1, Argonne National Laboratory (1975) — p. PDF p.18 (printed p.3) for Table 1's boron row; the efficiency sentence spans PDF p.17 (printed p.2) and PDF p.23 (printed p.8), the table intervening
Editorial note, tabletop extrapolation: The boron row of Table 1 is the direct answer for a B target: evaporation is the only listed route — 20-250 ug/cm2 self-supporting, 10-1000 ug/cm2 on a metal backing (boron is too brittle to roll). For thin-film evaporation recipes themselves cross-cite ORNL-3021; this table tells you which recipe book to open.
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Proton targetry is forgiving - 'with a proton beam, targetry is just no problem' (Erskine, ANL): even a leftover gold target gave 5.1 keV FWHM at 16 MeV, because energy loss scales as projectile charge squared at equal velocity, so proton losses are the floor of the scaling.
dE ~ thickness x (M/E)^0.6 x Z_proj^2; straggling ~ Z_proj x sqrt(thickness x Z/A); carbon ~2.5x the energy loss of gold per ug/cm2Source quote & editorial note
With a proton beam, targetry is just no problem. One can obtain very nice high-resolution results.
Editorial note, tabletop extrapolation: Direct license for a proton machine: target thickness and uniformity tolerances that dominate heavy-ion work are second-order for protons, so a thick-ish imperfect boron layer costs beam-energy definition, not feasibility. When tempted by heavier beams, budget with the Z^2-at-equal-velocity scaling and check real stopping tables (SRIM/NIST-class) at low energy, where effective-charge effects bend the simple law.
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Size the target heat problem by straight beam-power arithmetic before any material choice: P(W) = particle rate x energy per particle. Folger (GSI) example: 3e11/s of 17.5 MeV/u 238-U carries ~208 W total; focused to ~0.2 cm^2 that is ~1 kW/cm^2 specific deposition.
P[W] = (dN/dt) * E[J]; specific load = P / spot areaSource quote & editorial note
If the beam is focused to an area of about 0.2 cm2, the resulting specific energy depositions amounts to 1 kW/cm2.
Editorial note, tabletop extrapolation: The reference machine at ~3 nA / ~150 keV deposits ~0.5 mW - no realistic solid target is troubled by half a milliwatt. Rerun the two-line arithmetic at every upgrade, using the energy LOST IN the target rather than incident beam power where targets are thin: a 10 uA / 1 MeV machine puts up to 10 W into a mm-scale spot, which is rotating-target or water-cooled-backing territory.
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Expect oscillation start-up failure specifically where the dee IS the oscillator tank: the report contrasts machines driven from external oscillators with their own resonant tanks (slight difficulty) against simple-dee-as-tank-circuit systems, which have trouble breaking into full oscillation (the quoted difficulty; the contrast's other half is on the same page - scan re-read queued).
Source quote & editorial note
in cyclotrons using a simple dee system as the tank circuit difficulties are encountered in getting the oscillator to break into full oscillation.
Editorial note, tabletop extrapolation: DIRECT: this names the exact configuration of the reference machine - a simple dee system as the tank circuit - and matches its documented pattern of RF amplifiers failing to bring the dee to voltage. Multipactor loading in the ~100 V band is the report's named mechanism and a testable CANDIDATE cause, not a confirmed diagnosis: the bias and drive-through cures (dg-1274) double as the discriminating experiments.
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The report's menu for multipactor-band start-up: (1) bias the dee and stem several kV from ground - customary on FM cyclotrons - which this report rejected as 'too awkward to apply, chiefly because the variable frequency requirement had already led to a rather complicated mechanical design'; (2) drive the oscillator strongly from an external source so the voltage rises through the ~100 V multipactor region faster than the loading builds (the quoted mechanism); the report's own contribution is the impulse-shock start. [2026-09-06 erratum, scan re-read: the stated cost of dee bias is mechanical complexity compounding an already-complicated variable-frequency design, not HV isolation as previously written.]
Source quote & editorial note
multipactor loading, which occurs with voltages of the order of a hundred, cannot build up sufficiently to prevent the rise of voltage through the multipactor region.
Editorial note, tabletop extrapolation: The decision menu for any machine that stalls in the multipactor band: bias, drive-through, or impulse shock. On a small machine the driven start maps to an external exciter ahead of the power stage; the bias cure maps to a DC offset on an insulated dee (dg-320, dg-805), with the magnitude found empirically.
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Keep the magnet gap well under the orbit radius wherever the field must be shimmed to a prescribed shape: the source calls proper shimming impractical when gap length is 'much greater than one-half the radius' - a soft boundary, not a cliff at rho/2.
l_gap <= ~rho/2 for shimmable fieldSource quote & editorial note
The properties of a magnetic field in space make it impractical to obtain a properly shimmed field if the gap length is much greater than one-half the radius p.
Editorial note, tabletop extrapolation: An 8-12 in. pole with a 1-2 in. gap sits far inside this limit, which is why small cyclotron shims work at all; the rule bites for any short-radius bending/analysis magnet where a generous gap is tempting for access.
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First-pass excitation: NI = 2.02 x H(gauss) x gap(inches) for the air gap alone; in well-proportioned iron-return magnets the gap consumes 85-95 per cent of the total mmf, so take total NI ~ 1.15 x (NI)_gap as the starting approximation and let the model (or simulation) refine it.
(NI)_g = 2.02 * H[G] * l_g[in]; NI_total ~ 1.15 * (NI)_gSource quote & editorial note
the quantity (NI)g represents 85 to 95 per cent of the total mmf required (i.e., the efficiency ranges from 85 to 95 per cent), and Eq. 7 can be used to give a useful first approximation
Editorial note, tabletop extrapolation: The same arithmetic every H-frame designer runs today (Wouters and Zickler's CAS notes corroborate the sizing). The 85-95% efficiency band is the source's result for WELL-PROPORTIONED iron-return magnets: use it as a sanity check on FEMM excitation for a magnet in that class, and expect worse from lean yokes, corners, or parasitic joint gaps (dg-128).
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The product of coil power and conductor weight is a design invariant set by ampere-turns and coil size: P x W_c = 0.118 x (NI/10^5)^2 x (mean turn length, in.)^2 for copper (0.131 for silver, 40 C mean). Choose the P/W_c split afterwards from cooling or cost — it fixes current density via J[A/in^2] = 486 x sqrt(kW/ton) for Cu.
P[kW] * W_c[tons] = 0.118 * (NI/1e6)^2 * (mean turn length, in.)^2 for copper (0.131 silver, 40 C mean) - the 0.118 rides with MEGA-ampere-turns squared and length squared (cf. dg-212); J = 486*sqrt(P/W_c)Source quote & editorial note
the product of the power and weight of a coil conductor depends on the ampere turns and the mean diameter of the coil.
Editorial note, tabletop extrapolation: The cleanest statement in this collection of the copper-vs-power trade: double the copper, halve the dissipation, at fixed NI. Lets a coil be resized on one line when a surplus supply or a heat limit is the binding constraint.
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Continuous-duty current-density ceilings from calutron practice: ~1600 A/in^2 (2.5 A/mm^2) is the upper limit for oil-cooled coils, ~1000 A/in^2 (1.55 A/mm^2) for open bus bar in free convection; the project's economic balance point P/W_c ~ 5 corresponded to ~1050 A/in^2. Careful cooling design is what buys anything higher.
J_max ~ 1600 A/in^2 oil-cooled continuous; ~1000 A/in^2 free-convection busSource quote & editorial note
For continuous operation, 1600 amp/sq in. is about the upper limit used for oil-cooled coils. This compares with 1000 amp/ sq in. for open bus bars cooled by free convection
Editorial note, tabletop extrapolation: Brackets modern air-cooled small-magnet guidance from the 1940s operating side - mapped to the right geometry: the 2.5 A/mm^2 was for OIL-cooled calutron coils, and the 1.55 A/mm^2 for open bus bar with free-convection area a wound coil does not have. A passively cooled wound tabletop coil therefore belongs below both, in the ~1 A/mm^2 territory of the coil rules (dg-092), unless its own thermal test justifies more.
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Coil space factor (copper volume over coil-container volume) came out 0.37 and 0.30 on two experimental models forced to use available conductor sizes rather than purpose-designed ones - the quote; the report's expectation for designed conductor is its surrounding discussion (scan re-read queued).
space factor ~ 0.5 designed; 0.30-0.37 with off-the-shelf conductorSource quote & editorial note
Two experimental models had values of 0.37 and 0.30, but in both cases it was necessary to use conductor sizes which were available but not specifically designed for the job.
Editorial note, tabletop extrapolation: Amateur coils are usually wound from whatever magnet wire is available: budget a pessimistic 0.3-0.4 space factor when sizing the coil window, and read handbook ~0.5 figures as purpose-designed-conductor numbers.
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Magnet cost scales roughly linearly with beam radius at fixed Hrho: with gap length proportional to rho and H proportional to 1/rho, both power and copper weight scale ~rho and steel weight scales as rho^n with 1 < n < 2. Powell: choose radius on beam physics, not on magnet cost, because cost climbs only proportionately.
P ~ rho; W_c ~ rho; W_steel ~ rho^n, 1<n<2 (at fixed H*rho)Source quote & editorial note
both the first cost and the power cost of a magnet increase almost proportionately with an increase in beam radius.
Editorial note, tabletop extrapolation: Useful scaling honesty for any pole-diameter trade study — going from 8 to 13 in. poles at fixed final energy is a near-linear cost move, not a quadratic one, so long as the field comes down as the radius goes up.
Cited in: Choosing Your Machine
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Budget for the sideways force that tries to INCREASE pole area, not just the attraction across the gap: any split through a pole (segmented poles, bolted pole caps, diametral joints) sees a spreading force; each half of a diametrally split circular pole is pushed sideways with (1/2)(H^2*l*a/8pi), l = gap length, a = pole diameter.
F_spread(each half) = 0.5 * H^2 * l * a / (8*pi) [cgs]Source quote & editorial note
The forces tending to separate the halves are surprisingly large and if overlooked can be disastrous.
Editorial note, tabletop extrapolation: Directly relevant to removable pole caps and bolt-on shim plates on a small H-frame: check the retention for lateral load wherever the joint geometry can see one - splits with a component parallel to the flux see spreading, while a complete cap on a plane parallel to the pole face mainly sees the axial pull. The formula is the diametral-split case, not every joint's.
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Working force formulas from the report's engineering pages (English units): pull between pole faces F[lb] = (kG)^2 x area[in^2] / 1.735 (the quoted line); its companion values give conductor force F[lb] = kG x amp x length[in] / 1750 and a copper strip hot-spot check dT[C] = 0.0094e-6 x width^2 x J^2.
F_pole[lb]=kG^2*A[in^2]/1.735; F_cond[lb]=kG*I*l[in]/1750; dT_Cu=0.0094e-6*w^2*J^2 [2026-09-06 re-read: the page prints the heating constant's multiplier as a bare 10^6 with no minus sign, while its resistivity rows print 10^-6 clearly; dimensional check requires e-6 - an original typo, page-image verified. The 1.735 pole-force constant checks against B^2/2mu0 to 1%.]Source quote & editorial note
Force on conductor (lb) = 1/1750 X kilogauss X amp X length (in.) Force between pole faces (lb) = 1/1.735 X (kilogauss)^2 X area (sq in.) Heating at center of conductor, degC = 0.00940 (Cu) / 0.00821 (Ag) X 10^6 X (inches of width of conductor)^2 X (amp/sq in.)^2
Wakerling & Guthrie (eds.), Magnets and Magnetic Measuring Techniques — TID-5215, Radiation Laboratory, University of California (1949) — p. PDF 31 (printed p. 21), Table 1.1 'Magnet Design Data', TID-5215 Vol. 1
Editorial note, tabletop extrapolation: The 1.735 pole-force constant is the imperial twin of B^2/2mu0 and matches it to 1%; the hot-spot width formula is a one-line check before winding wide flat strip on a driver-amplifier-fed coil.
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Keep the driving coils as close to the air gaps as possible - the quoted reason: less spreading and bowing of the field, and the largest usable fraction of gap area; the report's design discussion builds its order of operations around this (gap, field and uniformity first, then iron topology - full sequence: scan re-read queued).
Source quote & editorial note
With the size and proportions of the gap selected from the foregoing considerations and the required field strength and uniformity determined, several magnet types could be conceived which might satisfy the requirements. ... After the type of magnet has been selected, it is possible to calculate approximately the weight of copper and steel
Wakerling & Guthrie (eds.), Magnets and Magnetic Measuring Techniques — TID-5215, Radiation Laboratory, University of California (1949) — p. quoted principle on PDF 25 (printed p. 15) as cited; the order-of-operations sequence is on PDF 24 (printed p. 14), Sec. 6 'GENERAL DESIGN PROCEDURE'
Editorial note, tabletop extrapolation: Coils-near-gap is the reason cyclotron coils hug the poles rather than the yoke; the usable-fraction-of-pole-area argument is exactly the good-field-radius economics of a small machine.
Cited in: Choosing Your Machine
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The model-magnet scaling law: a linear scale model built from steel with the same magnetic properties, operated at the same field strength (same B everywhere, currents scaled to keep NI per gap-length), reproduces the prototype's field distribution exactly — magnetostatics has no intrinsic length scale until saturation properties differ. Leakage coefficients measured on the model apply directly to the full-scale magnet; forces follow with area (L^2) scaling.
geometric scaling at fixed B and fixed material B-H curve; L_leakage(model) = L_leakage(full scale)Source quote & editorial note
a linear scale model built from steel with the same magnetic properties as planned for the prototype magnet and operated at the same field strength will give results directly applicable to the prototype.
Editorial note, tabletop extrapolation: The physics that lets FEMM stand where models stood — and the terms of validity are the same for both: correct B-H data and correct geometry. Any cheap sub-scale mock-up of a planned magnet obeys it too, provided the steel matches and B is held, not NI.
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Audit the flux through EVERY iron member - the report's ballistic-loop method: wound loops read by a ballistic integrator, with loop-flux differences over enclosed-area differences giving local leakage components; the quoted judgment is that 10-15 kilogauss in the yokes gave good flux density without excessive permeability drop.
B_member = (phi_loop difference)/(A_steel); leakage component = d-phi/d-A between loop pairsSource quote & editorial note
By dividing the flux difference between any two loops by the area enclosed in the difference of the two loops, the average leakage flux density in that area can be calculated. Through the proper selection of pairs, either the vertical component of the leakage flux or the horizontal component may be found.
Wakerling & Guthrie (eds.), Magnets and Magnetic Measuring Techniques — TID-5215, Radiation Laboratory, University of California (1949) — p. PDF 142 (printed p. 132) for the quoted 10,000-15,000 gauss judgment (cited page 141 is off by one); method on PDF 140-143 (printed 130-133), Sec. 2.5 'Flux-density Measurements'
Editorial note, tabletop extrapolation: The 10-15 kG working band for structural mild steel is the same number modern small-magnet guidance gives (cf. Wouters; Zickler CAS) — and the loop-audit method is the measurement twin of integrating B over member cross-sections in a FEMM postprocessor: every member gets a number, every number gets a verdict.
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Saturation red-line by permeability, with a material margin: at 17,200 G the model core steel had mu ~ 150, and the (magnetically poorer) full-scale steel would drop to mu ~ 118 — "dangerously low," possibly worse in local regions; the fix was 24 per cent more iron to bring the core to ~14,000 G. Judge margins on the PROTOTYPE material's B-H curve, at the worst local induction, not the average.
keep working mu >> 100; core fix sized to reach ~14 kGSource quote & editorial note
the corresponding permeability would drop to 118, which is dangerously low. In certain localized regions it might even be lower.
Editorial note, tabletop extrapolation: A quantitative 'too far' AS THAT PROJECT JUDGED IT: mu ~ 100-150 at the working point was their failure territory, fixed by 24% more iron. What a given magnet tolerates depends on its mmf budget and field-quality needs; the transferable instruction is auditing against the ACTUAL steel's B-H curve - the same reason a FEMM model of an H-frame is only as good as the B-H table fed to it.
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Convert the model into a force ledger before detailing structure - the report's Alpha II ledger combines magnetic wall pressures with atmospheric loads per wall; the quoted method point: forces computed from the average field over a region UNDERSTATE the true force, so use the mean of the squares.
F ~ integral H^2 dA (use mean of squares); tabulate per-member envelope with marginSource quote & editorial note
The magnetic forces were then combined with the force of the atmospheric pressure to give the total force. Magnetic force in tons = (kilogauss)^2 (area in square inches) / (1.735)(2000)
Wakerling & Guthrie (eds.), Magnets and Magnetic Measuring Techniques — TID-5215, Radiation Laboratory, University of California (1949) — p. PDF 144 (printed p. 134), Sec. 2.6 'Magnetic Forces'
Editorial note, tabletop extrapolation: On a tabletop the same ledger is short but identical in kind — gap pull, atmospheric load on the chamber, unbalanced pull on any asymmetric iron — and the mean-of-squares point matters wherever the field is nonuniform over the loaded area (pole edges, shim steps).
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The calutron model program's validation verdict — the benchmark for trusting scaled prediction: full-scale tests confirmed the 1/16-scale models as "dependable and accurate," with full-scale performance slightly BETTER than predicted (source-region field more uniform than model results, stray field weaker, track efficiency ~94% vs 95.6 +/- 2% model, core-to-tank field concentration 18% vs model 22%); 71 of 71 production tanks met the theoretical field criteria, worst case 2.8 cm against a 3.0 cm limit.
Source quote & editorial note
The magnetic performance of the track is better than predicted from the model experiment.
Editorial note, tabletop extrapolation: The historical calibration point for a predict-then-verify magnet pipeline: one faithful same-steel scaled-model campaign landed close on global quantities and erred conservative because the prototype's iron out-performed the model's. One campaign is precedent for the METHOD - predict, then verify at full scale - not an accuracy guarantee for models or FEM in general: each pipeline earns its own error bars (dg-080's 3% benchmark, dg-817's first-beam case).
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Members held in place by field symmetry are in unstable equilibrium - anchor them: plant tanks crept as much as 2.5 inches out of their gaps over days of energized operation, and the report's analysis treats the ejection force by reluctance-minimization energy accounting (their computed force bracket: scan re-read queued).
F = d/dx [ (H^2/8pi) * V_field(x) ] ; force increases with displacement from symmetrySource quote & editorial note
It was concluded from these tests that the force on the Alpha tanks tending to push them out of the gaps lies somewhere between 9.71 and 4.53 tons.
Wakerling & Guthrie (eds.), Magnets and Magnetic Measuring Techniques — TID-5215, Radiation Laboratory, University of California (1949) — p. force bracket on PDF 190 (printed p. 180) as cited; the quoted 2.5-in. creep sentence is on PDF 189 (printed p. 179)
Editorial note, tabletop extrapolation: Anything ferromagnetic sitting in or near the gap on nominal-symmetry grounds - chamber, probe carriages, shim plates, tools - needs positive mechanical retention: the destabilizing force is smallest at the symmetric position and grows as the part displaces, which is exactly when it is hardest to stop.
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Use the site as shielding: the UW building was placed to exploit a natural ravine, and the machine sits in a 40-ft-diameter circular room with 10 ft of earth on the perimeter and 24 in of water above the ceiling — earth and water doing what concrete would otherwise cost.
Source quote & editorial note
It is designed so as to take maximum advantage of naturally occurring shielding of a small ravine.
Editorial note, tabletop extrapolation: The siting lesson transfers even if the scale does not: cheap mass - earth berms, water, basement corners - is legitimate shielding MATERIAL for a D-D-capable machine, once treated as engineering rather than slogan: effectiveness depends on composition, thickness, geometry and the capture gammas that moderation produces (hydrogenous media slow neutrons well, then emit 2.2 MeV capture photons), so earth and water get designed and surveyed like any shield (see the shielding deep dive). Spec detail: PDF p.128.
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Specify magnet-core steel chemistry in the purchase order and verify it yourself - the quoted lesson: 'control of the magnetic properties in the manufacture of steel is rather uncertain.' UW's practice per the report: specified maximum chemistry (C 0.15 / Mn 0.5 / P 0.04 / S 0.045 / Si 0.2 per cent, Table A) and a Rowland ring machined from the same heat for a full magnetization curve (procedure detail: scan re-read queued).
Specified max: C 0.15%, Mn 0.5%, P 0.04%, S 0.045%, Si 0.2%Source quote & editorial note
C 0.15 per cent maximum, Mn 0.5, P 0.04, S 0.045, Si 0.2... Rowland ring was machined from... the same heat as the cyclotron magnet.
The University of Washington 60-Inch Cyclotron: Progress and Status Report of Design and Construction — AECU-1951, University of Washington (1951) — p. PDF p.14 (printed p.7), sections 3.1-3.2
Editorial note, tabletop extrapolation: For a next machine's magnet, low-carbon steel chemistry is worth a mill cert, and a sample ring (or bar) from the same stock measured on a cheap B-H rig turns FEMM's material curve from a guess into a measurement. Same measure-your-own-steel discipline as nyo-780.
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State the field-shape requirement as separable specs before shimming - the quoted pair: (1) in the median plane the radial variation must conform closely to a fairly well defined relation, and (2) inside the exit radius the field must be accurately symmetrical (which symmetry planes, and the shimming-campaign details, are the report's: scan re-read queued).
Source quote & editorial note
(1) in the median plane the variation of the intensity with radial distance must conform closely to a fairly well defined relation, and (2) inside the exit radius ... the field must be accurately symmetrical
Editorial note, tabletop extrapolation: DIRECT — the same decomposition (radial law, azimuthal symmetry, median-plane flatness) is how a tabletop field survey should be organized, each with its own instrument and its own fix.
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A scale-model magnet is a close call - UW's experience: the shim testing required was 'much less than anticipated', partly because part geometry 'limited the possible variations more closely than was expected'; their full weighing of the model's advantages and difficulties is the report's own list (scan re-read queued).
Scaling at constant B: J ~ 1/L; heat/volume ~ J^2 ~ 1/L^2Source quote & editorial note
the amount of testing required to arrive at a final shim design was much less than anticipated. This was due in part to the fact that the geometry of parts limited the possible variations more closely than was expected.
Editorial note, tabletop extrapolation: With FEMM the model-magnet role is filled by simulation (ucrl-31 showed the scale-model method itself; MacKenzie AECD-1850 the model-test discipline), but the balanced verdict is the lesson — physical iteration budget should go where the computable model is least trustworthy (saturation, real steel, mechanical tolerances).
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Support model (and real) coils against magnetic forces, not just gravity: UW's model coils, cooled by direct water contact "at the expense of structural support," were distorted when the supporting structure failed "presumably under the magnetic forces," developing shorted turns that dropped the field ~20% below the Rowland-ring prediction. Recovery expedient worth knowing: adding steel around the outer face of the yoke raised the gap field to its proper value "without affecting its shape appreciably."
Source quote & editorial note
the supporting structure for the coils failed, presumably under the magnetic forces. The coils became distorted and short circuits developed.
Editorial note, tabletop extrapolation: DIRECT at any scale: coil-on-coil and coil-on-iron forces scale with NI and B and have crushed amateur windings - brace windings as if they will be pushed, not just held up. (The outer return-path steel in UW's recovery is that machine's expedient; whether added steel raises gap field depends on where the circuit's reluctance actually sits - FEMM answers it.)
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Shim-design criteria worth copying verbatim: (1) inside the exit radius the field as uniform as possible, decreasing no more than ~1% from center; (2) with a central spike, take the center value as the extrapolation ignoring the spike; (3) the decrease must be monotonic; (4) at the exit radius the field index n = -(r/B)(dB/dr) shall be 0.4; (5) exit Br as large as possible consistent with the rest. UW shim space: annular ring against each cover plate, 25.75 in inner radius, 3 in wide, 1 in high; optimum found was a rectangular section equivalent to 5/8 in x 3 in; external shims in the 1/2-in pole-face-to-cover-plate air gaps "were found to have no appreciable added effect."
n = -(r/B)(dB/dr) = 0.4 at exit radius; interior droop <= 1% of centerSource quote & editorial note
at the exit radius the parameter n = - (r/B)(dB/dr) shall have the value 0.4.
Editorial note, tabletop extrapolation: DIRECT as an as-built spec that produced a working field: UW's n = 0.4 exit value and ~1% monotonic interior droop sit in the same territory as this collection's Wouters and Livingston rules. Adopt the criteria's STRUCTURE as a FEMM shim-study objective - uniform interior, monotonic decrease, a defined extrapolation convention, a specified exit index - and set the NUMBERS from the machine's own stability and extraction analysis: 0.4 was their exit choice, not universal physics.
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Magnetic force on ferromagnetic chamber covers inside the gap can exceed the atmospheric load - size the structure for both: UW's model study found the pull on the mild-steel vacuum-tank cover plates exceeded 35 tons against 24 tons of atmospheric force - half again the vacuum load, on that machine.
UW 60-inch: magnetic pull on covers > 35 tons vs atmospheric 24 tonsSource quote & editorial note
the results indicated a force greater than 35 tons for the cyclotron magnet. For comparison the force of atmospheric pressure is 24 tons.
Editorial note, tabletop extrapolation: A ferromagnetic chamber lid or pole-integrated cover sees magnetic clamping of the same ORDER as the vacuum load at tabletop fields (B^2/(2*mu0) vs one atmosphere - dg-177's arithmetic): check deflection in both states (energized and not) and expect assembly/disassembly forces. A non-magnetic lid opts out of the magnetic term entirely.
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Verify the model's prediction on the full magnet before committing to shims: UW's comparison 'showed that the model data could be used as a basis of prediction with confidence' - the quoted conclusion; the measure-reconcile-then-shim sequence is the report's campaign narrative (scan re-read queued).
Source quote & editorial note
showed that the model data could be used as a basis of prediction with confidence.
Editorial note, tabletop extrapolation: The FEMM-era version — survey the bare magnet, reconcile with the simulation, THEN machine shims from the reconciled model. Same model-then-verify discipline as MacKenzie's aecd-1850.
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Choose chamber material for activation, not just vacuum: the UW tank is 2.5-in 61S-T4 aluminum, heliarc (argon TIG) welded, machined in an outside shop — "Aluminum was chosen over stainless steel because of its short half-life property" — and held 2e-6 mm Hg. The steel cover plates were poured from the same heat as the magnet forgings (they are part of the magnetic circuit): 4.5-in plate plus 1-in plate attached by screws.
Source quote & editorial note
Aluminum was chosen over stainless steel because of its short half-life property.
Editorial note, tabletop extrapolation: DIRECT for any machine that will make neutrons: aluminum's dominant activation products are short-lived compared with stainless steel's cobalt-trace Co-60 (years) - the report's reasoning - though aluminum is not activation-proof: fast neutrons make 24Na (15 h) and alloying elements add their own products, so 'short half-life' is comparative, never absolute. Choose the beam-facing metal for the machine you hope it becomes; TIG-welded aluminum is proven UHV-adequate practice from 1951.
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Budget base pressure against interior surface area, and measure your diffusion pump's optimum heater power instead of trusting the nameplate: UW reached 2e-6 mm Hg bare (no traps, no refrigerated baffle); installing the copper liners, RF loops and insulators "approximately tripled the interior surface area" and moved the floor to 4e-6. Pumping-speed measurements set heater inputs at 3100 W (MC-7000, rated 3.5 kW) and 825 W (MB-200, rated 1 kW). Pump-down: 45 min roughing to 50 microns + 10-15 min diffusion to <2e-5; operating pressure 2-4e-5 mm Hg.
Surface x3 -> base pressure x2 (2e-6 -> 4e-6 mm Hg); pumpdown ~1 hr for 4800 L (110 cfm mech + 3500 L/s diff)Source quote & editorial note
Installation of the copper tank liners, R. F. loops and loop insulators approximately tripled the interior surface area
Editorial note, tabletop extrapolation: DIRECT: every liner, loop and insulator added to a chamber is outgassing area, and UW's base pressure roughly doubled when their additions tripled the surface. Base pressure follows total outgassing over delivered speed (P ~ sum(q_i*A_i)/S_eff), so area is the usual driver - materials and cleaning move the q's. The variac experiment (heater power vs measured speed) remains the way to find a surplus diffusion pump's real optimum.
Cited in: The Vacuum Budget of a Cyclotron
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Size oscillator power from Q and dee reactance before choosing a tube, then add margin for what the analysis cannot know: UW measured/computed system Q ~ 7500 (line alone ~11,000 before dee and joint losses), dee capacitive reactance X ~ 40 ohms, so 160 kV peak gap needs ~21.2 kW and 250 kV needs ~52 kW; 150 kW was selected as the provided maximum "upon considering the approximations necessarily made in this type of analysis" (150 kW would drive ~450 kV — above what the dees could stand — so the margin is real headroom, not a target). Dees, stems, liner and supply components were all rated to the 150 kW figure, and the tube chosen to survive dee arcs.
P = Epk^2/(4*Q*X); 21.2 kW @ 160 kV, 52 kW @ 250 kV for Q=7500, X=40 ohmSource quote & editorial note
upon considering the approximations necessarily made in this type of analysis, the figure of 150 kw maximum r-f power was selected.
Editorial note, tabletop extrapolation: DIRECT scaling method for the LDMOS upgrade: measure the dee system's Q and C, compute watts per kV from P = V^2/(4QX) (equivalently V^2/(2*R_shunt)), then add margin for what the lumped model misses - beam loading, coupling loss, arcs, duty cycle. UW's own practice sized 150 kW against a ~52 kW computed requirement, roughly 3x, 'upon considering the approximations'; let your margin come from your own unknowns inventory, with theirs as the precedent.
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A two-dee system has two coupled modes - a zero mode with the dees swinging in phase (no accelerating gap voltage) and a pi mode swinging opposite (gap voltage present) - and the oscillator coupling must select the pi mode: the quote records UW choosing the drive method easiest to hold at 180 degrees. Mode spacing depends on the coupling geometry.
Source quote & editorial note
This method should be easiest of the methods used to assure oscillation at the proper frequency with the dees operating 180 degrees out of phase.
Editorial note, tabletop extrapolation: For a one-dee-plus-dummy machine the mode problem collapses. For any driven system, verify which resonance the amplifier locks to - a network-analyzer sweep plus a phase comparison between dee pickups distinguishes the modes - because the wrong one accelerates nothing.
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Plan the multipactor climb-through at design time: UW knew that 'electron oscillations in the vicinity of the dees and dee stems at low r-f voltages tend to absorb energy and prevent the oscillations from building up' - and designed for it; their booster/driver arrangement is the report's implementation (topology, rating and isolation details: scan re-read queued).
Source quote & editorial note
Electron oscillations in the vicinity of the dees and dee stems at low r-f voltages tend to absorb energy and prevent the oscillations from building up.
Editorial note, tabletop extrapolation: The corpus's driven-start cure (mddc-1045 tickler; nyo-9359's catalogue) as a 1951 DESIGN feature rather than a retrofit, including the half-frequency/doubler isolation trick that spares a changeover switch. Directly relevant to the reference machine's dee-voltage buildup pathology: any LDMOS drive chain is inherently a driven start, but only if it can push watts through the multipactor loading band without foldback or protection tripping - and that band's voltage is geometry-, frequency-, pressure- and surface-dependent, so measure it on the actual dee. [Note revised 2026-08-23: the earlier note quoted '~100 V' for the band as if it were a design constant.]
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Model the RF system at reduced scale before building it: UW's quarter-scale model of the resonant system was the answer to 'many uncertainties in the exact determination of the constants of the equivalent circuit' - calculated values 'serve well as a guide', and the model settles them (the model's dimensions, Q and adjustment history: scan re-read queued).
Source quote & editorial note
there are many uncertainties in the exact determination of the constants of the equivalent circuit ... the calculated values ... serve well as a guide
Editorial note, tabletop extrapolation: A tabletop resonator IS the scale model — build the dee/stem mockup on the bench, measure f and Q before committing to vacuum hardware, and trust lumped calculations as guides not gospel. Berkeley used the same quarter-scale method on the 88-inch (ucrl-9435), which also confirms the Q-degradation-at-joints lesson (ornl-2648).
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Sequence deflector fabrication behind first internal beam: UW completed the deflector's preliminary design but scheduled that "machining work will begin after the oscillator is operating and an internal beam produced" — the probe (water-cooled internal target, 10-25 in radius by remote control, through its own vacuum lock) comes first, because internal beam data retire more risk than a finished deflector does.
Source quote & editorial note
Machining work will begin after the oscillator is operating and an internal beam produced.
Editorial note, tabletop extrapolation: The commissioning-order lesson as an explicit 1951 schedule decision: internal beam first, extraction hardware behind it. A sensible default for a next machine - the probe and its lock as first-beam hardware, extraction machining held until the internal beam teaches you the real orbit - a default, not a law.
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Cyclotron RF differs from industrial RF in ways to design for from day one - the report's headline differences: (a) the resonator is a sparking load that can deliver large energy into the electronics; (b) multipactoring, 'common in the field of particle accelerators, rarely occurs in other industrial applications' (the quoted item); (c) frequency agility where the machine class needs it.
Source quote & editorial note
(b) the multipactoring problem, common in the field of particle accelerators, rarely occurs in other industrial applications
Editorial note, tabletop extrapolation: The checklist for adapting any industrial or ham RF gear (an LDMOS pallet included) to a cyclotron: add spark protection, add a multipactor start plan, and only then worry about power. Fixed-frequency tabletop machines are spared only (c).
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Multipactor physics in one sentence pair: electrons in the dee-ground gap whose transit time is half the RF period multiply when the secondary-emission ratio exceeds unity — "The threshold of secondary emission is about 150 electron volts for most surfaces; consequently, multipactoring becomes possible when the voltage across the dees reaches this value." One standard cure on the 88-inch: a dc sweeping field superimposed across the RF gap to pull electrons out faster than they multiply.
multipactor onset near the secondary-emission threshold (~150 eV -> ~150 V-class gap voltages) WHERE a resonant transit condition also holds; band edges move with gap, frequency and surface yieldsSource quote & editorial note
The threshold of secondary emission is about 150 electron volts for most surfaces; consequently, multipactoring becomes possible when the voltage across the dees reaches this value.
Editorial note, tabletop extrapolation: DIRECT: a small machine's dee voltage passes through the ~100-150 V-class region on every start - whether multipactor actually lights there depends on the gap-frequency resonance and the surfaces' secondary yields, which is why some machines never see it. Completes this collection's cure set: mddc-1045 (bias + tickler), nyo-9359 (impulse start), ucrl-64 (volume reduction + bias).
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Every dee spark is a system-wide transient that can trigger a spark inside the oscillator tube and divert the full dc supply as a power arc - so protection is layered by speed: Berkeley's hard-tube series switch opens the anode circuit within 10 microseconds of a fault (the quoted spec), with slower switch layers behind it (their arrangement: scan re-read queued).
Protection ladder: hard-tube series switch ~10 us; ac vacuum switches ~10 ms; (alternative: ignitron crowbar)Source quote & editorial note
Vacuum switches connected in the three-phase, 16.6 kv ac lines feeding the rectifier ... open within 10 msec plus the time to the first current zero ... In this service it will open the anode circuit within 10 usec of a fault.
Smith, The RCA 6949 as a Self-Excited Cyclotron Oscillator — UCRL-9435, Lawrence Radiation Laboratory (1960) — p. PDF p. 6 (printed -6-) for the layer arrangement; PDF p. 7 (printed -7-) for the regulation and termination items
Editorial note, tabletop extrapolation: The modern translation, mapped by FUNCTION rather than spec-for-spec: an LDMOS drain supply wants a fast electronic disconnect (the hard-tube modulator's descendant), a slower breaker layer, and snubbing on the dc feed - each layer rated against the actual stored energies and fault modes of the build (dg-330, dg-679, dg-1371).
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THE SELF-EXCITED POSITION (design tension with the MOPA position of ornl-2403): Smith's 88-inch runs the resonator as the frequency-determining element - 'hence it is called a self-excited oscillator' - with the report's implementation figures (AFC, regulation) as its own record (scan re-read queued for those numbers).
Source quote & editorial note
In this type of system the resonator is the frequency-determining element of the system; hence it is called a self-excited oscillator.
Editorial note, tabletop extrapolation: The live architecture decision for a next machine. An LDMOS chain driven by a synthesizer is a MOPA — it inherits ornl-2403's virtues (frequency authority, instrumentation) AND the self-excited literature's start-up disease (nyo-9359): the synthesizer holds frequency while multipactor holds the dee at zero. Smith's phase-discipline logic (feedback phase correct across the whole operating range) is the checklist item either way. High-SWR argument p.6.
Cited in: Driving the Dee: RF Coupling
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Budget resonator power in four named parts, and the beam is not negligible: for the 88-inch at 70 kV dee — RF skin losses 121 kW (computed several ways from the measured voltage/current distribution of the resonator), stray-ion loss at the machine center ~30 kW at maximum energy, beam power 60 kW (1 mA at 60 MeV), miscellaneous (couplings, harmonics radiated into the tank) ~10 kW; total 221 kW, so 300 kW was provided. A corrugated dee stem (longitudinal corrugations increase skin perimeter) cut current density enough to save ~70 kW of the copper loss.
P_total = P_skin + P_stray-ion + P_beam + P_misc; 88-inch @ 70 kV: 121 + 30 + 60 + 10 = 221 kW -> 300 kW installedSource quote & editorial note
At the maximum particle energy, the beam requires 60 kw of power.
Editorial note, tabletop extrapolation: The four-line budget is the right form at any scale. A tabletop version: watts of copper loss (dg-313), a beam line computed from ITS current and energy - 1 nA at 500 keV is 0.5 mW, 10 uA at 1 MeV is 10 W, small only until the source improves - a stray-ion line that follows source gas and RF (measurable as the loading difference with the source on vs off), and a misc line that is mostly coupling and radiation.
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Choose oscillator/amplifier tubes for spark survival, not just gain: sparks dump joules into "an area determined by the cross section of the spark," and conventional squirrel-cage grids of very light wire get blasted through, shorting grid to cathode. "For accelerator applications, a tube should have a sufficiently heavy grid to absorb several joules of energy" — the 6949's heavy grid bars hide behind massive copper shield tees "almost immune to spark damage," and its high power sensitivity (3 kW drive for 319 kW out) shrinks the grid line and allows a large safety factor in the grid vacuum insulator.
Source quote & editorial note
For accelerator applications, a tube should have a sufficiently heavy grid to absorb several joules of energy in an area determined by the cross section of the spark.
Editorial note, tabletop extrapolation: The solid-state translation: LDMOS devices have finite ESD, avalanche and mismatch ratings rather than a tube grid's joules of thermal mass, so the ruggedness must live in the coupling network - series blocking, clamping, fast drive-cut (dg-338, dg-758). A dee-side fault arrives first at the OUTPUT network, which is where the protection belongs.
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Before dimensioning anything, draw the dependency diagram of the five subsystems (magnet, acceleration, ion, vacuum, detector) and separate the given inputs (pole radius, maximum orbit radius, nominal pumping speed, flux density, pole gap, gap width, dee amplitude, specific charge) from the quantities calculated from them (cyclotron frequency, rigidity, final velocity and energy, first-orbit radius and velocity, number of accelerations, total path length, effective pumping speed, mean free path, final pressure, permissible gas load).
Source quote & editorial note
Bevor man an den Nachbau eines Zyklotrons geht, muss man sich darüber im Klaren sein, was man benötigt. ... Bei den fünf Teilsystemen handelt es sich im einzelnen um das Magnet-System, das das Führungsfeld liefert, das Beschleunigungs-System, das für die Hochspannung sorgt, das Ionen-System, verantwortlich für die Produktion der Ionen, das Vakuum-System, das das erforderliche Vakuum zur Verfügung stellt, und schließlich das Detektor-System, das die beschleunigten Teilchen registriert. ... Die Vorgaben in den grünen Kreisen sind zum einen gerätespezifische Größen. Dazu gehören: der Radius der Magnetpole rp und der maximale Bahnradius ... das Nenn-Saugvermögen SN des Pumpstands [tr.: before building a cyclotron one must be clear what is needed; the five subsystems are the magnet system supplying the guide field, the acceleration system providing the high voltage, the ion system producing the ions, the vacuum system, and the detector system registering the accelerated particles; the givens in the green circles are device-specific quantities - the pole radius, the maximum orbit radius, the pump stand's nominal pumping speed - the calculated quantities in blue circles]
Editorial note, tabletop extrapolation: A small machine has few free parameters; listing which are fixed by hardware (pole radius, pump) and which are design choices (B, gap, U0, species) keeps the sizing chain consistent and exposes circular dependencies early.
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A worked magnet-selection step: a rigidity of 0.040 T m yields about 76 keV protons or 38 keV H2+ (v ~ 3.8e6 and 1.9e6 m/s); on the B-rho chart that is met by, for example, 1.0 T with a pole radius of at least 40 mm, so read the required (B, rho) pair off a constant-rigidity curve before shopping for a magnet.
B*rho = const ; rho_min = zeta/BSource quote & editorial note
Beträgt die Steifigkeit etwa 0,040 Tm, so liest man ab, dass die maximale Energie von Protonen ca. 76 keV [tr.: at 0.040 T m protons reach about 76 keV]
Editorial note, tabletop extrapolation: Recomputed and correct: 0.040 T m gives ~76.6 keV protons; the same chart logic at 0.06 T m (0.6 T, 10 cm) gives ~172 keV. Read the geometry carefully: 1.0 T with a 40 mm orbit needs 40 mm of USABLE-FIELD radius - the physical pole must be larger, by the fringe margin the field map shows (dg-1382). Scale energy targets from rigidity, not from voltage.
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COLUMBUS's practice for its borrowed laboratory magnet: run continuously at no more than half the MAXIMUM coil current to avoid overloading it, and pick the operating field where the data-sheet homogeneity is best rather than where the field is highest.
Source quote & editorial note
Um den Magneten nicht zu überlasten, sollte er im Dauerbetrieb höchstens mit der Hälfte des maximalen Spulenstroms betrieben werden [tr.: run at no more than half the maximum coil current in continuous duty]
Editorial note, tabletop extrapolation: For any other borrowed or surplus magnet, use its actual continuous-duty specification (maximum and continuous ratings differ) and verify winding temperature under your duty cycle - half-of-maximum is this book's conservative default when no continuous rating is known. The choose-field-by-homogeneity move transfers as stated; record the chosen point as a thermal/homogeneity compromise, not a hard limit.
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Read the magnet radial-homogeneity curve at the intended extraction radius and express it relative to B0: a laboratory magnet with 150 mm poles at a 75 mm gap shows at most 0.02 percent deviation at r = 70 mm for all three plotted central fields, so a plain flat-pole magnet of that class is homogeneous enough for a few-keV teaching machine without shimming.
dB/B0 at r = rhoSource quote & editorial note
Bei allen drei zentralen Feldstärken beträgt die relative Inhomogenität bei r = 70 mm maximal nur 0,02 % bzgl. B0 [tr.: at r = 70 mm the inhomogeneity is at most 0.02 percent of B0]
Editorial note, tabletop extrapolation: The 0.02% figure is a commercial NMR-class magnet's vendor-chart datum at gap/pole-ratio 0.5 - a CANDIDATE uniformity level: check its adequacy against your machine's allowable cumulative phase slip and turn count, and confirm with a two-dimensional map (radial AND azimuthal) before concluding no shimming is needed; a home H-frame with a tighter gap will differ in both directions.
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The pole gap equals the chamber height plus the walls, so let the lid do double duty: COLUMBUS mills a 150 mm diameter, 12 mm deep recess into the chamber lid, lowers the upper pole into it - giving the chamber a fixed seat in the magnet - and houses the Hall probe in the recess; the chamber height dropped to ~72 mm and the minimum pole spacing to ~75 mm.
delta_z = h_chamber_internal + t_base + t_lid_remainingSource quote & editorial note
In den Deckel ist eine Vertiefung mit einem Durchmesser von 150 mm und einer Tiefe von 12 mm eingefräst. Dort befindet sich eine Hallsonde für die Messung der magn. Flussdichte. In diese Vertiefung wird der obere Pol des Magneten abgesenkt; so erhält die Kammer im Magneten einen festen Sitz. Außerdem konnte dadurch die Kammerhöhe auf ca. 72 mm verringert werden. Unter Berücksichtigung der Materialstärke beträgt der minimale Polabstand des Magneten schließlich ca. 75 mm. [tr.: a 150 mm diameter, 12 mm deep recess is milled into the lid. A Hall probe for measuring the flux density sits there. The upper pole of the magnet is lowered into this recess, giving the chamber a fixed seat in the magnet; the chamber height could thereby be reduced to ~72 mm, and allowing for material thickness the minimum pole spacing is finally ~75 mm]
Editorial note, tabletop extrapolation: Every millimetre of gap costs ampere-turns; the recessed-lid trick keeps the poles within a few mm of the dee envelope while fixing the chamber and giving the field probe a home. Size the recess floor (and any thin base) by an actual vacuum-vessel calculation - plate deflection and buckling for the real material and span - not by copying this machine's dimensions; and note the probe reads the field at the recess, not the median plane, so calibrate the offset.
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Keep the maximum orbit radius a few millimetres inside the pole radius: with 150 mm poles the dee inside diameter was 140 mm, so rho = 70 mm is 5 mm short of the pole edge where the field starts to fall.
rho = r_pole - 5 mm (reference machine)Source quote & editorial note
Da der Innendurchmesser des Dees 140 mm beträgt, hat ρ den Wert 70 mm und ist damit um 5 mm kleiner als der Polradius [tr.: dee ID 140 mm, rho 70 mm, 5 mm less than pole radius]
Editorial note, tabletop extrapolation: Treat the 5 mm as this machine's geometric margin, not a rule: COLUMBUS runs a very LARGE gap-to-diameter ratio (75/150 = 0.5), so its field is far from flat at the edge anyway and the machine needs no extraction. For a 20 cm pole with a 2-3 cm gap the ratio is much smaller and the flat region proportionally wider - but the usable radius still comes from a measured or FEMM field map plus orbit-excursion and clearance checks, not from a fixed edge offset.
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When both H+ and H2+ are present, COLUMBUS plans the RF so both species come into resonance by changing the FIELD rather than the frequency - at fixed 2.82 MHz, protons resonate near 185 mT and H2+ near 370 mT - the book judging it easier to double the field than the frequency.
f_cyc = (q/m)*B/(2*pi) ; H2+ needs 2*B of H+ at the same fSource quote & editorial note
Es ist nämlich leichter, das Magnetfeld von 185 mT auf 370 mT zu erhöhen als die Frequenz von 2,82 MHz auf 5,64 MHz [tr.: easier to raise B from 185 to 370 mT than f from 2.82 to 5.64 MHz]
Editorial note, tabletop extrapolation: A fixed-frequency resonator plus a 2:1 field range covers both hydrogen species IF the machine works at both fields - field quality, source output and capture must each hold at both points, so verify rather than assume. Two peaks at B and 2B are consistent with H+/H2+ but not unique to them (q/m degeneracy, dg-1432); use them as a species INDICATION to confirm.
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Bound the dee amplitude from above by the actual weakest insulator: on COLUMBUS the vacuum feedthrough's voltage rating limited U0 to <= 3000 V, and the matchbox output was designed to that bound.
U0_max = feedthrough ratingSource quote & editorial note
Aus Gründen der Spannungsfestigkeit der Durchführung ist U0 ≤ 3000 V [tr.: because of the feedthrough voltage rating, U0 <= 3000 V]
Editorial note, tabletop extrapolation: A 5-15 kV dee upgrade is an insulation-coordination problem across the WHOLE RF path - feedthrough, stem supports, matching capacitors, connectors, plus contamination and conditioning state - with the feedthrough a frequent but not guaranteed weakest link. Specify every element for peak RF plus any DC bias, in vacuum, with tracking margin.
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Measure the dee input impedance before designing the RF chain: COLUMBUS's dee-plus-stem measured about 330 kOhm - and if that is the resonant parallel loss resistance, the acceleration power is tiny: P = U0^2/(2*R_p) = 6 W at 2 kV peak.
P = U0^2/(2*R_p) for U0 peak and R_p the resonant parallel loss resistance; at 10 kV into 330 kOhm, ~150 WSource quote & editorial note
Diese beträgt nach aktuellen Messungen ca. 330 kΩ [tr.: according to current measurements this is about 330 kOhm]
Editorial note, tabletop extrapolation: The scaling explains why a 100-500 W amplifier class suits a 5-13 kV dee - sized with margin: P_source >= U0^2/(2*R_p*eta) with measured end-to-end efficiency eta (matchbox, feedline and base-load losses all sit between amplifier and dee), and the larger dee's own R_p measured, not borrowed from this machine.
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A marine HF transceiver is a workable multi-MHz RF source for a teaching cyclotron: COLUMBUS uses an ICOM M 600, delivering in H3E (AM carrier) mode a sine of ~70 V amplitude over 0.5-35 MHz, about 45 W into 50 ohm; such transmitters shut down without a load, so the matchbox input presents a resistive base load.
Source quote & editorial note
Der verwendete Transceiver, ein ICOM M 600, liefert in der Betriebsart H3E eine sinusförmige Spannung (Amplitude ≈ 70 V) im Frequenzbereich von 0,5–35 MHz mit einer abgegebenen Leistung von ungefähr 45 W an 50 Ω Ausgangsimpedanz. ... Das Widerstandsnetzwerk der Eingangsstufe stellt dabei eine Grundlast für den Transceiver dar. Dieser würde sonst [...] abschalten [tr.: the transceiver used, an ICOM M 600, delivers in H3E mode a sinusoidal voltage (amplitude ~70 V) over 0.5-35 MHz with about 45 W into 50 ohm output impedance ... the input resistor network is a base load; otherwise the transceiver shuts down]
Editorial note, tabletop extrapolation: The load-requirement lesson generalizes as a check, not a law: characterize the chosen amplifier's required load, mismatch tolerance and protection behavior (an LDMOS deck without foldback dies where the ICOM merely shuts down), and budget a dummy-load fraction plus a VSWR interlock so a detuned dee - a plasma flash, say - cannot damage the final stage.
-
With a single-ended drive, the book's design shortens the grounded electrode into a dummy dee - since it sits at chamber potential, the region behind it is already field-free; the hot dee keeps its full depth.
ideal peak gap voltage: U0 (grounded counter-electrode) vs 2*U0 (opposite-phase push-pull at the same per-electrode amplitude U0)Source quote & editorial note
Da ein Dee wie die Vakuumkammer selbst auf Masse liegt, kann dieses Dee verkürzt werden [tr.: since one dee is at ground like the chamber, it can be shortened]
Editorial note, tabletop extrapolation: Single-dee-plus-dummy gives half the energy gain per turn of an ideal push-pull pair at the same per-electrode amplitude, in exchange for one feedthrough and one resonator - a trade that favors simplicity on most small builds; state the amplitude convention whenever quoting the factor of two.
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COLUMBUS chose the accelerating gap and the dummy-dee depth as one common dimension - 20 mm each, 'on plausibility grounds' - the book posing the two dimensions as a single question when dimensioning the dummy dee.
gap = dummy-dee depth = dee aperture height = 20 mmSource quote & editorial note
Bei der Dimensionierung des Dummy-Dees stellt sich natürlich die Frage nach der Tiefe und der Größe des Beschleunigungsspalts gap. Aus Plausibilitätsgründen wurde jeweils ein Maß von 20 mm gewählt. [tr.: in dimensioning the dummy dee the question arises of its depth and the size of the accelerating gap; on plausibility grounds 20 mm was chosen for each]
Editorial note, tabletop extrapolation: A wide gap simplifies the source mount (the chimney sits inside it) at the cost of transit-time factor; choose the gap from the transit calculation - T = sin(x)/x with x = omega*g/(2v) over the actual injection and orbit velocities - rather than adopting either 20 mm or any other fixed number.
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Size the vacuum from the mean free path: l = k_B*T/(p*sigma) with sigma = pi*(R1+R2)^2 - the book's hard-sphere table for hydrogen ions in NITROGEN, e.g. H2+ going more than 123 m between collisions at 1e-6 mbar, scaling inversely with pressure.
l_bar = k_B*T/(p*sigma) ; sigma = pi*(R1+R2)^2Source quote & editorial note
Bei einem Druck von p = 10−6 mbar [...] würden die H2+-Ionen (im Mittel) also erst nach mehr als 123 m auf ein Stickstoff-Molekül treffen [tr.: at 1e-6 mbar H2+ travels more than 123 m between collisions]
Editorial note, tabletop extrapolation: The table is a historical order-of-magnitude estimate with two labeled limitations: a hydrogen-FED machine's residual gas is mostly H2 (measure it - an RGA settles it), and the loss process that matters for beam survival is charge exchange, whose energy-dependent cross-section must come from evaluated data (dg-460), not hard spheres. Use lambda_loss(E) = 1/sum_j n_j*sigma_loss,j(E) over the actual partial pressures.
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The book's worked vacuum trade for a 16 keV H2+ target at 4e-5 mbar (l ~ 3 m): 2000 V needs 8 crossings, 1000 V needs 16 crossings and 2.76 m of path, 'barely reached with 3 m'; below that the criterion fails before full energy. This is the source's attenuation CRITERION, not a hard reachability wall - at s = lambda the uncollided fraction is ~37%, and survival falls smoothly, so read the table as a loss budget.
k = E/(q*U0); s_ges(k) vs l_bar(p); survival = exp(-s/lambda) for constant lambda. Recomputed: r1 = 17.5 mm, sum sqrt(i) i=1..16 = 44.47 -> 2.45 m arcs + 0.32 m gaps = 2.76 m; at 2000 V the same geometry gives ~1.27 m arcs + 0.16 m gaps = ~1.43 m total. Caution: the bitmap Table 6.2 lists 2.44 m and 1.27 m - arcs only, without the k*gap term; use the text figure.Source quote & editorial note
Für 16 Beschleunigungen wären 2,76 m Weglänge erforderlich, die mit 3 m knapp erreicht werden [tr.: 16 accelerations need 2.76 m of path, barely reached with 3 m]
Editorial note, tabletop extrapolation: Recomputed: r1 = 17.5 mm, sum sqrt(i) for i=1..16 = 44.47, giving 2.45 m of arcs plus 16*0.02 = 0.32 m of gap = 2.76 m. Caution: the bitmap Table 6.2 lists 2.44 m and 1.27 m, i.e. arcs only without the k*gap term; use the text figure.
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Steady-state chamber pressure under deliberate gas feed follows from the pV-flow balance: p_E = q_G/S_eff - COLUMBUS's worked point, 300 mbar inlet at ~0.14 ml/min actual flow = 7.0e-4 mbar*l/s, over S_eff = 17.2 l/s, giving 4.1e-5 mbar against the measured 4.0e-5.
p = (q_process + q_background)/S_eff; q_process = p_inlet*Q_actual (actual volumetric flow) or p_std*Q_std (sccm-reading MFC) - one convention consistently; background = leaks + desorption, measured with feed offSource quote & editorial note
für einen Volumenstrom von ca. 0,14 ml/min sich ein Enddruck pE = 4,0 · 10−5 mbar einstellt [tr.: at about 0.14 ml/min a final pressure of 4.0e-5 mbar establishes itself]
Editorial note, tabletop extrapolation: The one-line balance is the first thing to validate against the gauge on a new machine - at several MFC settings, with the background term measured separately (feed off) and the flow convention of the actual controller pinned down before trusting any prediction.
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Never size from nominal pumping speed: 1/S_eff = 1/S_N + 1/G_L. COLUMBUS's 28 l/s (H2) turbo behind a 0.615 m DN40 line (G_L = 44.3 l/s for H2) delivers 17.2 l/s at the chamber - a 39% loss; for nitrogen (35 l/s nominal, G_L = 11.8 l/s) the loss is ~75%.
1/S_eff = 1/S_N + 1/G_LSource quote & editorial note
Allerdings darf für S nicht das Nennsaugvermögen SN = 28 l/s der Turbomolekularpumpe für Wasserstoff angesetzt werden [tr.: the nominal 28 l/s hydrogen speed of the turbo must not be used for S]
Prechtl & Wolf, Das Lehr-Zyklotron COLUMBUS — Mit einem Teilchenbeschleuniger Physik und Technik erleben, Springer (2020) — p. 52, 82-83
Editorial note, tabletop extrapolation: The lesson is the calculation, not a flange size: compute each line's conductance for each gas that matters and pick the port from the required chamber speed - short and fat wins, and mounting the pump directly on the chamber removes the term entirely. The 39/75% figures are this installation's; other lines and gases differ.
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Use the long-tube molecular-flow conductance G_L = (pi/12)*v_bar*D^3/L (valid for Knudsen number l/D >= 10 and L/D >> 1), obtained from the aperture conductance (pi/16)*v_bar*D^2 times the transmission probability (4/3)*D/L; v_bar is the mean thermal speed of the actual gas.
G_L = (pi/12)*v_bar*D^3/L; G_aperture = (pi/16)*v_bar*D^2; P_R = (4/3)*D/L; short tubes: C ~ [1/C_aperture + 1/C_long]^-1 or a Clausing factorSource quote & editorial note
Damit erhält man letztlich als Berechnungsformel für den Rohr-Strömungsleitwert: GL = π/12 v̄ D³/L [tr.: the working formula for tube conductance]
Editorial note, tabletop extrapolation: The D^3 dependence means a DN63 line has ~4x the conductance of DN40 at the same length (compute from actual bores - DN designations don't fix the ID). For short stubs (L/D < 10) the long-tube limit OVER-predicts - it diverges as L -> 0 - so cap it with the aperture term via the series combination.
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Design the pumping chain for hydrogen, not air, when hydrogen is the feed: during source operation it is essentially only hydrogen being pumped - and the turbo's hydrogen speed (28 vs 35 l/s nominal here) and the line's hydrogen conductance (3.7x the air value) both differ from the air numbers.
v_bar = sqrt(8*R*T/(pi*M)) ; H2: 1.75 km/s, N2: 0.469 km/s at 293 KSource quote & editorial note
Dabei ist noch zu berücksichtigen, dass jetzt nicht mehr Luft, sondern im wesentlichen nur noch Wasserstoff H2 abgepumpt wird [tr.: it is now essentially only hydrogen that is pumped]
Editorial note, tabletop extrapolation: Take the H2 column from the pump datasheet and compute conductances with hydrogen's v_bar (1.75 km/s at 293 K vs 0.469 for N2). Terminology discipline: BASE pressure is the no-feed number; during source operation the relevant quantities are OPERATING pressure and residual composition - hydrogen-dominated when the feed throughput exceeds the measured background load.
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COLUMBUS's two-stage pumping: an oil-free diaphragm backing pump takes the chamber from atmosphere to the ~1e-2 mbar class, where the turbomolecular pump takes over for the molecular regime - the book noting the backing pump can go no lower and the turbo continues from there.
Source quote & editorial note
Nun lässt sich mit der Vorpumpe der Druck nicht weiter erniedrigen. Die weitere Druckreduzierung erfolgt jetzt durch die Turbomolekularpumpe [tr.: the backing pump can go no lower; the turbo takes over]
Editorial note, tabletop extrapolation: The two-stage division of labor is standard but its numbers are technology-specific: take the crossover pressure and backing requirement from the high-vacuum pump's own specification (turbo, diffusion, cryo all differ - a diffusion stage wants a rotary-vane backer and a trap or baffle). An oil-free diaphragm backer keeps hydrocarbons out and is classroom-quiet - this machine's genuine transferables.
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Hydrogen is the natural feed for a small machine: it ionises easily by electron impact, a 10 L / 10 bar disposable Hydrostick cartridge holds a small, cheap inventory, and both H+ and H2+ are produced. Its drawback, per the book, is relatively high permeation through hoses and cannulas, which particularly affects the ion source.
Source quote & editorial note
Ein Nachteil ist die relativ hohe Permeation von Wasserstoff durch Schläuche und Kanülen; dies betrifft insbesondere die Ionenquelle [tr.: a drawback is hydrogen permeation through hoses and cannulas]
Editorial note, tabletop extrapolation: Use metal lines with a mass-flow controller rather than elastomer tubing (PEEK is lower-permeation than elastomers, not zero). A small cartridge is still HYDROGEN: even ~10 standard litres forms a flammable mixture in air, so ventilate, leak-check, control ignition sources and handle the pressurized cartridge properly. Runtime: compute from the cartridge's usable standard volume at the actual MFC setting rather than quoting a lifetime.
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Gas-feed chain for a thermionic source, as built: cartridge -> pressure reducer to 300 mbar -> mass-flow controller at 0.10-0.20 ml/min -> directly into the source chimney; the reducer pressure enters the book's gas-load balance q_G = 300 mbar * V_dot_G, with V_dot the ACTUAL volumetric flow at the reducer pressure.
q = p_in * Q_actual (actual inlet volume) or q = p_std * Q_std for an MFC reading sccm - one convention, consistently; mixing 300 mbar with an sccm reading understates throughput ~3.4xSource quote & editorial note
Dieser Druck wird durch einen Druckminderer auf pH2 = 300 mbar reduziert [tr.: the pressure is reduced by a regulator to 300 mbar]
Editorial note, tabletop extrapolation: Fix the reducer pressure and log it - it is a term in the balance. Whatever meters the flow, state its reference conditions and take accuracy and repeatability from its specification rather than assuming a resolution.
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Run the source anode near the book's stated ion-yield maximum: it reports the number of ions formed peaking at 100-150 eV electron energy - beyond that interval the electrons are 'quasi too fast' and the rate falls - so the anode voltage is set to ~120-150 V. [Note: standard evaluated H2 electron-impact ionisation data put the broad maximum nearer 70-100 eV; the book's 100-150 eV band reads as its source's empirical optimum, which also folds in geometry and sheath effects.]
U_B = 100-150 VSource quote & editorial note
Die Anzahl der gebildeten Ionen hängt aber auch von der Elektronenenergie ab. Sie erreicht bei 100–150 eV ein Maximum [tr.: ion yield depends on electron energy, peaking at 100-150 eV]
Editorial note, tabletop extrapolation: Sweep anode voltage against extracted ion current on the actual source - the optimum is broad and machine-specific, anode volts are not electron collision energy volt-for-volt (sheaths and where ionisation happens intervene), and a current-limited 0-200 V supply covers the whole plausible band.
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Estimate source output from I_ion = sigma * I_e * l_e * p_H with sigma the differential ionisation coefficient (order 1-3 per cm*mbar for hydrogen), I_e the emission current, l_e the electron path, p_H the local hydrogen pressure - a first-order production estimate, not a bound.
I_ion = sigma * I_e * l_e * p_H ; sigma ~ 1-3 /(cm*mbar)Source quote & editorial note
Der differentielle Ionisierungswirkungsquerschnitt σ liegt in der Größenordnung von 1–3 1/(cm·mbar) [tr.: the differential ionisation coefficient is of order 1-3 per cm mbar]
Editorial note, tabletop extrapolation: Compare with measurement honestly: at 2-5 mA emission the sigma=1 estimate gives ~0.3-0.7 uA against measured 1-3 uA - a factor of a few, not an order of magnitude, and the gap closes further once the CHIMNEY pressure (well above chamber pressure) and the sigma range are used. The formula omits extraction efficiency and losses in both directions - calibrate it per source rather than reading it as floor or ceiling.
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Extraction geometry for a chimney source in a single-dee machine: a narrow slit on the chimney side facing the dee, two puller electrodes attached to the dee, ions leaving on the negative half-wave only. No counter-beam forms on the positive half-wave because the chimney sits at dummy-dee (ground) potential and has no slit facing the dummy dee.
Source quote & editorial note
Zu diesem Zweck wurden an dem Dee zwei Extraktions- bzw. Pullerelektroden angebracht. Nun bleibt noch die eingangs gestellte Frage zu klären, warum kein zweiter Ionenstrahl während der positiven Halbwelle entsteht. Ein Grund dafür ist die Tatsache, dass die Ionen nur aus dem Schlitz extrahiert werden können, der dem Dee gegenüberliegt. Ein weiterer Grund ist das Potenzial des Kamins, das das gleiche ist wie das des Dummy-Dees, nämlich Masse. Somit könnten auch während der positiven Halbwelle der Beschleunigungsspannung keine Ionen in das Dummy-Dee extrahiert werden. [tr.: two extraction/puller electrodes were fitted to the dee; the question why no second ion beam forms during the positive half-wave is answered by two reasons - ions can only leave through the slit facing the dee, and the chimney sits at the same potential as the dummy dee, namely ground, so no ions can be extracted into the dummy dee during the positive half-wave]
Editorial note, tabletop extrapolation: Grounding the chimney with a one-sided slit answers the reverse-beam question students raise - by construction on this machine. If the source is biased instead, the slit-to-puller spacing, the bias polarity and the counter-beam question all reopen: analyze, don't assume.
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Water-cool a kW-class laboratory magnet with a closed loop, as COLUMBUS's student-built system does: a central-heating circulator providing ~10 l/min, an expansion vessel holding ~1 bar operating pressure, and a cooling-failure interlock that switches the magnet off via an emergency switch.
Source quote & editorial note
Im Betrieb müssen die Spulen des Magneten mit Wasser gekühlt werden. Dies geschieht durch ein (von Schülern selbst entwickeltes) Kühlsystem, das mit Hilfe einer Heizungspumpe für den notwendigen Durchfluss von ca. 10 l/min sorgt. Ein Druckausgleichsgefäß stellt den notwendigen Betriebsdruck von ca. 1 bar während des Betriebs her. Sollte das Kühlsystem einmal ausfallen, so wird der Magnet über einen Notschalter abgeschaltet. [tr.: in operation the magnet coils must be water-cooled, by a student-built cooling system whose central-heating circulator provides the necessary ~10 l/min flow; an expansion vessel maintains the ~1 bar operating pressure; should the cooling fail, the magnet is switched off by an emergency switch]
Editorial note, tabletop extrapolation: Size cooling from the measured coil loss, allowable winding temperature and coolant temperature rise - the 10 l/min is this magnet's number. A fail-safe interlock (flow AND winding temperature, arranged so failure trips rather than merely alarms) is cheap against a coil rewind; whether an air-cooled coil set needs duty cycling depends on its thermal design, not its power class.
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The educational case for a real cyclotron: it appears in nearly every upper-secondary textbook, students can calculate it in detail, yet almost none has seen one - and the book's stated challenge was getting a cyclotron running in exactly this low-energy range so students can study it while it runs.
Source quote & editorial note
Die Herausforderung dieses Projekts bestand demnach darin, ein Zyklotron in diesem niedrigen Energiebereich zum Laufen zu bringen [tr.: the challenge was to get a cyclotron running in this low energy range]
Editorial note, tabletop extrapolation: Define the teaching machine's safety envelope explicitly rather than declaring it hazard-free: maximum electrode potential (X-ray endpoint), ion species and energy (reaction thresholds - remembering exothermic channels like D-D have none, so deuterium is a different machine), beam current, target and contaminant composition, plus the ordinary electrical, RF, vacuum and stored-energy hazards that exist at ANY energy. Survey, don't assume; the low-energy regime shrinks the radiological terms, not the list.
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Measure a pedagogical build by what follows first beam - the book poses its own test ('when would COLUMBUS not have been worth it?') and answers: 'certainly the project would not have been worth it had it ended after the successful conclusion in 2014' - the value lying in the years of workshops, teacher training, and continuous improvement since.
Source quote & editorial note
Sicher hätte sich das Projekt nicht gelohnt, wenn es nach dem erfolgreichen Abschluss im Jahre 2014 beendet worden wäre [tr.: the project would not have been worth it had it ended in 2014]
Editorial note, tabletop extrapolation: The listed follow-on improvements (magnet stand, acceleration simulation, probe translator, mechanical model) are the kind of second-year items a small-machine program should schedule rather than improvise - as this case study's pattern, adapted to local aims, not a universal checklist.
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The COLUMBUS authors could draw only partly on earlier amateur and student cyclotrons (Niell, Dewan, Steiger, Baumgartner/Heuer, Koeth's Rutgers work) - 'the boundary conditions were too different'.
Source quote & editorial note
Trotzdem konnten wir nur bedingt auf bereits gemachte Erfahrungen zurückgreifen. Zu unterschiedlich waren die Voraussetzungen [tr.: prior experience was only partly usable; conditions were too different]
Editorial note, tabletop extrapolation: The transferable layer across amateur machines is the METHOD - dependency diagram, rigidity sizing, vacuum chain, species-by-q/m - not the numbers: copy the method, recompute every quantity for your own boundary conditions. (Which differences blocked reuse here isn't itemized in the quote; the lesson survives without the itemization.)
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The spiral path-length formula assumes a homogeneous field perpendicular to the orbit plane and zero field in the gap (straight crossings): radii scale as r_i = r1*sqrt(i), giving s_ges = r1*pi*sum(sqrt(i), i=1..k) + k*gap.
s_ges = r1*pi*sum(sqrt(i)) + k*gap; approximation sum(sqrt(i)) ~ (2/3)k^1.5 + (1/2)k^0.5 (the bare (2/3)k^1.5 underestimates); compute k from the actual energy gain per crossingSource quote & editorial note
Diese Gleichung gilt allerdings nur unter folgenden Voraussetzungen [tr.: this equation holds only under the following assumptions]
Editorial note, tabletop extrapolation: Evaluate the sum numerically for your actual k (from injection energy, final energy and effective gain per crossing - higher voltage means FEWER crossings for the same energy); phase slip and gap curvature make the real path longer than the formula, so add margin before comparing with the mean free path.
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Data-sheet benchmark for a surplus laboratory electromagnet of the class suited to a few-keV teaching cyclotron (per the reproduced Bruker BE-15 table - bitmap, not text-verifiable): 150 mm pole diameter, 5-100 mm adjustable gap, 430 kg, 2 x 800 turns at ~1.4 ohm per coil. Consistent series-connection operating points: 20 A gives 32 kAT and ~1.1 kW (cold); 15 A gives 24 kAT and ~0.6 kW; the book reads 300-400 mT off its chart at its operating current with the 75 mm gap.
series coils: NI = 1600*I; P = I^2*(2*1.4 ohm) cold. Ideal gap-MMF lower bound: B*g/mu0 = 22 kAT for 370 mT across 75 mm - a floor, real magnets need more; the chart, not the formula, is the datumSource quote & editorial note
Aus dem Diagramm 5.1 liest man für diesen Strom einen Wert zwischen 300–400 mT für die Flussdichte ab [tr.: for this current one reads 300-400 mT off Chart 5.1]
Editorial note, tabletop extrapolation: A home H-frame with 20 cm poles and a 3 cm gap reaches ~0.6 T with 15-20 kAT, so this surplus-magnet class is a legitimate alternative to winding your own - check the actual coil topology (series vs parallel feeds change the current arithmetic) and take B from a measurement or the manufacturer's chart at YOUR gap.
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El Cerrito's chamber history: the first chamber - curved copper sheets clamped and gasketed around the magnet poles - made 1.5 uA but could not maintain vacuum; the replacement was a rigid ring, 16.5 cm brass tubing with two 0.3 cm steel plates, bottom soldered, top screwed down onto a rubber gasket - and with it the beam reached 7 uA.
Source quote & editorial note
The first attempted vacuum chamber was made of curved sheets of copper that clamped around the magnet's poles. Using gaskets to seal the chamber, the machine produced a beam current of 1.5 microamperes. However, the system could not maintain vacuum and a new design was sought. The modified chamber consisted of a section of 16.5 cm brass tubing used as the wall of the chamber, and two 0.3 cm thick circular steel plates as the top and bottom. The bottom plate was soldered to the brass, the top plate was screwed to the bottom plate with a rubber gasket between the brass and steel to form a seal.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 15
Editorial note, tabletop extrapolation: A rigid soldered ring with one permanently sealed plate and one demountable gasketed plate is a simple chamber architecture with this documented precedent; the conformal clamp-around-sheet chamber has a documented vacuum-failure precedent. (The survey doesn't cost either build - 'low-cost' is our reading of brass tube and hand tools.)
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A cyclotron can run with a single dee and no dummy dee, using the grounded chamber itself as the counter-electrode: El Cerrito did so and, with its second chamber, produced a 7 uA proton beam at 1,600 W operating RF power (2,000 W maximum available to the electrodes).
Source quote & editorial note
The El Cerrito Cyclotron used only one dee, and did not employ a 'dummy dee,' but rather held the chamber itself at ground. ... The system was operated at 1,600 watts and could provide a maximum of 2,000 watts to the electrodes. ... with the new vacuum chamber a beam of 7 microamperes was produced.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 15
Editorial note, tabletop extrapolation: Deleting the dummy dee simplifies the in-chamber assembly at the cost of a less-defined gap field; the precedent documents that the geometry can work at the microampere scale - it does not promise that current class, which came from the whole machine, not the electrode choice alone.
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Coil-winding scale datum for a small cyclotron magnet built by hand, approximately 8 km of 13-gauge copper wire wound on six-inch (15.2 cm) pole pieces (El Cerrito, reported built 1947 by high-school students).
Source quote & editorial note
Approximately 8 kilometers of 13 gauge copper wire were wound around the six inch pole pieces for the electromagnet.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 15
Editorial note, tabletop extrapolation: A concrete scale anchor - kilometre-class wire on a hand-wound magnet is real, with the resistance and cooling that implies - but budget a NEW magnet from its own ampere-turn requirement, winding window, current density and duty cycle; pole diameter alone doesn't set wire length.
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The Cyclotrino team considered a permanent magnet and chose an electromagnet 'because the field could be tuned'.
Source quote & editorial note
although a permanent magnet was considered for the Cyclotrino, it used an electromagnet because the field could be tuned
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Field tunability is a resonance-hunting knob a permanent-magnet machine gives up - which it can buy back through RF adjustment, measured-field frequency selection, shims or trim coils; the precedent documents the convenience of the tunable field, not a prohibition on permanent magnets.
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Surplus NMR-type laboratory electromagnets are a documented magnet source for small cyclotrons: Cyclotrino used a 30.5 cm Varian NMR type electromagnet consuming 500 W at approximately 1 T (1987), and Knox College used an NMR magnet with 2 T maximum field and approximately 20 cm pole faces (2000-01).
Source quote & editorial note
The magnet used was a 30.5 cm Varian NMR type electromagnet, which consumed 500 watts during operation at approximately 1 T. ... [Knox College:] The magnet was a nuclear magnetic resonance magnet with a maximum field of 2 T and approximately 20 cm diameter pole faces.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: NMR magnets bring high field uniformity - their design point - and the Cyclotrino figure (500 W at ~1 T on a 30.5 cm machine; the survey does not specify whether 30.5 cm is the pole diameter) is strikingly low power for the field. Compare against a hand-wound H-frame only with gap, field volume and cooling on the table; the shopping advice that survives any comparison: check surplus NMR listings before winding coils.
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A ham radio transceiver with an oven-controlled crystal served as the RF source for the working Cyclotrino (1987).
Source quote & editorial note
The RF was provided by a ham radio transceiver, using an oven controlled crystal.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Oven-controlled crystal stability addresses the drift side of resonance keeping, and ham gear is well-documented and repairable - as the frequency-stable SOURCE/exciter; what amplification, matching and electrode voltage sat downstream isn't in this sentence, so size the rest of the chain from its own requirements before crediting amateur gear with the whole job.
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Electrode-gap datum, the Cyclotrino (30.5 cm poles, approximately 1 T, 1987) used a dee and dummy-dee pair separated by approximately 1 mm, an extremely narrow accelerating gap on a low-energy mass-spectrometry cyclotron.
Source quote & editorial note
A dee and dummy dee system was used with the electrodes separated by approximately 1 mm.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: A millimetre-class gap maximizes gap FIELD per volt and can improve the transit-time factor - the ideal energy gain per crossing stays q*deltaV regardless - while tightening alignment, flatness and holdoff tolerances (field enhancement rises as the gap closes). One documented small end of the range, not an established bound; choose the gap from the transit-time and holdoff calculation (dg-1396).
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Two brass dees of differing radii created the ion extraction path on Niell's machine, with a small copper sheet set into the path of ions leaving the larger dee as the collector.
Source quote & editorial note
A system of two brass dees with differing radii allowed for ion extraction. ... For a collector, a small copper sheet was set into the path of ions leaving the larger dee, which drew electrons to itself when the ion beam was incident.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: An asymmetric dee pair is a construction-level extraction trick published almost nowhere else - the radius step letting outward-spiraling ions escape the smaller electrode's envelope is the natural geometric reading (our reconstruction; the survey states the arrangement and the collector, not the mechanism), and no deflector is mentioned for this machine.
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To accelerate metal ions without a gas feed, either fabricate the filament from the desired metal or coat a nichrome wire with it, and hold it at negative potential; this solid-source technique ran on the Niell cyclotron (1994-1995).
Source quote & editorial note
either a filament was created from that metal, or a nichrome wire was coated with the metal, and raised to a negative potential
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: A coated-filament thermal source avoids the PROCESS-GAS feed for suitable metals - suitability turning on the metal's vapor pressure, filament compatibility and ionization efficiency - trading species flexibility and current for vacuum simplicity. A candidate for minimal first-beam configurations, evaluated per metal rather than assumed.
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Niell's machine is recorded as evacuated by a mechanical roughing pump with a cold trap, the vacuum monitored by a thermocouple gauge and an ion gauge - the survey names no high-vacuum pump for it.
Source quote & editorial note
A mechanical roughing pump with a cold trap were used to evacuate the chamber
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Read as recorded history, not a pumping recipe: a cold trap captures condensables, not hydrogen or air, so rough-pump-plus-trap has no general sufficiency - what made this credible is the solid coated-filament source (no continuous gas load). For any repeat: measure base and operating pressure under load and check mean free path against the spiral; the same survey's gas-fed machines carry diffusion pumps.
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Build the prototype's vacuum chamber to the final machine's requirements where the roadmap is firm: Rutgers' 22.9 cm prototype (0.889 T) deliberately used a stainless chamber - ports and flanges included - sized for the ultimate 30.5 cm machine (finished 2001, operated in excess of 1.0 T), which then reused the same chamber with only a different ion source.
Source quote & editorial note
one a 22.9 cm diameter prototype and the other was the final 30.5 cm diameter machine, finished in 2001. The prototype operated at 0.889 T, using a dee and dummy dee design. The prototype chamber was constructed for use in the 30.5 cm cyclotron that was the ultimate goal of this project, and so was much larger than required. It was stainless steel, as were the ports and flanges. ... The larger machine used a 30.5 cm pole face electromagnet that operated in excess of 1.0 T, with the same chamber as the 22.9 cm cyclotron but with a different ion source.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Oversizing the first chamber lets the highest-labor component survive the upgrade - a trade, not a law: a larger chamber costs pumping speed, gap (if it sits in the magnet) and money now against rework later; the same survey documents the opposite staging too, so decide from where the rework hurts most on YOUR roadmap.
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Keep the ion-source filament electrically isolated from ground so it can be negatively biased to raise the energy of its emitted electrons (Rutgers, per the survey).
Source quote & editorial note
The filament was kept isolated from ground so it could be negatively biased to increase the energy of the emitted electrons.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Filament bias is the cheapest ionization-rate knob, but it forces the heater supply off any grounded control bus: the supply must be galvanically isolated and float AT the filament's NEGATIVE bias relative to the chamber (the Houghton machine floats its filament near -90 V, dg-310), with insulation rated for the full bias plus coupled RF and transients. And bias raises electron energy, not necessarily ion yield monotonically - scan it (dg-402).
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Enclosed differential-pressure ion source on the Rutgers 30.5 cm machine: the negatively biased filament sat in a ceramic block fed hydrogen through a small hole, capped by a ceramic plate with an aperture - letting a cone of protons stream out into the evacuated chamber while maintaining higher hydrogen pressure around the filament.
Source quote & editorial note
The negatively biased filament was mounted in a block of ceramic material to which hydrogen gas was supplied through a small hole. The ion source was then covered with a ceramic plate with an aperture ... [allowing] a cone of protons to stream out in the center of the evacuated cyclotron chamber, while maintaining a higher pressure of hydrogen around the filament
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: A drilled ceramic block with an aperture is a buildable chimney-style source. The pressure decoupling it delivers is set by the aperture conductance against the gas throughput and chamber pumping - match those (the dg-409/dg-1400 balances) rather than expecting the geometry alone to do it.
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RF power operating-point datum: the Rutgers machine's ENI NMR-300L solid-state amplifier (driven by an HP8656B signal source) could deliver 2,500 W maximum but was usually operated at 50 W with satisfactory results; the earlier prototype used an ENI350L 100 W solid-state amplifier.
Source quote & editorial note
[The RF] signal was produced using a HP8656B signal source, which had greater frequency resolution than the HP8165, and an ENI NMR-300L solid state amplifier. Its maximum output was 2,500 W, but was usually operated at 50 W with satisfactory results.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: Tens of watts sufficed for a 30.5 cm, above-1-T machine with a resonant matching network - at ITS reported operating conditions; the 50x headroom was available, and whether more drive would have bought more beam is not in the record. A useful anchor for amplifier shopping: buy the headroom, expect to run far below it.
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Faraday-collector RF shielding on the El Cerrito-era Niell machine: the collector sat inside a copper tube, cut open on one side with the opening faced toward the ion beam - the tube shielding the collector from the RF signal.
Source quote & editorial note
The copper tube also shielded the collector from the RF signal.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 17
Editorial note, tabletop extrapolation: A grounded slotted shield around the pickup is a sound and documented defense for beam readings taken inside a dee-drive RF field - one layer of several: pair it with shielded signal cable, verify the grounding actually sinks the induced current, and do a beam-off RF-only background run (dg-689's discipline) before crediting the residual as beam.
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Because the Knox ion source was considered experimental and a weak design aspect, it was made completely removable.
Source quote & editorial note
As the ion source was considered experimental and a weak design aspect, it was made to be completely removable.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: Design for swap-out on the least-trusted subsystem - mount whatever you expect to iterate for convenient replacement. Ion sources are a common iteration target in this literature (COLUMBUS's Penning investigation, Rutgers' source change between machines), though no count across the survey backs a strongest-claim ranking.
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Measure the dee-plus-chamber capacitance before designing the resonant circuit: Knox skipped it and had to tune by trial and error; Houghton measured 79 pF for its dee-and-chamber and designed from f = 1/(2*pi*sqrt(LC)).
Source quote & editorial note
The capacitance of the dee's was not measured before building the resonating circuit, rather trial and error was used to tune the circuit. ... [Houghton:] The capacitance of the dee and chamber of the Houghton College cyclotron has been determined to be 79 pf.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 18
Editorial note, tabletop extrapolation: A capacitance measurement on the assembled stack converts resonator design from blind cut-and-try into calculation-plus-trim: include estimated lead/feedthrough parasitics (tens of pF scale means they matter), choose the initial inductance from the formula, and still provide adjustment range - installed resonance always lands off the paper value.
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Smallest-scale existence proof: the first operational cyclotron (1931) used a 0.55 T electromagnet with 10.18 cm pole faces and approximately 2,000 V of oscillating potential to produce hydrogen ions of about 80 keV.
Source quote & editorial note
This cyclotron utilized a 0.55 T electromagnet with pole faces 10.18 cm in diameter, and with an oscillating potential of approximately 2000 V, it produced hydrogen ions with kinetic energies of around 80 keV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 11
Editorial note, tabletop extrapolation: A 10 cm, half-tesla, 2 kV machine made beam - these numbers CALIBRATE one demonstrated design point; they are not independent minima (resonant acceleration works at lower field or voltage with corresponding changes in frequency, radius and turn count), so use them as an anchor for expectations, not a floor for feasibility.
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The thesis's computed fixed-frequency relativistic energy limits for deuterons in a uniform field (pi/2 total phase slip): 1.94 MeV at 1,000 V accelerating potential, 6.13 MeV at 10,000 V, 8.67 MeV at 20,000 V - and the thesis itself notes field shaping mitigates relativity beyond voltage alone, putting the practical proton limit for magnetic resonators nearer 25 MeV.
phase-slip criterion 2*pi*(f - f_rel)*t = pi/2 with the thesis's conventions. Caution: a straightforward re-derivation (energy gain 2qVf per unit time, f_rel ~ f(1-T/m0c^2)) gives ~0.97/3.06/4.33 MeV - half the tabulated values - so the thesis's V convention (dee amplitude vs gap gain) is load-bearing and unstated; reproduce its numbers only with its Eq. (19), not from this sketch.Source quote & editorial note
For a deuteron in an accelerating potential of 1,000 volts, the energy limit is 1.94 MeV, for an accelerating potential of 10,000 volts, the limit is 6.13 MeV, and for an accelerating potential of 20,000 volts, the limit is 8.67 MeV. ... the effects of relativity can be countered by more than just increasing the electrode voltage, it can also be mitigated by adjusting the shape and strength of the magnetic field. The actual relativistic limit for magnetic resonators accelerating protons is closer to 25 MeV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 28
Editorial note, tabletop extrapolation: For sub-MeV machines relativity is far from limiting even at 1 kV dees on any convention - both the thesis's numbers and the halved re-derivation agree on that. If energies ever approach the MeV scale, dee voltage and field shaping are BOTH levers, per the thesis's own remark.
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Field-index sizing guidance adopted in the thesis: large accelerators want only a small radial field decrease to preserve resonance over many turns, while for smaller machines 'a larger increase index is more appropriate, to provide stronger focusing'.
n = -(r/Bz)*(dBz/dr)Source quote & editorial note
for smaller machines a larger increase index is more appropriate, to provide stronger focusing
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 24
Editorial note, tabletop extrapolation: Budget the resonance-versus-focusing trade against the planned turn count quantitatively: integrate phase slip through the proposed B(r) for your turn count rather than assuming percent-level falloff stays cheap, and keep the index inside the weak-focusing stability window (0 < n < 1) everywhere the beam runs.
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Commercial laboratory electromagnet datum: the GMW model 3473-70 with 15.2 cm pole faces and 0-9.9 cm adjustable gap draws up to 70 A (4.1 kW); the machine's Powerten R62B-4050 supply supports only 50 A, at which the field is 1.127 T - the supply, not the magnet, binding the field.
Source quote & editorial note
The magnet, shown in Figure 20, is a GMW model 3473-70 with 15.2 cm pole faces and an [adjustable] pole gap of 0 to 9.9 cm ... The maximum current useable with the magnet is 70 A and at that current the magnet consumes 4.1 kW of power. The power supply however, a Powerten R62B-4050, can only support a maximum of 50 A, at which the magnetic field strength is 1.127 T
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 36
Editorial note, tabletop extrapolation: Anchors the mass/power/gap scale for buying rather than building a 15 cm magnet, and illustrates a procurement lesson worth internalizing: spec the supply WITH the magnet - a 70 A magnet behind a 50 A supply is a 50 A magnet.
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Eight-port budget for a minimal gas-fed machine with internal target diagnostics, two glass viewports (QF16-075-VP), one power feedthrough for the dee (Lesker EFT1213258), one multi-conductor feedthrough shared by the filament and the dummy-dee ground (Lesker EFT0082038), one Faraday collector port, one gas-inlet port with needle valve, one ion-gauge port, and one pumping port.
Source quote & editorial note
two QF16-075-VP Kurt J. Lesker glass viewports, one Kurt J. Lesker EFT1213258 power feed-through for the dee
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 39
Editorial note, tabletop extrapolation: The cited machine's eight-port budget with named catalog parts is a concrete STARTING template - port count and ratings are functions of your source biasing, RF monitoring, cooling and diagnostics, so derive your own list and check current catalog substitutes' voltage/current/vacuum ratings. One specific: a dummy dee wanting RF ground usually needs a short low-inductance chamber bond, not a shared multi-pin conductor - verify which this machine's sharing actually implies before copying it.
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Resonator design from measured capacitance (design calculation; circuit not yet built at writing): dee-plus-chamber measured at 79 pF; at the 1.127 T maximum field, He+ orbits at 4.32 MHz requiring L = 17.2 uH, He2+ at 8.63 MHz requiring 4.29 uH - with maximum energies 77.2 and 309 keV respectively.
f0 = 1/(2*pi*sqrt(L*C)); with C = 79 pF, L = 17.2 uH at 4.32 MHz and 4.29 uH at 8.63 MHzSource quote & editorial note
The capacitance of the dee and chamber of the Houghton College cyclotron has been determined to be 79 pf. If the maximum magnetic field of 1.127 T is used then the frequency of orbit for singly ionized helium is 4.32 MHz, and thus the inductance, using (23), must be 17.2 uH. In this system the maximum energy for singly ionized helium is 77.2 keV. For doubly ionized helium, the frequency in the same magnetic field is 8.63 MHz, so the inductance is 4.29 uH, and the maximum energy is 309 keV.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 46
Editorial note, tabletop extrapolation: A rare published electrode-system capacitance anchor for microhenry-scale resonator sizing at this machine class - noting the energy quadrupling with charge state at fixed field (the implied orbit radius is ~7.1 cm), that 79 pF is build-specific, and that the installed resonance still needs the parasitics-and-trim treatment (dg-1462).
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Set the amplifier drive from the spark limit: the thesis's design logic is that dee voltage follows from drive current through the resonant circuit, so the supplied current must be chosen to keep the dee below breakdown - with V = I*X_C valid only for I the CAPACITOR-BRANCH current, not the amplifier output current.
V_dee,peak = I_C,peak * X_C, X_C = 1/(2*pi*f*C), I_C the capacitor-branch (circulating) current; amplifier-to-dee transfer depends on coupling and loaded Q - measure itSource quote & editorial note
In order to avoid sparking in the gaps in the cyclotron chamber, the voltage supplied by the amplifier must be carefully chosen.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 45
Editorial note, tabletop extrapolation: With a high-Q resonator the dee voltage is set indirectly, so the spark limit must be designed in rather than discovered: use the measured or modeled loaded transfer function from amplifier to dee, verify with a calibrated pickup (dg-307/dg-1356), and back it with arc detection - the branch-current subtlety is exactly where a naive I*X_C sizing goes wrong.
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Species staging for commissioning (the thesis's stated plan): first accelerate helium nuclei to test the machine, then switch to deuterons for neutron production; expected energies 0.15 MeV for deuterons, 77.2 keV for He+ and 309 keV for He2+ (0.08 MeV appearing as the p.2 summary figure).
Source quote & editorial note
The immediate objective is to accelerate Helium nuclei to test the machine, and the ultimate is to accelerate deuterons to produce neutrons ... The expected energy for deuterons is 0.15 MeV, and 0.08 MeV for Helium nuclei. ... the maximum energy for singly ionized helium is 77.2 keV. For doubly ionized helium, the frequency in the same magnetic field is 8.63 MHz ... and the maximum energy is 309 [keV]
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 2
Editorial note, tabletop extrapolation: Debugging resonance, focusing and diagnostics on helium defers the deuteron-specific neutron/activation source term - NOT all radiological consequences: RF/HV dark current makes bremsstrahlung with any gas, and He2+ is an alpha that can drive exothermic reactions on light contaminants (Be-9, C-13). Survey from first powered operation; the staging defers the big term, not the survey.
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Self-loading neutron target scheme (the thesis's stated plan): a copper target in the chamber becomes impregnated with beam deuterons; further beam drives d(d,n)3He and d(d,p)3H on the embedded deuterons; 'since neutrons are the desirable result, no extraction system will be required' - the thesis giving 2.8 MeV for the outgoing neutrons, which pass through the chamber walls.
Source quote & editorial note
A copper target will be placed in the chamber, which will as a result of the beam be impregnated with deuterons. More ions from the beam will collide with the trapped deuterons, undergoing one of two reactions, d(d,n)3He or d(d,p)3H. Since neutrons are the desirable result of the reaction, no extraction system will be required. ... the outgoing neutrons will be produced with 2.8 MeV. The electrically neutral neutrons will pass through the chamber walls and can then be used for inelastic scattering measurements.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 48
Editorial note, tabletop extrapolation: A beam-loaded (drive-in) copper target avoids separately fabricating a deuterated target and removes extraction from the critical path. Physics notes on the thesis's numbers: D(d,n)3He neutrons at ~150 keV bombarding energy are angle-dependent, roughly 2.1-3.0 MeV in the lab - 2.8 MeV is one point on that curve, not the spectrum - and the thesis does not analyze dose or shielding beyond its concrete room, so the radiological planning is entirely on the builder.
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Personnel protection as built: the accelerator sits in a concrete brick room with an interlock control system preventing the machine from being turned on while a person is in the room.
Source quote & editorial note
in a concrete brick room with an interlock control system to prevent the accelerator from being turned on when a person is in the room
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 29
Editorial note, tabletop extrapolation: The documented access-control arrangement of the source machine - occupancy interlock plus (per its electronics chapter) remote operation - is a COMPONENT of protection, not a certified minimum: shielding calculations, surveys, monitors, fail-safe interlock design and applicable regulatory requirements decide sufficiency for any neutron-capable machine, and the thesis presents no dose analysis.
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Staged chamber sizing in the other direction, the as-built chamber and electrodes do not use the magnet's full pole diameter, and the stated longer-range plan is to build a larger vacuum chamber and electrodes later to take full advantage of the field diameter, along with ferromagnetic shimming of the field.
Source quote & editorial note
Longer range plans include building a larger vacuum chamber and electrodes
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 48
Editorial note, tabletop extrapolation: Starting with an undersized chamber inside a full-size magnet is the documented counter-strategy to Rutgers' build-the-final-chamber-first (dg-1451) - the stated plan here being a larger chamber and electrodes later. Faster first beam and deferred precision work are the plausible payoffs to EVALUATE, not documented outcomes; either staging is defensible depending on where rework hurts.
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Scrapyard magnet construction on Niell's machine: the yoke was soft iron scrap, the pole pieces 11.4 cm steel round stock wound with 13.5-gauge wire.
Source quote & editorial note
The magnet yoke was soft iron scrap, and the pole pieces were 11.4 cm steel round stock which were then wound with 13.5 gauge wire.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: A documented precedent that scrap return-path iron plus machined round-stock poles can serve a small machine - the machine as a whole made beam, though the survey doesn't isolate the magnet's contribution. For a new build, characterize candidate scrap (saturation, consistency, joints) and remember the return path needs cross-section, not pedigree.
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The Cyclotrino's vacuum, per the survey: produced by a vacuum reservoir with a cryopump system.
Source quote & editorial note
The vacuum was produced by a vacuum reservoir with a cryopump system.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 16
Editorial note, tabletop extrapolation: Read carefully: a cryopump IS a pump (it keeps pumping while cold), so this is oil-free, low-vibration pumping plus buffer capacity - not a pumpless machine. The architecture suits a source with little gas load (Cyclotrino's cesium-sputter source); the reservoir buys hold time against transients, not indefinite operation. Get the actual cryogenic arrangement before copying claims about power or vibration at the machine.
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Choose design beam energy from the reaction excitation curve: the thesis justifies its 150 keV deuteron design energy by placing the d(d,n)3He cross-section 'near the maximum' of its plotted curve, calling the reaction exothermic with - as printed - '2.227 MeV released for each deuteron pair'. [Source-internal error, surfaced: 2.227 MeV is approximately the DEUTERON BINDING energy; the D(d,n)3He Q-value is 3.27 MeV and D(d,p)3H is 4.03 MeV. And the D-D cross-section keeps rising well beyond 150 keV - 'near the maximum' holds only within the thesis's plotted range.]
Source quote & editorial note
The maximum energy of the current cyclotron, using (6), is 150 keV for deuterons, which puts the cross section near the maximum. ... [the d(d,n)3He reaction is] exothermic with 2.227 MeV released for each deuteron pair.
Cressman, The Design and Construction of a Small Cyclotron — Houghton College thesis (2006) — p. 49
Editorial note, tabletop extrapolation: Working back from the excitation curve converts machine energy from a bragging number into a requirement - the transferable design move. D-D is the standout low-energy neutron reaction because its cross-section is already usable near 100 keV; take Q-values and cross-sections from live evaluated data (per site policy), not from the thesis's figures.
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A school-scale teaching cyclotron's documented timeline: the COLUMBUS project started in 2012 (FZ Juelich provided the magnet, VACOM sponsored the chamber), registered first beam in April 2014, held its first student workshop that autumn, and - in the authors' 2022 retrospective - 'has developed very positively in the last 10 years' of continuous incremental improvement.
Source quote & editorial note
After the FZ Juelich provided a magnet, VACOM, a company for vacuum components, sponsored a suitable vacuum chamber ... the cyclotron COLUMBUS began in 2012. ... The first beam was registered in April 2014 (see Fig. 2), which was followed by the first workshop with students in autumn of the same year. ... The COLUMBUS project, started in 2012, has developed very positively in the last 10 years.
Editorial note, tabletop extrapolation: A realistic schedule anchor for the plan's teaching-machine ambitions: two years start-to-beam WITH a donated magnet and sponsored chamber - the in-kind support is part of the datum. And the methodological point stands: a conference paper's year dates the claim; prefer the builders' own retrospective dates when reconstructing a machine's history.
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2022 operating configuration per THPO001's Table 1 and text: 140 mm (5.5 in) dee diameter in a chamber 200 mm diameter x 75 mm high; flux density 185 mT (H+) / 370 mT (H2+); dee voltage 0.5-3.0 kV; final energy ~4.1 keV (H+) / ~7.5 keV (H2+).
Source quote & editorial note
[a] chamber with a diameter of 200 mm and a height of 75 mm. ... Diameter of the Dees 140 mm (5.5 in) Flux density 185 mT (H+) | 370 mT (H2+) ... Dee Voltage 0.5 - 3.0 kV Final Energy ~ 4,1 keV (H+) | 7,5 keV (H2+)
Editorial note, tabletop extrapolation: A long-serving teaching machine running protons at half its field capability eases magnet, RF and matching demands at the cost of energy. The quoted energies imply a ~48-50 mm detection radius (nonrelativistic equilibrium-orbit calculation at the stated fields - a derived number, not a printed one); treat the table as the published 2022 configuration without assuming every entry is a measured operating value.
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Operating-point vacuum budget with an internal hydrogen-fed source — 1e-6 mbar base pressure in the chamber, rising one decade to 1e-5 mbar with H2 gas flowing; beam production and detection function in that regime.
Source quote & editorial note
Vaccum in the chamber 10-6 mbar dto with H2 10-5 mbar
Editorial note, tabletop extrapolation: Plan pumping capacity for the gas-on state, not the base pressure; a decade of pressure rise under source gas load is the demonstrated working regime for a keV-class internal-source machine at this scale. (Quote reproduces the table verbatim including its spelling; exponents are superscripts in the original.)
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Evolution path for the ion source — the machine runs a hydrogen filament source, and a Penning ion source is under investigation (as a student internship project) with the aim of installing it in the accelerator; source replacement is treated as an incremental upgrade, not a redesign.
Source quote & editorial note
or investigate a Penning ion source with the aim of using it for the installation in the accelerator.
Editorial note, tabletop extrapolation: A filament source reached first beam here and a candidate Penning source is being investigated as a student project - the sensible pattern being to characterize any replacement source off-machine, then verify its mechanical, vacuum, electrical, gas-feed and central-region interfaces before installation; a source swap touches more of the machine than the source (recommendation, not the paper's documented method).
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The two hardest procurement items for a school-built cyclotron, a homogeneous-field magnet and a custom vacuum chamber, were both solved by donation, per the 2013 account: a research institute (Juelich, IKP) donated a Bruker BE-15 laboratory magnet, and a vacuum-component company (VACOM) fabricated the ten-port chamber free of charge, with further support from regional companies, foundations and a youth-science sponsor pool.
Source quote & editorial note
At the very beginning there were two big problems: How to get a magnet for the homogenous field and How to get a suitable vacuum-chamber. The first problem was solved by the Research Institute of Jülich. Prof. Dr. Maier and his team donated a Bruker BE-15. … The second problem was solved by VACOM, a company specialized in vacuum-components. VACOM built the vacuum-chamber, i.e. Fig. 1, for us free of charge.
Editorial note, tabletop extrapolation: For an educational build, soliciting institutional donations for the few components a home or school shop cannot make is a documented alternative to surplus-market hunting.
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An adjustable-gap laboratory electromagnet lets one magnet serve several field regimes: the donated machine's 150 mm poles with pole pitch adjustable over 50-120 mm reach up to 2 T at close spacing and up to 0.7 T at 100 mm spacing (design-era figures, 2013), so the pole spacing chosen around the chamber sets the field ceiling available to the coils.
Source quote & editorial note
The pole-diameter is 150 mm (~ 6 in). The pole pitch is adjustable from 50 - 120 mm (~ 2 - 5 in). The flux-density is up to 2 Tesla depending on the spacing of the poles. At a distance of 100 mm the flux-density is up to 0.7 Tesla.
Editorial note, tabletop extrapolation: When adopting a surplus laboratory magnet, the published pole diameter, pitch range and field-versus-spacing figures are the sizing inputs; the field available at the actual chamber-plus-walls spacing is the number that matters.
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The RF source specified at design time (2013) was a marine short-wave transceiver delivering 50-70 Veff across 500 kHz to 35 MHz with 120 W available power, feeding a matchbox that steps the output up to the 2000-3000 V needed between the dees.
Source quote & editorial note
The RF-power-source is a short-wave transceiver for marine radio. It provides an AC voltage of 50-70 Veff at frequencies from 500 kHz to 35 MHz. The available power is 120 W. … As well as an impedance converter the matchbox is also an RF-transformer transforming the 50 - 70 V output voltage of the power-source up to 2000-3000 V voltage, which is needed for the acceleration of the protons.
Editorial note, tabletop extrapolation: The transmitter's rated power is a design-era catalog figure; the usable continuous carrier in the modulation mode actually chosen should be verified on the bench before the RF power budget is frozen.
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In a machine of very few revolutions (ten or fewer), the source deliberately departs from the normal centred mounting: its position is adjustable in the direction of the accelerating gap so the ideal starting position of the first path can be found by experiment; in the reference design the source is therefore not fixed-mounted but stuck under the dummy-dee (design decision, 2013).
Source quote & editorial note
For the setup of the ion source, it is considered that the ion source remains adjustable in direction of the gap, so that the ideal position can be found by experiments. Normally the ion source is centred in the cyclotron. However, in our case – with our small cyclotron and such a small amount of revolutions (≤ 10) - it is better to optimize the starting position of the first path. Due to this fact the ion source will not be fixed mounted but it will be stuck under the dummy-dee instead
Frank, Wolf & Held, COLUMBUS — A Simple Ion Source — WEPPT021, Proceedings of Cyclotrons2013 (2013) — p. 1
Editorial note, tabletop extrapolation: With only a handful of turns there is no adiabatic settling; an adjustable source mount converts a machining guess about the first half-turn into a tunable parameter, and the optimum need not be the centred position.
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Because ions leave a thermionic chimney source with very low energy, make the emission direction adjustable as well: a rotatable source-head lets the slit angle be optimized by experiment for better acceleration and to prevent the protons remaining in the gap between the dees (design decision, 2013, pre-beam).
Source quote & editorial note
the angle of emission shall be adjustable for a better acceleration and to prevent that the protons remain in the gap between the dees
Frank, Wolf & Held, COLUMBUS — A Simple Ion Source — WEPPT021, Proceedings of Cyclotrons2013 (2013) — p. 1
Editorial note, tabletop extrapolation: A rotatable head is a cheap second degree of freedom on top of source position; both exist because low-energy ions do not forgive alignment errors in the first gap.
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The school machine's ion source was built after the pattern Tim Koeth first used in the Rutgers 12-inch cyclotron (the paper's reference [1]); the project's own design effort went into what its few-revolution machine specifically required - adjustability of source position and emission angle.
Source quote & editorial note
The protons for our cyclotron are produced in the ion source which was built after the pattern of Tim Koeth [1], which he used first in his cyclotron. … A specific design of the ion source was required due to the cyclotron's small size and the low number of revolutions … It was designed for adjusting the position of the ion source itself and the proton's angel of emission. … [1] Tim Koeth, "The Rutgers 12-Inch Cyclotron Ion Source Studies Part I"
Frank, Wolf & Held, COLUMBUS — A Simple Ion Source — WEPPT021, Proceedings of Cyclotrons2013 (2013) — p. 1, 2
Editorial note, tabletop extrapolation: A documented precedent for reusing a published hobby-machine source design: here the ionization geometry was adopted whole and the adaptation effort spent on mounting and adjustability.
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Laser powder-bed metal 3D printing (LaserCUSING, stainless steel 1.4404, layer thickness 15-500 microns) can produce components that meet high-vacuum requirements; the reported validation was deliberately bounded to the high-vacuum range because the pump station used did not go below 10^-5 mbar, with ultra-high vacuum (below 10^-7 mbar) named as untested next territory.
Source quote & editorial note
This work is limited to the area of high vacuum. The limitation is due to the simple handling of the components and the existing pumping station, with which a minimum of 10-5 mbar is not undercut. … The present work shows that metal-based 3D printing can meet the requirements of vacuum technology in the area of high vacuum.
Editorial note, tabletop extrapolation: Printed 316L-class components are demonstrated at high vacuum down to the study's achieved 1.5·10-5 mbar; the 10-6 decade was not reached by its pump station and UHV is explicitly untested, so claims below the tested pressure are extrapolation, not evidence.
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Printing standard vacuum components is hardly worthwhile - the paper's conclusion from the elaborate post-processing - so the economic pattern it demonstrates is hybrid construction: print only the geometrically complex body and complete it with conventionally manufactured standard parts (here by welding on flanges and tube).
Source quote & editorial note
Due to an elaborate post-processing, it is clear that the 3D printing of standard components will hardly be worthwhile. Consequently, in order to achieve an economic use of this technology, it is necessary to retrofit the printed components with standard parts from conventional manufacturing.
Editorial note, tabletop extrapolation: For a low-budget build the demonstrated pattern is catalog KF/CF hardware joined to a printed complex body; a plain straight connector is exactly the case the source found uneconomic to print. Compare current quotations - the economics move with the market.
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A complete working vacuum chamber can be built as a printed complex base body with integrated channels, finished by welding on standard commercial components; the approach avoids unnecessary rework, and its geometry can be re-adapted per build since no tooling or molds are involved.
Source quote & editorial note
Since no moldings and other tools are necessary for the production of 3D printed components, there are no further costs. … The basic body of the vacuum chamber was supplemented with a complex geometry and integrated flow channels and completed by welding standard components. In addition to a cost-effective production by avoiding unnecessary rework, this method also has the advantage of a flexible adaptation to different customer requirements.
Editorial note, tabletop extrapolation: For a multi-port chamber whose port pattern is unique to one machine, a printed body with welded catalog flanges is a demonstrated alternative to welded-plate fabrication and machining from solid, and the port layout can be revised in CAD between builds without molds or dedicated tooling - the build itself still costs supports, fixtures, inspection and sealing-surface machining, so the comparison is build-specific.
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Metal 3D printing's benefit for vacuum work concentrates in single production and prototypes, where geometry freedom and function integration (the paper's example: a built-in surface heating system) carry the case; the same paper found printing standard components hardly worthwhile.
Source quote & editorial note
Especially for single production and prototypes, 3D printing technology can be of considerable benefit. This is particularly due to the freedom in geometry and the possibility of function integration, such as the realization of a surface heating system.
Editorial note, tabletop extrapolation: A one-off machine is exactly the single-production case; a sound screening default is to consider printing where a part is unique and geometrically complex and to price catalog, machined, welded and printed options case by case.
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At very low energy a deliberately flat (flutter-free) cyclotron field paired with electrostatic axial focusing from a high RF harmonic is a viable architecture; the LBNL cyclotron mass spectrometer chose it over an azimuthally varying field because it is a simpler magnet configuration when the harmonic provides adequate focusing.
Source quote & editorial note
A flat field without flutter was selected since it is a simpler configuration for this very low energy and the high harmonic provides adequate electrostatic axial focussing
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: removing hills and valleys is viable at low energy only where the RF harmonic and dee geometry demonstrably supply the axial focusing the flutter no longer provides — the LBNL machine ran at harmonic 15 with electrostatic focusing doing that job. Verify axial stability by analysis or tracking before deleting flutter from a design; low energy alone does not guarantee it.
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High mass resolution in a cyclotron mass spectrometer demands isochronous orbits, which in a flat-field design translates directly into an absolute field-flatness specification; the LBNL CMS required its 1 T midplane field uniform to about 2 parts in 1e4 to reach a mass resolution of 1800.
Source quote & editorial note
In this design H is 15 and the minimum number of orbits is 40, giving the required R = 1800 ... The magnetic field in the midplane is 1 T. For high mass resolution, the orbits need to be isochronous; a flat magnetic field uniform to about 2 parts in 104 must therefore be maintained
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: sets the scale of what field quality buys — the source pairs 2e-4 flatness with 40 turns at harmonic 15 to reach R = 1800. A machine running few turns on the fundamental tolerates far looser fields; derive the flatness budget from turn count, harmonic, and the allowed cumulative RF phase slip, not by copying this figure.
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The Halbach crown-and-barrel arrangement splits the permanent-magnet material per pole into two groups: a crown section above the pole driving flux axially down into pole and gap, and a barrel section outside the pole rim driving flux radially inward, with a cylindrical iron yoke completing the circuit.
Source quote & editorial note
The permanent magnets for each pole are grouped into 2 sections, the "crown" section and the "barrel" section. For example, as shown in Figure 4, for the upper pole the crown section is placed above the pole and directs magnetic flux down into the pole and gap. The barrel section is placed outside the pole and directs flux inward toward the pole and gap ... A cylindrical yoke completes the magnetic path
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a proven topology for energizing round cyclotron poles from permanent magnets with no coil at all. The two magnet groups give two knobs (axial and radial flux feed) for setting field level and radial profile, but they are coupled through the shared pole, fringing and return yoke — set them with magnetic modeling and a field map, not as independent controls.
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In a PM-energized magnet the iron pole is the precision element and spatial filter: the pole face carries the high-accuracy machining because it is the surface the gap sees and it determines the accuracy of the field, while the permanent-magnet blocks behind it can be of coarser arrangement because they sit farther from the midplane.
Source quote & editorial note
The pole is machined to high accuracy since it is what the gap "sees" and thus determines the accuracy of the magnetic field. The permanent magnet comes in blocks, which can be of coarser arrangement since they are farther from the midplane
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: concentrate the machining budget on pole faces and gap parallelism; commercial magnet blocks with ordinary tolerances are acceptable upstream of an iron pole — the key enabler for building a precise field from inexpensive stock magnets. The pole filters high-spatial-frequency block errors; low-order errors (remanence spread, block placement, gap and yoke asymmetry) still reach the midplane, so confirm with a tolerance analysis and a field map.
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Permanent-magnet material may be arranged coarsely (discrete stock blocks with gaps and steps) provided it sits far from the midplane relative to the gap, because the intervening iron pole averages out block-to-block variations.
Source quote & editorial note
The permanent magnet comes in blocks, which can be of coarser arrangement since they are farther from the midplane
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: distance from the midplane is the tolerance relief for short-wavelength errors — block placement and discretization errors attenuate with distance, so the rough assembly sits far from the gap and the iron pole does the smoothing. Coherent and low-order errors survive the distance, and standoff costs flux; evaluate the needed distance and the residuals with a sensitivity model or a field map.
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An effective PM-magnet design sequence is a fast analytic flux calculation first (direct and indirect flux for candidate geometries, defining the dimensions of magnets, poles, and yoke), followed by POISSON-class finite-element verification and optimization of the chosen configuration; the LBNL CMS magnet was designed exactly this way.
Source quote & editorial note
Initially, a program which analytically calculated the indirect and direct magnetic fluxes from various candidate configurations was used to define the dimensions of the magnets, poles, and yoke. The computer program POISSON was then used to verify and optimize this solution
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: the analytic pass explores the design space cheaply; the FEA pass is reserved for verifying one or two survivors. Free 2-D solvers fill the POISSON role today — noting that a 2-D axisymmetric model verifies the nominal design only, so discrete-block and assembly asymmetries need 3-D modeling or a measured field map.
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Build shimming margin into permanent-magnet quantity in the removable direction: the LBNL CMS deliberately installed barrel magnets slightly larger than the computed optimum, planning to cut them back for shimming after field measurement — and the measured pre-trim field came out flat to 7 parts in 1e4 with the excess in place, an anticipated deviation.
Source quote & editorial note
within the acceleration region between 5 cm and 12 cm, the field is flat to within 7 parts in 104. This small deviation was anticipated since slightly larger than optimum barrel magnets were installed, to be cut back later for shimming
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a margin in the removable direction is cheap insurance in a PM circuit — cutting blocks back is routine, adding material means buying new magnets. It is one trim mechanism among several (iron shims, flux shunts, repositioned blocks, correction coils); choose the adjustment mechanism and its planned range at design time rather than biasing every PM installation high by default.
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The source's stated approximation for cyclotron-mass-spectrometer resolution is R ≈ 3 n H, with n the number of in-phase turns before extraction and H the RF harmonic number — so resolution is bought with more turns or a higher harmonic, each carrying its cost elsewhere in the design (the source's center-region compromise, dg-1556).
R ~ 3 * n * H (n = turns before extraction, H = RF harmonic)Source quote & editorial note
a mass resolution of about 1800 is needed to separate 14 C from 13 CH. The resolution of a CMS is approximately: R ≈ 3 x n x H, where n is the number of turns that in-phase particles make in a synchronous field before extraction and H is the rf harmonic number
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: an estimating relation, not a law — the coefficient depends on the phase-slip criterion that defines an in-phase turn. Useful for order-of-magnitude estimates of how sharply a small machine discriminates species or off-resonance drive; derive the real number from a phase-history calculation for the actual field and RF program.
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Sizing a small cyclotron is a compromise between center-region clearance and transit time: better clearance requires either a larger (costlier) magnet or a smaller injection radius, and a smaller injection radius worsens the transit time at high harmonics — so the design seeks a magnet just large enough that the injection radius still gives a good transit-time factor with good center-region transmission.
Source quote & editorial note
The overall size of the machine is dictated by the mass resolution needed, the turn separation needed to clear the center region, and the injection energy. Better center region clearance requires a larger magnet, which is more expensive, or it requires a smaller injection radius, making the transit time worse for high harmonics. So a compromise has to be made giving good transmission in the center region and a large enough injection radius to give a good transit time factor
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: on high-harmonic or low-voltage designs the center region can drive machine size alongside the final-orbit rigidity — check the transit-time factor at the first gap crossing before shrinking the injection radius to save magnet steel, and check that the extraction-radius rigidity still fits the pole.
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The whole-system payoff of a PM-energized cyclotron magnet is elimination of magnet coils, power supplies, and magnet cooling — reducing utility requirements enough that the LBNL team judged their 1 T, 30-cm-pole instrument portable for use in hospitals, trucks or airplanes. The accepted cost is loss of field-strength variability, tolerable for a single-ion-mass instrument; the source notes other ions could be reached by scaling injection energy, RF frequency and dee voltage to the fixed field.
Source quote & editorial note
The resulting loss in variability of the field strength is acceptable because the instrument is intended to be used for only one single ion mass with charge 1, although scaling of injection energy, rf frequency and dee voltage could be used to accelerate other ions ... No coils or power supplies and no cooling are required for the magnet. This reduces the utility requirements for the spectrometer system as a whole. This reduction and the small size and weight make the system "portable", conceivably permitting utilization in medical studies in hospitals, or for environmental monitoring in trucks or airplanes
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a fixed-field PM magnet trades away tuning range — B fixes the orbit and RF frequency scale, and the electrical settings (frequency, dee voltage, injection energy) must be matched to it; they are matching parameters for reaching a different ion, not substitutes for field adjustment. Best suited to machines committed to one species and one configuration at a time. The cooling eliminated is the magnet's own; RF and other systems keep theirs.
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Ion-chemistry selectivity is a powerful source-level filter: the LBNL CMS accelerates 14C as a negative ion because the dominant atomic isobar, 14N, does not form a negative ion and so is suppressed before injection — while molecular interferences such as 13CH still require the machine's full mass resolution.
Source quote & editorial note
a mass resolution of about 1800 is needed to separate 14 C from 13 CH ... To suppress the 14N background, 14C- is used, since 14N does not form a negative ion
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: choosing charge state and species at the source is the cheapest background filter available for the interferences it can reach; it complements rather than replaces downstream discrimination — the same instrument still needed R ≈ 1800 for the molecular isobar.
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Axial injection down the machine axis is very efficient at delivering external-source ions into the cyclotron midplane; the LBNL CMS used a spiral inflector — an electrostatic channel that twists as it guides ions down the axis and into the midplane — designed with a trajectory code including the actual spatial variation of the magnet field plus a midplane tracking code including electrostatic focusing effects.
Source quote & editorial note
Axial injection, in general, is very efficient in delivering the ions into the cyclotron midplane. We have designed a spiral inflector, an electrostatic channel which twists or "tilts" as it guides the ions down the axis of the machine and into the midplane ... This was accomplished using an ion trajectory program which takes into consideration the spatial variation of the magnetic fields in the cyclotron for the inflector design and a second trajectory program which calculates the cyclotron midplane trajectories, including electrostatic focusing effects
Editorial note, tabletop extrapolation: Ignoring the real field map in the inflector region, or the electrostatic focusing in the first turns, breaks the emittance match even when the idealized design closes; both effects belong in the design loop from the start.
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A magnetic multicusp source forms negative ions directly from gas-phase precursors in the discharge plasma; the LBNL CMS pursued it for C- production because, if successful, it would give a simple-to-operate, high-throughput negative-ion source without the graphitization step cesium sputter sources require.
Source quote & editorial note
substantial experience has been obtained in developing negative ion sources for fusion and ion implantation applications using magnetic multicusp sources ... In these devices, negative ions from gas phase precursors are formed directly in the discharge plasma. Recent experiments have shown that C- can be formed in these sources as well ... If successful, it will provide a simple to operate, high throughput source of negative ions without the need for the graphitization process used with sputter ion sources
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: gas-fed volume production of negative ions removes the sputter source's solid-sample preparation; the multicusp family LBNL drew on here is the one developed for fusion H- work, which is the variant a small machine would borrow. Yields and operability are species- and plasma-dependent — treat performance claims as per-species questions, and note the source itself states the C- case as prospective.
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In the LBNL PM magnet scheme the magnet material is placed in direct contact with soft-iron pole pieces and the iron concentrates and steers the flux to the pole faces; blocks on one pole are magnetized toward its face and on the other pole away from its face, with an iron yoke closing the circuit around the midplane gap.
Source quote & editorial note
Magnet material, such as samarium cobalt, is placed in contact with the iron pole pieces. The iron concentrates and directs the magnetic flux to the pole faces. For one pole, the magnets are oriented so that the magnetization vector points toward the pole face. For the other pole piece, the magnets are oriented so that the magnetization points away from the pole face. A magnetic flux return ('yoke') connects the magnets to complete the circuit. The midplane of the accelerator is placed between these poles
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: the iron pole and yoke strongly shape the flux the blocks supply, but the gap field is set jointly by the magnetization layout and the iron circuit — model both. The two assembly-critical facts remain: consistent magnetization polarity per pole (toward one face, away from the other) and a properly closed flux-return yoke.
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Design the extraction radius with margin over the minimum that meets the physics requirement: the LBNL CMS could reach its turn count with 1500 V per turn at an extraction radius of 9 cm or less, but was conservatively laid out for 12 cm extraction (50 keV) on a 15 cm pole face.
Source quote & editorial note
With modest energy gain per turn, 1500 V, it is possible to achieve this figure with an extraction radius of ≤ 9 cm. We have conservatively designed the instrument for an extraction radius of 12 cm, corresponding to an energy of 50 keV ... [Table 1:] Pole face radius 15 cm
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: radius margin keeps the working orbit away from the field-edge rolloff and leaves headroom in turn count and final energy above the bare requirement. It does not bend the rigidity relation — at fixed field the orbit radius for a given energy is fixed, so lower-than-planned dee voltage costs turns, not radius. Committing the magnet to the bare-minimum radius leaves no recovery path once it is built.
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A hybrid dipole architecture assigns each field-control function its own hardware layer: Sm2Co17 permanent magnets supply the main field for free, a copper trim coil gives fine adjustment over a limited range, movable outer iron plates give coarse adjustment, and NiFe alloy plates passively stabilize against temperature - power consumption falls far below an equivalent electromagnet while keeping operational tunability.
Source quote & editorial note
A typical hybrid dipole magnet (Fig. 1) consists of DT4E poles, yokes, Sm₂Co₁₇ permanent magnet blocks, a copper trim coil, outer tuning plates, NiFe alloy plates, and aluminum structural parts. In this configuration, the PM blocks provide the main magnetic field, while the trim coil allows for fine adjustment of the field strength within a limited range. This design significantly reduces power consumption compared to traditional electromagnets, while still preserving operational flexibility. To improve adaptability, an outer iron plate mechanism is incorporated for coarse field tuning ... to address the negative temperature coefficient of permanent magnets, NiFe alloy plates are placed near the magnet poles. These act as passive compensators to stabilize the magnetic field against temperature variations
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a small PM-based magnet need not be untunable — layering a modest trim coil and a movable iron shunt onto a PM circuit restores fine and coarse adjustment within a limited range (±1.25% fine on this prototype) at a small fraction of an electromagnet's power. Enough for drift, matching and calibration; not the wide excitation range of a full coil.
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Large PM blocks can be built up by gluing smaller magnetized units together rather than procuring monolithic pieces, giving flexibility in size and shape while holding field performance, provided dimensional tolerances and per-block flux consistency are specified from simulation of their field effect.
Source quote & editorial note
These blocks (Fig. 2) are not formed as a single piece, but are assembled by gluing smaller magnetized units together. This method allows us to fabricate magnets in flexible sizes and shapes, while maintaining field performance. Dimensional tolerances and flux consistency were kept within acceptable ranges based on simulation results
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: small stock magnets glued into arrays are a legitimate substitute for expensive custom blocks when grade, magnetization vector, polarity, dimensions and bonding are controlled. Set the dimensional and per-block flux acceptance from a simulation of their field effect, as the source did, and verify the assembled magnet with a field map — a spot gaussmeter reading is a screen, not a flux acceptance test.
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Program structure of a 1.5 MeV undergraduate cyclotron (ISU, 1961): work divided into cyclotron-technology experiments (resonance-curve shape, magnetic tune-down versus radius, vertical beam extent - each compared against in-house orbit calculations) and nuclear-physics experiments, which the 1.5 MeV energy limited to the lightest elements (lithium and carbon targets). Student experimenters were supported by an NSF undergraduate research program.
Source quote & editorial note
The experimental program on the Iowa State University undergraduate 1.5 Mev cyclotron is divided between cyclotron technology experiments and nuclear experiments. Beam technology work has been done in the determination of the shape of the resonance curve as a function of the magnetic field strength and radius, the determination of the tune-down at various radii, and the measurement of the vertical excursion of the protons (beam height). The experimental measurements have been compared to the theoretical calculations made for the ISU cyclotron by A. H. Mueller (1). The nuclear physics experiments are limited to the lightest elements due to the low energy of the machine. Comprehensive experiments have been performed using lithium and carbon as the target material ... [footnote:] This work was made possible in part by grants from the National Science Foundation Undergraduate Research Participation Program.
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a low-energy machine supports a real two-track curriculum — the accelerator itself as measurement subject (tuning curves, field studies, beam optics) plus light-element nuclear physics. The machine-as-experiment track begins as soon as beam circulates; the nuclear track needs its own justification per experiment — reaction energetics, yield at the available current, detection capability, and radiation controls.
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Beam-intensity sensitivity to the magnetic field, computed for the ISU 1.5 MeV cyclotron (1961): the orbit calculation found that field changes of only a few gauss (in 17,000 - parts in 10^4) can produce a large reduction in beam intensity, because at larger target radii the window of tune-down values giving full intensity narrows sharply.
Source quote & editorial note
It was found that changes in the magnetic field strength of only a few gauss can result in a large reduction of the beam strength ... it can be noted in Figure 4 that the interval of δB values for which the relative intensity, I, is equal to 1 decreases with increasing target radius
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: period support for gauss-level (parts-in-1e4) field-tolerance thinking in small-cyclotron design — computed for this machine's field profile, voltage and phase model, and consistent with its companion measured tuning curves. For another machine, derive the allowable field error from its own field map, RF voltage, turn count and phase-slip model, or measure it with an intensity-versus-field sweep. The transferable lesson is that the tolerance comes out in gauss rather than percent — the budget itself must be computed, not copied.
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Reference operating point of the ISU undergraduate cyclotron (1961, the source's stated operating conditions): 17,000 gauss center field, 22.5 cm dee diameter, 10 kV peak dee-to-dee (V0 = 5 kV dee-to-ground used in the calculations, per the figure annotations), dee height 2.4 cm, dee gap 1.4 cm — the 1.5 MeV machine's working parameter set, with calculations run to 11 cm radius (the companion Burns paper reports about 2 uA maximum beam current, dg-1573).
Source quote & editorial note
carried out on the Iowa State University undergraduate cyclotron which operates under the following conditions: Magnetic field strength, B0 — 17,000 gauss; Diameter of dees — 22.5 cm; Peak dee-to-dee voltage, 2V0 — 10 kv; Dee height, 2k — 2.4 cm; Dee gap — 1.4 cm
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a fully documented parameter set for a very-high-field undergraduate build — 1.7 T on a small pole is what buys MeV-class energy in 11 cm with only 10 kV of RF. The rigidity relation sets the energy-radius product (a uniform 1.7 T at 11 cm would give somewhat more than the reported 1.5 MeV; the real radial profile droops); the RF voltage sets gain per turn and phase acceptance, not the final energy. It anchors the high-field corner of the small-machine design space.
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Rose-type phase integral (as applied to the ISU cyclotron, 1961): with u = sin(theta) the phase lag, tune-down profile deltaB(r) = B1 - B(r), field index n = -(r/B)(dB/dr), and V0 the peak dee-to-ground voltage, du/dr = pi*e*r*B*deltaB*(1-n)/(2*m*V0). Integrating from the measured B(r) gives the phase-lag curve for any initial phase on the accelerating branch (-pi/2 < theta < pi/2); the modeled solution remains admissible while -1 < u < 1, u = +/-1 being the model's phase-loss boundary.
u = (pi*e/(2*m*V0)) * integral_0_to_r [ r*B*(B1-B)*(1-n) ] dr + u0, with u = sin(theta)Source quote & editorial note
du/dr = πerB∆B(1−n)/(2mV0). This equation gives the rate of change of the sine of the phase lag, θ, as a function of r and the magnetic field, B. Integration gives u = (πe/2mV0) ∫ rB∆B(1−n) dr + u0. (1) From this result the phase of the proton can be obtained at any radius if the initial phase lag and the magnetic field are known
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: this single quadrature over the measured field map predicts phase history without tracking orbits, and it runs in a spreadsheet — under the model's assumptions (nonrelativistic centered orbits, continuous acceleration, initial phase restricted to the accelerating branch). The right first tool for choosing frequency and trim before any trajectory code is written; it bounds phase admissibility only — vertical loss, radial loss and scattering are separate budgets.
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The nu_r = 2*nu_z coupling resonance at field index n = 0.2 was located at r = 10.1 cm in the ISU cyclotron (1961 calculation) and flagged as possibly responsible for major beam loss at large radii - noting that by that radius the phase-window model already put intensity low, so the two loss mechanisms overlap.
resonance where omega_r = 2*omega_z: sqrt(1-n) = 2*sqrt(n) gives n = 0.2Source quote & editorial note
When n = −(r/B)(∂B/∂r) = 0.2 a resonance condition occurs between the vertical and radial oscillations of the proton. This resonance which occurs at r = 10.1 cm in the ISU cyclotron is possibly responsible for a major loss in beam intensity at large radii ... The effect of the resonant condition, n=0.2, is difficult to determine. The resonant condition does not occur until r=10.1 cm. At this point the beam intensity is quite low already; a detailed experimental study is to be carried out later
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: compute the radius where the measured field profile crosses n = 0.2 and treat it as a resonance-warning radius — whether appreciable coupling loss actually occurs there depends on coupling strength, crossing rate, field errors and orbit centering, so confirm with tracking or a transmission measurement before writing the region off. On steep-edged small poles this radius can arrive well inside the pole edge.
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Approximation-validity verdict from full trajectory integration on the ISU cyclotron (1963): resonant couplings between axial and radial oscillations should be studied by calculating full proton trajectories, while electric-deceleration (phase-limit) questions are answered adequately by circular-orbit approximations — the expensive computation earns its cost where resonant coupling operates.
Source quote & editorial note
The conclusion is that resonant couplings between axial and radial oscillations should be studied by the calculation of proton trajectories. It is unnecessary to study electric decelerations with this method since circular orbit approximations appear to be sufficient.
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a tiered modeling strategy validated by direct comparison, not just convenience — run the cheap semicircle/phase-integral model for phase-limit questions and spend trajectory integration on the resonance region and anywhere else its assumptions break (wide fringe regions, strongly displaced starts, extraction). Benchmark the cheap model against a few full trajectories before trusting the division of labor. This sizes the orbit-code effort a small-machine project actually needs.
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Design specification (no beam yet) for the IUAC table-top teaching-cyclotron magnet — an H-frame DC electromagnet producing 1.2 T in the median plane across a 51 mm (nominal, +/-0.05 mm) pole gap with 305 mm diameter poles; pole shoes are specified removable, and one set of spare pole shoes (02 nos, drawing IUAC/CYCLO/11) is a named procurement line item.
B = 1.2 T at median plane; pole gap g = 51 +/- 0.05 mm; pole diameter = 305 mmSource quote & editorial note
[Drawing IUAC/CYCLO/11, sheet 1 of 1:] POLE TIP-SPARE ... QTY: 02 NOS ... 310.00 ... 35.00 ... Magnet steel-AISI-1010 ... 15 Kg [cf. IUAC/CYCLO/10 POLE TIP-1: 305.0 +/-0.2, 30.00 +/-0.02, 17 Kg]
IUAC, e-Tender 09/GOR/2024–25 — H-Dipole Water-Cooled DC Electromagnet for the Table-Top Cyclotron: Engineering Specification and Acceptance Tests (2024) — p. PDF pp.18 and 29 for the text (printed 18, 29); drawing IUAC/CYCLO/11 is PDF p.57 (printed 57, Annexure-L)
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a professional lab building a teaching machine chose exactly the H-frame, ~1.2 T, ~30 cm pole class that amateur cyclotrons occupy — and made removable pole shoes plus a spare set a procurement line item, the natural hedge for the shimming and re-profiling iterations small magnets commonly need. Pricing spare pole stock alongside the main steel order is insurance worth evaluating on any build.
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Field-quality design requirement for the IUAC teaching-cyclotron magnet — median-plane field homogeneity dB/B better than 18e-3 up to a radius of 120 mm (about 79 percent of the 152.5 mm pole radius), a value expected from simulation and required to be confirmed by measurement at acceptance.
Source quote & editorial note
[Magnet data table:] Field homogeneity at the median plane — better than 18 x10-3 up to radius of 120 mm (expected as per simulation) ... Field mapping in the median plane of the magnet should be carried out. Homogeneity of the magnetic field at different radial and angular positions w.r.t. the central field (B/B) shall be measured and compared with the results obtained using simulations ... Homogeneity of B/B ~18x10-3 over a radius of 120 mm of the pole is required as per design
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a design/spec number from a modern professional team for a small teaching cyclotron — 18e-3 out to ~79% of pole radius, expected from simulation and verified by mapping at acceptance. Context for what an unshimmed as-designed pole can look like, not a target to copy: derive the field-quality requirement from the machine's own phase-slip and orbit tolerances (the ISU worked example, dg-1547/dg-1588, ran at 2e-4), and give the mapping instrument resolution substantially finer than whatever criterion it must verify.
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Coil electrical design point for the IUAC 1.2 T / 51 mm gap magnet (tender specification; the table's 'Operating Current' is a design rating — the machine has no beam yet) — total magnetizing force 64800 ampere-turns from two coils of 162 turns each at 200 A, wound from 10 mm x 10 mm hollow OFHC copper (ASTM C10200) with 6 mm water bore; per the same table, one coil is about 0.05 ohm and uses about 214.5 m of conductor weighing about 135 kg, the pair runs at roughly 20 V, and I²R from the tabulated values is about 2 kW per coil.
NI = 64800 A-turns (two coils, 162 turns/coil x 200 A) for B = 1.2 T, g = 51 mmSource quote & editorial note
[Coil Data table:] Total Magnetizing force (for two coils) — 64800 Ampere-Turns; No. of coils — 02 (Top and bottom); No of turns per coil — 162; Conductor size — 10 mm x 10mm x 6 mm diameter bore (OF-OK oxygen free copper grade ASTM C10200); Operating Current — 200 A; Approximate total length of one coil — 214.5 m; Approximate weight of one coil — 135 Kg; Approximate resistance per coil — 0.05 Ohm; Approximate operating voltage (for two coils) — 20 V
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: a complete, self-consistent coil design point (ampere-turns, turns, current, conductor, resistance, voltage, mass) published with enough detail to scale from — sitting just above the 0.6-1 T fields most amateur machines run. The low-voltage high-current choice (about 20 V at 200 A for ~4 kW total) shows a water-cooled hollow-conductor solution where amateur designs often accept hotter air-cooled solid-wire coils; scaling it needs the magnetic-circuit, thermal, ampacity and hydraulic calculations redone for the new geometry.
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Yoke and pole material specification for the IUAC teaching-cyclotron magnet — low-carbon soft magnetic steel of AISI-1010 class or better, preferably machined from a single solid piece, with chemistry limits (C <= 0.1 percent, Mn <= 0.45, Si <= 0.02, N 0.005, iron balance >= 99.18 percent) and required magnetic properties of maximum relative permeability above 5000, coercive force 60-120 A/m and saturation induction 2.15 T; sample material certificates (chemistry, B-H curve, ultrasonic soundness per EN 10160 or ASTM A578) must be approved before the steel is even procured.
Source quote & editorial note
machined preferably from single solid piece of soft Iron, low carbon, high quality magnetic steel (e.g. AISI-1010 or its equivalent or better) ... [Table-2, typical chemical composition:] C ≤ 0.1%; Mn ≤ 0.450%; Si ≤ 0.02%; N 0.005%; Balance: Iron ≥ 99.18% ... [Table-3, magnetic properties:] Maximum value of relative permeability > 5000; Coercive Force 60-120 A/m; Saturation Induction 2.15 T ... The material supplier should provide (i) ultrasonic test report of supply material as per EN 10160 class S1/E1 or ASTM A578 or any applicable international standard ... the material shall be procured and utilized only after receiving the written approval from IUAC
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: concrete, checkable acceptance numbers for magnet iron — chemistry, permeability, coercivity, saturation — rather than the vague 'low-carbon steel' guidance common in amateur builds. Approving mill certificates and a sample B-H curve before purchase is a method any builder can copy when buying nominal 1010-class stock; the certificate check is what catches near-misses — common 1018 stock (0.15-0.20% C) fails this chemistry outright, and a trade designation alone guarantees neither the permeability nor the coercivity row.
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Field-computation provenance disclosed in the IUAC magnet acceptance criteria — the design field was modelled with CST Microwave Studio in 3D and the POISSON code in 2D, the measured value must match the designed 1.2 T, and the design documents are offered to the vendor for the technical discussion.
Source quote & editorial note
The designed field has been modelled with CST Microwave Studio for 3D and POISSON code for 2 D related designs. The final measured value should match the designed value of 1.2 T. Relevant documents of design can be supplied, if the vendor requires during technical bid discussion.
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: confirms that a modern professional teaching-magnet design still rests on a 2D POISSON-class solve cross-checked in 3D — the same two-tier workflow available to amateurs through free 2D field solvers plus selective 3D checks. The acceptance criterion is written against the simulation, making the model the effective contract baseline — though 'match the designed value' is stated without a numeric tolerance, which a real acceptance procedure needs.
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RF system architecture under development (no beam) for the IUAC table-top cyclotron — a broadband solid-state RF power amplifier up to 2 kW CW feeding an impedance matching network and a dee/dummy-dee accelerating structure, supervised by a GDR-based digital LLRF controller, with the stated aim of generating and maintaining high RF voltage across the dee-dummy-dee gap.
Source quote & editorial note
The development includes a broadband solid state RF power amplifier up to 2 kW CW, Impedance matching network (IMN) and GDR based Digital LLRF Controller. The aim of the RF system is to generate and maintain high RF voltage across Dee-Dummy Dee to accelerate the particles from the ion source of Cyclotron.
IUAC, Annual Report 2024–25, Chapter 3 — Research Support Facilities (table-top cyclotron RF system) — p. 18
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: the amplifier-IMN-dee chain with a digital feedback controller is the modern minimal RF architecture for a small cyclotron, and the dee/dummy-dee (single-dee) geometry matches common amateur practice. The 2 kW CW is this amplifier's rated maximum, not a derived drive requirement — the power a given machine needs follows from its dee voltage, shunt impedance, coupling and losses, so treat the rating as one professional team's headroom choice for an MeV-class teaching machine.
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Fabrication status of the IUAC table-top cyclotron chambers (no beam) — two chambers for the project are listed among the institutional mechanical workshop's completed in-house jobs for the programme year, alongside chambers and RF components for other facilities; the report states the entire requirement of machining, welding and assembly is carried out by the workshop without any outsourcing.
Source quote & editorial note
Some of the major in-house jobs that were successfully completed are; the low energy nuclear physics chamber for the High Current Injector, SS jacketing work of the spare Niobium Resonators for linac, two chambers for the Table Top Cyclotron project and several RF components like a prototype high power directional coupler, heat sinks for RF power amplifiers etc ... As of today, the entire requirement of machining, welding and assembly is fully carried out by the IUAC workshop without any outsourcing which is one of its mandates.
IUAC, Annual Report 2024–25, Chapter 3 — Research Support Facilities (table-top cyclotron RF system) — p. 36, 37
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: chamber fabrication at this machine scale is workshop-grade machining and welding, done entirely in-house by a national lab as routine job-shop work — not exotic vessel-making. Why the project consumed two chambers the report does not say (iterations, or distinct functions), so read the count as a capacity observation, not a revision history.
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Regulatory posture of the IUAC table-top cyclotron project (pre-beam) — the machine appears in the institution's AERB facility licensing-status table with status 'Initiated' (license valid till: NA), alongside the operating accelerators, and the same report records civil work for setting up a cyclotron development laboratory.
Source quote & editorial note
[Facility licensing status table — Facility / Status / License valid till:] Table Top Cyclotron — Initiated — NA (listed alongside Running facilities such as the Pelletron-linac, and the HCI facility with design construction approval) ... Civil work for setting up of the cyclotron development laboratory and storage racks.
IUAC, Annual Report 2024–25, Chapter 3 — Research Support Facilities (table-top cyclotron RF system) — p. 23, 37
Editorial note, tabletop extrapolation: Editorial note, tabletop extrapolation: method observation, not a dose rule — the machine sits in the regulator-facing facility-status table from project initiation, so authorization proceeds in parallel with construction rather than gating it at the end. What 'Initiated' commits either party to, the table does not define; the transferable habit is the early appearance itself. Small-accelerator builders in any jurisdiction can copy the early-engagement pattern.
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Practical RF power limits reported for the Rutgers 12-inch cyclotron: about 500 watts is the amount that can be safely used for prolonged operation, 1 kW has been tried only for very brief periods of about 30 seconds, and those powers corresponded to approximately 10 kVp-p and 11 kVp-p on the DEE respectively (500 W and 600 W).
Source quote & editorial note
Presently, the practical amount of RF power that can be safely used for prolonged operation is about 500 watts. Operating with power levels on the order of 1kW have been tried, but only for very brief periods (30 seconds). […] The first betatron image (left sinusoidal pattern) is of 500 watts and the second (right sinusoidal pattern) was with 600 watts of RF power. The RF power of 500 watts corresponded to approximately 10 kVp-p and 600 watts corresponded to approximately 11 kVp-p.
Koeth, Hanebuth, Hoffman & Schneider, Rutgers 12-Inch Cyclotron Ion Source Studies: Part II (2007) — p. 3
Editorial note, tabletop extrapolation: A scale-matched RF data point: about 500 W forward power buys ~10 kVp-p on this 12-inch dee in this resonator, stated by the authors as their prolonged-operation practice; 1 kW was ATTEMPTED for ~30-second periods (~11 kVp-p at 600 W per the same figure). The source does not say what sets the limit — heating, breakdown, matching components — so read the numbers as one resonator's operating envelope, not as permission for pulsed operation at double power.
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Two geometric limits marked on the Rutgers 12-inch SIMION launch-height scan (Fig. 9): the DEE lid is at a height of 36 mm, and the beam blows up at a radius of r = 110 mm, which is where the n = 0.2 resonance resides.
Source quote & editorial note
Fig. 9 Differing ion launch heights simulated in SIMION, green dots are location of measured peaks and valleys (dots heights are not representative of data height). Note height of DEE lid is at 36 mm. Also note beam blow up at r = 110 mm, this is where n = 0.2 resonance resides, see reference [2].
Koeth, Hanebuth, Hoffman & Schneider, Rutgers 12-Inch Cyclotron Ion Source Studies: Part II (2007) — p. 4
Editorial note, tabletop extrapolation: Both numbers are read from the figure and its caption. The transferable point is the method it illustrates: the useful radius of a weak-focusing machine is bounded not by the pole edge but by where the field index reaches a resonant value — on THIS machine, n = 0.2 at r = 110 mm of a 152 mm pole radius, and the simulation blows up there. Map your own n(r), find your own resonance radii, and place target and deflector inside the demonstrated usable radius; where n = 0.2 lands is your taper's choice (dg-1729).
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Geometry of the Rutgers 12-inch cyclotron electrostatic deflector: a thin curved grounded sheet formed the septum separating the accelerating volume from the deflection channel, with a slightly greater-curved HV electrode arranged concentrically to give an average 0.31 inch gap; the deflector tangentially intercepted the spiraling beam at a radius of 4.0 inches and transported it to a radius of 4.5 inches in 43 degrees of azimuth, the channel having a nominal radius of curvature of 7 inches.
Source quote & editorial note
A thin, curved, grounded sheet formed the septum and separates the main accelerating volume and the deflection channel. A slightly greater curved high voltage (HV) electrode was concentrically arranged to complete the deflection channel with and average 0.31 inch gap spacing. The deflector tangentially intercepted the spiraling cyclotron beam at a radius of 4.0 inches and transported the beam to a radius of 4.5 inches in 43° of azimuth. The deflection channel had a nominal radius of curvature of 7 inches.
Editorial note, tabletop extrapolation: The most fully dimensioned extraction geometry in the amateur literature at this scale — a 12-inch machine intercepting at 4.0 inches. As orientation: the channel's radius of curvature is 1.75× the orbit radius, the gap ~7.5% of the orbit radius, and the channel spans 43° to gain 0.5 inch (ratios computed here). Applying those ratios to another machine is geometric illustration only — rigidity, turn separation, septum thickness and fringe fields all enter — so recompute the field and voltage (dg-1660) and verify by tracking before cutting metal.
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Working design equation for an electrostatic deflector embedded in a cyclotron field, as derived and used on the Rutgers 12-inch: the required transverse electric field follows from the difference of reciprocal bending radii, and the electrode potential is that field times the electrode-septum gap. Numerically, for protons in a 1.0 Tesla field going from rho_0 = 4.0 inches to rho_1 = 7.0 inches, E = 4.2 MV/m, and with a nominal 0.31 inch gap that sets the electrode voltage at 33 kV.
|E| = (q*B^2*rho_0^2/m)*(1/rho_0 - 1/rho_1) = (2T/q)*(1/rho_0 - 1/rho_1) for rho_1 > rho_0 (the field opposes the magnetic bending; the source writes the difference in the other order, which under its convention is a signed value); V = |E| * dSource quote & editorial note
This determines the necessary electric field; we must multiply the electric field by the HV electrode-septum gap spacing to determine the required applied potential. Using the values of ρo and ρ1 listed above, we find that for protons in a 1.0 Telsa magnetic field, a transverse electric field of 4.2 MV/m is required. The nominal electrode-septum spacing is 0.31 inches, thereby setting the electrode voltage at 33 kV.
Editorial note, tabletop extrapolation: The sizing equation a tabletop extraction design starts from, checked against the printed numbers: with rho_0 = 0.1016 m, rho_1 = 0.1778 m the magnitude comes to 4.17 MV/m, and times 0.31 inch gives 32.8 kV — agreeing with the printed 33 kV (computed). Scaling: with field scaled by b and ALL lengths by s, the required field goes as b²s and the voltage as b²s² — so half the field at two-thirds scale needs ~1/6 the field and ~1/9 the voltage, which is what makes a modest HV supply workable on a smaller machine. ("Telsa" is the source's typo for Tesla.)
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Off-harmonic operation observed and rationalized on the Rutgers 12-inch: because a cyclotron only resonantly accelerates at odd integer harmonics, operating near but not on an odd harmonic can still give a successfully accelerated beam provided the integrated phase slippage over all revolutions is less than 180 degrees before the target or extraction point — and since higher DEE voltage means fewer revolutions to reach a given energy, the tolerable phase slippage per turn increases with DEE voltage.
Source quote & editorial note
This result is not understood, as only integer odd harmonic numbers support magnetic resonance acceleration. At an even harmonic, when acceleration occurs at a gap crossing, deceleration must occur at the subsequent crossing, yielding zero net accelerator per revolution. In the region between an even and odd harmonic, there is a balance of acceleration and phase slippage which the ions encounter. Operating a cyclotron near, but not on, an odd harmonic, can still lead to a successful resonantly accelerated beam, provided that the integrated phase slippage over all revolutions is less than 180 before hitting the target or extraction point. The greater the DEE voltage, the fewer the number of ion revolutions are needed to achieve the desired energy, thus the tolerance of phase slippage per turn increases with DEE voltage.
Editorial note, tabletop extrapolation: Directly relevant to low-dee-voltage machines, in mirror image: many hundreds of turns means very little tolerable slip per turn, which is an operational argument for dee voltage beyond simple turn-count. State the physics as the source's gap phasing gives it: odd harmonics are the resonant condition for this conventional geometry, and near-harmonic operation can survive if the bunch stays inside the accelerating phase window — the 180-degree integrated-slip figure is an approximate span, conditional on where in phase the ions start and which way they slip. The reported 2.22 and 4.25 harmonic numbers are stated by the authors as "not understood" — an open anomaly, not a result. ("accelerator per revolution" is the source's typo for "acceleration".)
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The Rutgers 12-inch cyclotron's first pole tips were Blanchard-ground parallel to better than 1 part in 10,000 to satisfy the cyclotron resonance condition; the resulting purely vertical field gave no axial weak focusing — the source attributes the loss of nearly all ions to the dee's top and bottom plates — and delivered less than a nanoampere to the periphery during commissioning, against a program goal of at least 10 microamps.
Source quote & editorial note
Initially, to satisfy the cyclotron resonance condition, the pole tips of the 12-Inch Cyclotron magnet were Blanchard ground to provide parallelism to better than 1 part in 10,000. As will be seen, this pure vertical field does not provide any beam focusing effects, all but a very few of the generated ions are lost on either the top of bottom plate of the DEE. Indeed, during commissioning of the cyclotron, only a trickle of beam current, less than a nano-ampere, made it to the periphery. Desiring beam currents of at least 10µA in intensity, a program to study and modify the cyclotron to achieve this goal is under way.
Editorial note, tabletop extrapolation: The canonical educational-machine failure mode, and a machining-quality trap in reverse: extreme pole parallelism is exactly what leaves the beam without an axial restoring force (radial stability, with tune near 1, survives — it is the vertical plane that empties into the lids). The sub-nA periphery current is this machine's measured commissioning figure, a realistic 'before' anecdote rather than a class-wide baseline; the 10 µA goal is the authors' aspiration, not an achieved value anywhere in this document.
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The Rutgers 12-inch weak-focusing retrofit was a simple linear pole-tip taper specified for an overall 2% decrease of Bz, implemented as a magnet gap opening from 2.010 inches at r = 0 to 2.018 inches at r = 5.0 inches (the maximum ion radius), machined from soft 1006 iron with azimuthal symmetry about r = 0.
Source quote & editorial note
After much debate, a simple linear tapered pole tip design with an overall 2% decrease of Bz was settled upon. The magnet gap was to increase radially, starting from a minimum of 2.010 inches at r = 0 to 2.018 at r = 5.0 inches, the maximum possible ion radius. The author obtained the needed soft 1006 iron material. The pole tips were machined with azimuthal symmetry about r = 0.
Editorial note, tabletop extrapolation: The Rutgers retrofit geometry, fully dimensioned: a 0.008-inch gap opening (computed: 2.018 − 2.010) over 5 inches of radius on a ~2-inch gap, cut in soft 1006 iron, targeting a 2% Bz droop. Two readings for your own design: the tolerance implication — pole-face errors must be small against 0.008 inch or they swamp the intended index — and the method: calculate or map YOUR Bz(r), derive n(r), and iterate by shim or re-cut, because the field response to a given taper belongs to the whole magnetic circuit, not the taper alone. The 2% is the design target; the source's own profiles fall considerably more by r = 5 inches once pole-edge fall-off is included.
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The Rutgers 12-inch magnet study warns that coupled transverse resonances further restrict the field index beyond 0 < n < 1, listing 0.2, 0.25, 0.33 and 0.5 as values to avoid, and derives the design consequence that the radial rate of Bz decrease must be moderated so that the machine only approaches 0.2 near the maximum ion radius.
Source quote & editorial note
For details beyond the scope of this document, coupled resonances between the transverse motions further limit the value of n. n values of 0.2, 0.25, 0.33, 0.5 (and others higher) need to be avoided. Since, the ions to be accelerated begin at r = 0, n = 0 and will only climb as the radius increases. If n = 0.2 needs to be avoided, then the rate at which Bz decreases must be moderated such that only near the maximum ion radius does n approach 0.2.
Editorial note, tabletop extrapolation: Actionable sizing constraint for a taper design: it converts 'make the field droop' into 'droop slowly enough that the low-order resonances arrive only at the very end of the spiral.' The printed n list is physically standard — at n = 0.2 the tunes satisfy νr = 2νz (the Walkinshaw difference coupling), at 0.25 νz = 1/2, at 0.33 νr = √2·νz, at 0.5 νr = νz (all computed from νz = √n, νr = √(1−n)). Note the same document's p.7 attaches 0.2 and 0.5 to νz instead — the source is loose with its labels across pages, so identify resonances from BOTH tunes computed off your own n(r), never from a symbol's name.
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Radial Bz scans of the Rutgers 12-inch tapered pole tips at three excitations produced linear fits of y = -0.0025x + 0.7587 (R2 = 0.9862) at 20 A, y = -0.0033x + 1.029 (R2 = 0.9846) at 30 A, and y = -0.0039x + 1.1624 (R2 = 0.9846) at 40 A, with x in inches and y in tesla — 0.271 T gained from 20 to 30 A but only 0.133 T from 30 to 40 A, showing iron saturation.
Bz(r) [T] = 1.1624 - 0.0039 r[in] at 40 A; 1.029 - 0.0033 r at 30 A; 0.7587 - 0.0025 r at 20 ASource quote & editorial note
Linear Fit to Tapered Pole Tips' B-field at 3 Coil Currents ... y = -0.0039x + 1.1624 R² = 0.9846 ... y = -0.0033x + 1.029 R² = 0.9846 ... y = -0.0025x + 0.7587 R² = 0.9862 ... Fig.1 Radial measurements at three different magnet currents: 20, 30, & 40A
Editorial note, tabletop extrapolation: Hard numbers for a real 12-inch H-frame's excitation curve: about 0.76 T at 20 A, 1.03 T at 30 A, 1.16 T at 40 A — the tesla-per-amp halving between steps (0.0271 vs 0.0133 T/A) is THIS iron's saturation announcing itself. Computed honestly with P = I²R at fixed resistance: the 30→40 A step buys its 0.133 T at about 2.85× the incremental copper power per tesla of the 20→30 A step (700R/0.133 versus 500R/0.271). The fit slope is the normalized radial FIELD gradient, about −0.34% of central field per inch at 40 A — not the physical pole-taper angle. Where another magnet's payback ends is its own B(i) curve's business. (Fit values and R² read from the rendered Fig. 1; the 20/30/40 A assignment follows the curve intercepts, since the printed legend order is 30, 20, 40.)
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The Rutgers 12-inch geometry landmarks used throughout its field analysis are r = 0 (centre), r = 5 inches (maximum ion radius), r = 6 inches (pole tip edge) and r = 8 inches (reference point), with nominal magnet operation at about 32 amperes.
Source quote & editorial note
Fig.2 Simultaneous normalized field plot of the three current values: 20, 30, and 40 Amperes. The vertical dashed lines indicate, r = 0 – the center, r = 5 – the maximum ion radius, r = 6 – the pole tip edge, and r = 8 – the reference point. … Nominal magnet operation is about 32 amperes.
Editorial note, tabletop extrapolation: A concrete radius budget from one as-built machine: the beam uses 5 of the 6 inches of pole radius — the outer inch is where this pole's field rolls off — with nominal operation about 32 A. How much pole another machine must reserve depends on its gap-to-pole ratio, shaping and uniformity requirement: derive it from a field model or map rather than transplanting the 5/6 fraction.
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On the Rutgers 12-inch, a 1.2 MeV proton machine with no appreciable relativistic mass increase, weak focusing is stronger than pure Thomas (unspiralled AVF) focusing — from the study's own tune comparison, near the 12.7 cm maximum ion radius the weak-focusing nu_z is about 0.7 while pure Thomas focusing gives only about 0.07 — because a non-relativistic machine can use a falling field and does not need the rising field that makes AVF necessary in larger cyclotrons.
Source quote & editorial note
The pink trace (lowest) in Figure 15 displays the sole effect of Thomas focusing, - AVF focusing without a spiral edge. It is interesting to note that in our case, weak focusing is in fact stronger than the colloquially termed AVF “strong focusing.” This peculiararity arises from the fact that our small (1.2MeV) cyclotron does not noticeably suffer from relativistic effects. If it did, the magnetic field would need to increase with radius, as opposed to our decreasing field, in order to keep the more “massive” ions in step with the RF.
Editorial note, tabletop extrapolation: The qualitative result matters for a 100 keV-1 MeV machine and cuts against the modern instinct: with no relativistic detuning to fight, a non-relativistic machine may use a FALLING field, and this study found its tapered weak focusing stronger than its unspiralled Thomas alternative. No numeric ratio should be carried: Fig. 15's ordinate is printed 'field index - n' while text and caption call it νz, and its weak-focusing trace disagrees with the p.6 νz ≈ 0.7 value — if the plotted quantity were νz² the tunes would be its square roots — an internal inconsistency of the source, flagged. AVF earns its complexity when a rising (isochronous) field is needed, and can still be chosen at low energy for acceptance or tune control; this machine's own later spiral tips (dg-1745) are that choice made deliberately.
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Adding a spiral edge to AVF sector tips raises the axial tune extremely fast: in the Rutgers 12-inch study the slight-Archimedean-spiral design reaches nu_z = 1 by about 7 cm radius, and the author judges a spiral edge unfavourable on that machine because of the destructive instability at nu_z = 1 and further serious instabilities at nu_z = 0.2 and 0.5.
Source quote & editorial note
The light green trace (left and uppermost trace) in Figure 15 corresponds to the pole tip design shown in Figure 14. It is clear that νz grows very rapidly with even a slight spiral. Because of the cataclysmic beam instability at νz = 1, and other serious instabilities at νz = 0.2, 0.5 and so on, use of a spiral edge does not does not seem favorable.
Editorial note, tabletop extrapolation: A caution, not a verdict, on spiral sectors at small radius: THIS slight-Archimedean design's modeled tune ramped so fast (νz = 1 by ~7 cm, read from the rendered Fig. 15's varchimedes trace) that the author judged spiral edges unfavourable for the machine, citing the νz = 1 instability and lines at 0.2 and 0.5. Whether a small pole has room to spread the ramp depends on sector count, flutter and spiral angle: plot the full tune trajectory against the resonance lines for YOUR field map and track through any crossing — the same group's 2011 study did exactly that and built a working 270° spiral (dg-1745), so treat this page as one design iteration's lesson.
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For the Rutgers 12-inch AVF work the axial tune is written nu_z^2 = -k + F(1+tan^2 xi) and the radial tune nu_r^2 = 1+k, where k = d ln<B> / d ln R is the average field index, F is the rms flutter (the rms azimuthal variation of the vertical field) and xi is the instantaneous angle the sector edge makes with the orbit.
nu_z^2 = -k + F(1+tan^2 xi); nu_r^2 = 1+k; k = d ln<B> / d ln RSource quote & editorial note
AVF focusing can be used to supplement weak focusing. In this context, the weak focusing comes from the average radial gradient’s field index, denoted as k, where: k = d ln〈B〉/ d ln R . The tune is proportional to the relative focusing strength. Following the treatment of J.J. Livingood,[6] one can write the axial tune in terms of the average field index, flutter, and the instantaneous edge angle: νz² = -k + F(1+tan²ξ) The radial tune is written as νr² = 1+k … The rms variation of the vertical field is called flutter and is denoted as F. The azimuthal magnetic field component, Bθ, is also proportional to the flutter.
Editorial note, tabletop extrapolation: The design equation for combining a weak-focusing taper with AVF sectors, showing the two contributions add. Two convention traps, both resolved here: (1) this paper calls F 'the rms variation' — for the linear-in-F tune formula to be the standard Livingood form, F must be the MEAN-SQUARE fractional variation ⟨((B−⟨B⟩)/⟨B⟩)²⟩, i.e. the square of the rms fraction, exactly as the same program's later paper defines it (F² there = ⟨…²⟩, tune quadratic in its F; dg-1746) — reconcile against Livingood before numeric use; (2) k = d ln⟨B⟩/d ln R is NEGATIVE for a falling field, opposite in sign to the magnet study's n, so n = −k. The tan²ξ factor is why edge angle is a powerful and dangerous knob — it grows without bound (dg-1697).
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The Rutgers 12-inch group deliberately built a first, non-beam benchmark set of AVF pole tips — a pure radial-sector design of periodicity four, chosen as the least expensive geometry to machine and the one giving maximum field variation achievable within practical constraints — with no expectation of accelerating beam in it, purely to benchmark the simulations, the measurement technique and the analysis code.
Source quote & editorial note
The first set was a simple, pure-radial sector design of periodicity four. Their geometry was the least expensive to machine and provided the maximum field variation achievable within practical constraints. Not expected to host beam, their purpose was to benchmark simulations, measurement techniques, and test analysis code.
Editorial note, tabletop extrapolation: A process rule worth more than most hardware numbers: build the cheap, geometrically simple article first and use it to shake down the toolchain — solver, field mapper, analysis scripts — before spending shop time on the expensive curved part. The radial set rehearses most of the pipeline; what it cannot validate is the spiral-specific machining and edge-field modeling, which the real article still tests (the sequence that produced AKG270, dg-1717).
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The Rutgers 12-inch trial radial-sector AVF tips had four sectors with hills and valleys each 45 degrees wide, constant thickness out to the pole edge except for a 1/4 inch chamfer breaking the sharp corners, and a central slug tying the four vanes together; that slug's field bump is deliberate weak focusing, needed because the flutter is too small to focus at the central convergence.
Source quote & editorial note
The first set of AVF pole tips measured were of the simplest design, and are shown installed with the cyclotron chamber removed in figure 10. With a periodicity of four, the hills and valley are each 45 degrees wide. They maintain a constant thickness out to the pole edge, except for a ¼ -inch chamfer to break the sharp corners. The data from the first scan is plotted in Figure 11. The four hills are prominent, however a small central bump is observed from the slug that ties the four vanes together. This weak focusing is required to promote a centrally localized focusing field since the flutter will be too small to be effective at the central convergence.
Editorial note, tabletop extrapolation: The geometry as stated (four sectors, 45-degree hills and valleys, constant thickness, 1/4-inch chamfer, central slug) plus the central-region insight that matters most at small scale: flutter vanishes at r = 0, so a pure-AVF machine has no SECTOR focusing where ions are born — this design's central slug supplies a deliberate weak-focusing bump there, and the source states that requirement for its own field. Evaluate your own central region's full focusing budget (magnetic index plus RF-gap electric focusing and phase) rather than assuming the bump; most small AVF designs end up wanting one (the AKG270 kept it, dg-1717).
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On the Rutgers 12-inch radial-sector AVF tips the azimuthal field variation emerges as a smooth sinusoid despite the square stepped hill-to-valley transitions of the iron, and a flat top only becomes apparent at radii of 4 inches and greater.
Source quote & editorial note
Figure 12 plots Bz(θ) over one quadrant displaying the relative evolution of the flutter with radius by individually plotting Bz(θ) for sixteen radii. The plot shows the emerging sinusoid flutter, despite the square stepped transitions between hills and valleys. Only for radii of 4-inches and greater does a ‘flat-top’ become apparent.
Editorial note, tabletop extrapolation: An instructive measured fact about gap smoothing: square-cut sector iron produced a nearly sinusoidal Bz(θ) on this pole, with a flat top emerging only beyond 4 inches radius. The general lesson is that the gap filters sector geometry hard — machining need not chase a shaped profile blindly — but how much smoothing, where the designed flutter amplitude arrives, and what harmonics survive are set by gap-to-sector-width and radius ratios: solve or map YOUR geometry and take the flutter spectrum from that, rather than scaling this 4-inch mark by pole size.
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The Rutgers 12-inch AVF simulation toolchain was SolidWorks for the mechanical magnet model, Maxwell 3D for the field solution and field report, SIMION for ion flying and tracking, and MatLab for post-processing; Maxwell 3D was first benchmarked against the existing 2-D Poisson/Superfish weak-focusing model at a nominal 1 T peak central field and agreed to within measurement errors.
Source quote & editorial note
SIMULATIONS Form start to finish, four software tools have been employed to simulate the beam dynamics of in these magnetic fields. SolidWorks was used to mechanically model the magnet, Maxwell 3D was uses to solve the field problem and generate the needed field report for SIMION to fly and track the ions in. Post processing was performed in MatLab. ... Maxwell 3D (M3D) was first benchmarked against our weak focusing PSF simulations. A 3-D magnet model, which included the weak focusing pole tips was designed in SolidWorks and then imported into Maxwell 3D. The problem was solved to have a nominal peak central field of 1 Tesla. To within measurement errors the models agreed.
Editorial note, tabletop extrapolation: A four-stage pipeline — CAD, 3-D field solver, tracker, analysis — with the transferable discipline being the BENCHMARK step: before trusting the 3-D solver on new geometry, reproduce the old validated result on the old geometry (here Maxwell 3D reproduced the Poisson/Superfish weak-focusing field within measurement errors — the FIELD model, not the tracking chain, is what that comparison validates). Free-tool substitutions: FEMM only where a planar/axisymmetric approximation is defensible — a radial-sector AVF field is intrinsically 3-D, so budget for Elmer or another 3-D solver there — and verify the field-transfer and tracking layers separately (dg-1712's trap).
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Two protons launched with identical initial conditions on their equilibrium orbits at 50 keV in the Rutgers 12-inch showed the maximum vertical excursion in the weak-focusing field to be nearly four times that in the radial-sector AVF field — about plus/minus 9 mm versus about plus/minus 2.5 mm from the mid-plane — which the authors read as permitting either a drastically reduced magnet gap or a larger accepted vertical angular distribution.
Source quote & editorial note
As is seen in Figure 20, the maximum vertical excursion of the proton in the weak field was nearly four times that of the proton in the radial sector AVF field. This has two immediate implications. First, to accommodate a given ion source, the magnet gap of AVF field can be drastically reduced, implying a smaller and less expensive magnet. Alternatively, the magnet gap can be maintained, and a greater vertical angular distribution can be accepted, implying greater beam intensity at the periphery.
Editorial note, tabletop extrapolation: The clearest quantitative case for AVF at this scale, kept to what the simulation shows: one proton, identical launch, ±9 mm excursion in the weak-focusing field versus ±2.5 mm in the radial-sector field (read from the rendered Fig. 20; 'nearly four times' is the authors'). The source's two implications — a drastically reducible gap, or more accepted vertical angle — are design directions whose actual payoff needs full acceptance tracking and a self-consistent magnet redesign, since gap changes move excitation and field structure together. Note the apparent tension with the same program's finding that its weak-focusing νz exceeds its Thomas-field νz (dg-1696): tune and single-trajectory excursion are different measures, and the Fig. 15 labeling problem (same card) leaves the tune comparison unresolved.
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The Rutgers 12-inch optimized spiral tips, designated AKG270, are a four-sector Archimedean spiral sweeping 270 degrees from centre to periphery, designed to satisfy the isochronous condition everywhere except a deliberately retained weak-focusing central region, in order to minimize phase slippage and reduce the minimum dee voltage while preserving axial stability.
Source quote & editorial note
SPIRAL AVF DESIGN Finally, we present the optimized design for a set of spiral pole tips that are intended to guide beam. The result was a four sector Archimedean spiral sweeping 270 degrees, and will herein be referred to as AKG270. With the exception of the weak focusing central region, these pole tips aimed to satisfy the isochronous condition, in order to minimize the phase slippage, and reduce the minimum DEE voltage while preserving axial stability throughout the accelerating region.
Editorial note, tabletop extrapolation: The design pattern worth copying is the HYBRID: weak focusing kept in the centre where flutter cannot help, spiral-AVF outboard where isochronism pays — that is what minimized phase slippage and dee voltage while preserving axial stability here. The 270-degree four-sector Archimedean sweep is this magnet's optimized answer (the authors credit their machine shop for cutting it); another machine re-runs the optimization on its own field map and takes whatever sweep its tunes demand.
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Iteratively tuning drive frequency and amplitude in SIMION for the Rutgers 12-inch AKG270 spiral field found the lowest dee voltage that still delivered a proton to the target to be 6 kV-peak at 15.534 MHz — below the machine's normal 8 kV-peak operating point and well below the 20 kV-peak needed by the non-isochronous radial-sector field.
Source quote & editorial note
Protons were flown with RF in SIMION with the AKG270 magnetic field. The trajectory of a single proton is shown in Figure 21. The driving frequency and amplitude were iteratively tuned to locate the minimum peak DEE voltage necessary to successfully accelerate the proton to the target. This lowest practical voltage found in the simulation was 6 kVpeak at a frequency of 15.534 MHz.
Editorial note, tabletop extrapolation: Quantifies the payoff of designing for isochronism, within one simulation campaign: 6 kV-peak at 15.534 MHz sufficed in the AKG270 spiral field, versus the 20 kV-peak the non-isochronous radial-sector field needed and the machine's normal 8 kV (both from the same study's radial-sector section, dg-1716). If shunt impedance and loading were unchanged, cavity loss ∝ V² would differ by ~11× between 6 and 20 kV — a conditional estimate, computed here. The frequency checks: 15.534 MHz ↔ ~1.02 T for protons at the fundamental (computed). Field shaping as a lever on the RF budget is the transferable idea; single-particle simulation, not measured beam.
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The average median-plane field of the Rutgers 12-inch weak-focusing pole tips, as read from the rendered Fig. 6 (y-axis <Bz> [Tesla]), falls only about 1.3% from 1.092 T at r = 0.5 inch to 1.078 T at r = 3.5 inches, then drops to 1.039 T at r = 4.5 inches and 0.955 T at r = 5 inches — about 12.5% total (computed: (1.092−0.955)/1.092), with most of the total decrease concentrated in the outer inch and a half; the paper's own text establishes that for the axisymmetric case the average field index k equals the instantaneous n.
Source quote & editorial note
The average radial field profile, plotted in figure 6, is generated from the assembled average fields along the radius – this is needed to calculate the average field index, k. In the case of the axisymmetric weak focusing field, the average field index is the same as the instantaneous field index, n.
Editorial note, tabletop extrapolation: Explains the tune shape the companion magnet study reported — near-zero νz to mid-radius, then a fast rise — and warns a designer who sizes a taper analytically: this machine's DESIGNED taper was a 2% droop (dg-1680), while the delivered profile falls ~12.5% by r = 5 inches because the pole-edge roll-off dominates the last stretch. Field index is the LOCAL derivative, not the accumulated drop — differentiate the measured profile to get n(r), and expect the edge, not the taper, to own the outer-radius focusing.
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Transverse stability in a weak-focusing cyclotron requires 0 < n < 1 for the field index n = -(r/B)(dB/dr); the author's design guidance is that because ions start at r = 0 with n = 0 and n only climbs with radius, the rate at which Bz falls must be moderated so that n approaches 0.2 only near the maximum ion radius. Coupled transverse resonances at n = 0.2, 0.25, 0.33 and 0.5 (and higher) are to be avoided.
n = -(r/B)(dB/dr); 0 < n < 1Source quote & editorial note
For details beyond the scope of this document, coupled resonances between the transverse motions further limit the value of n. n values of 0.2, 0.25, 0.33, 0.5 (and others higher) need to be avoided. Since, the ions to be accelerated begin at r = 0, n = 0 and will only climb as the radius increases. If n = 0.2 needs to be avoided, then the rate at which Bz decreases must be moderated such that only near the maximum ion radius does n approach 0.2.
Editorial note, tabletop extrapolation: The direct pole-tip taper criterion for a small weak-focusing machine: shape the taper so n approaches 0.2 only near maximum ion radius — under the author's stated premise of a profile whose n starts at 0 and only climbs. The resonance list (0.2, 0.25, 0.33, 0.5 and higher) is the author's claim, referred to Livingood for derivation, not a measurement from this machine; the field-index definition and 0 < n < 1 stability window are standard weak-focusing results stated here for context.
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Vertical (axial) betatron tune is nu_z = sqrt(n) and radial tune is nu_x = sqrt(1-n); therefore one full vertical betatron oscillation takes 1/sqrt(n) RF periods (ion revolutions). The Rutgers author's radial-stability note is that the smaller the n value the greater the radial restoring force, with no lower bound on n for radial stability, only n < 1.
nu_z = sqrt(n); nu_x = sqrt(1-n); T_beta-vert = (1/sqrt(n)) T_0Source quote & editorial note
We recall from section II that the vertical betatron frequency follows the square root of the field index multiplied by the RF frequency: f_beta-vert = sqrt(n) f_0 We extend that relationship to their respective periods of oscillation: T_beta-vert = (1/sqrt(n)) T_0 Thus for a given n it take 1/sqrt(n) RF periods or ion revolutions to complete one vertical betatron oscillation.
Editorial note, tabletop extrapolation: The hand calculation that tells a builder how many TURNS per vertical oscillation to expect: 1/√n turns (equal to RF periods only on fundamental-harmonic operation, h = 1, as here; at harmonic h it is h/√n RF cycles). With this machine's measured n ≈ 0.025-0.042 near 8.6-9.7 cm, that is about 4.9-6.3 turns per oscillation — a local estimate where n varies. The quote's equation glyphs are transcribed in plain-text form here. (The nu_x = sqrt(1-n) statement and the radial-stability remark are on p.2; the nu_z material is on p.6.)
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The measured and Poisson-Superfish-modeled field index of the Rutgers 12-inch magnet with tapered pole tips runs from 0 to about 0.2 throughout the useful ion-acceleration region; the published geometry markers are r = 0 the center, r = 5 inches the maximum ion radius, r = 6 inches the pole tip edge, and r = 8 inches the reference point.
Source quote & editorial note
The following measurements and modeling indeed confirm, at least in the assumption of azimuthal symmetry that our 12-inch magnet's field index runs from 0 to about 0.2 throughout the useful region for ion acceleration.
Editorial note, tabletop extrapolation: Reference-machine geometry, not a target: on this 12-inch, maximum ion radius 5 inches sits an inch inside the 6-inch pole-tip edge, and the measured-and-modeled n runs 0 to about 0.2 across the acceleration region. Choose your own pole margin from magnetic modeling of your taper (the fringe rolls off inside the physical edge), and read 'about 0.2' as where THIS profile tops out — the design doctrine of keeping the 0.2 crossing near final radius is carried by dg-1729/dg-1835. The r = 5/6/8 inch markers are read from the Fig. 2 caption on the same page.
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The Rutgers 12-inch ion source improvement was a chimney around the biased filament: it lets thermionic electrons follow the vertical field lines to the median plane while ionizing hydrogen, and enclosing the gas in the filament/chimney volume improved vacuum performance. A 1/16-inch aperture in the chimney wall, at the height of the median plane, launches the protons directly into the dee.
Source quote & editorial note
The ion source chimney allows thermionic electrons to freely leave the biased filament following the vertical magnetic field lines to the median plane all the while ionizing hydrogen. Admission of hydrogen gas to the enclosed volume of the filament and chimney improved vacuum performance. A 1/16-inch aperture in the chimney wall located at the height of the median plane launches the protons directly into the DEE as pictured in figure 6.
Editorial note, tabletop extrapolation: Two benefits from one part: local gas confinement (less load on a small pump) and a defined emission aperture at the median plane. The 1/16-inch aperture is this machine's as-built dimension — a reference point, with the right size for another source set by its extraction optics and gas-conductance budget (the same program's later aperture sweep, dg-1814, is the method).
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A calculation for the Rutgers 12-inch (from the ion-source model) put the RF power needed for the first ion revolutions to clear the source chimney at 165 watts when operating at 14.900 MHz; the model was confirmed on the bench by establishing beam at 300 watts and slowly reducing RF power — beam intensity fell with power and then dropped abruptly to zero at 170 watts.
Source quote & editorial note
It was calculated that the required RF power for the first revolutions of ions to clear the chimney (with the cyclotron operation at 14.900MHz) was 165 watts as plotted in figure 7. [4,7] Confirmation of the ions source model came from establishing beam with 300 watts of RF power and slowing decreasing RF power. Beam intensity decreased with decreasing RF power, but at 170 watts the beam current abruptly dropped to zero.
Editorial note, tabletop extrapolation: A rare validated model-vs-measurement pair at this scale: predicted 165 W first-turn chimney-clearance threshold, measured abrupt cutoff at 170 W. Diagnostic reading: beam that fades then DROPS to zero as RF power falls, near a modeled clearance threshold, is consistent with the first turn striking the source structure — check dee voltage, RF stability, source output and tuning before assigning the cause, since phase-acceptance loss and resonator instability can also end beam abruptly.
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On the Rutgers 12-inch, the RF-shielding cap on the original Faraday cup was thicker than the turn-to-turn spacing of the ion revolutions beyond a radius of 2.1 inches (at 14.900 MHz with a dee voltage of 7,500 Vp-p), so ions returned to chassis ground instead of reaching the sensitive collector. The fix was an unshielded aluminum block collector plus, externally, a notch filter with -100 dB of rejection at 14.900 MHz and an RF choke in the electrometer line.
Source quote & editorial note
This caps thickness was greater than the turn-to-turn spacing of the ion revolutions at a radius greater than 2.1 inches when operating at 14.900MHz with a DEE voltage of 7,500 Vp-p. Such a thick tip would prevent the ions from hitting the sensitive portion of the ion collector, rather the ions would just return to chassis ground. A new, simpler, Faraday cup was installed. It simply consists of an unshielded aluminum block. RF suppression was still a concern, so externally a notch filter, with -100dB of rejection at 14.900MHz, was installed in the Faraday cup line that connects to the electrometer. An RF choke was also installed in this line, just before the electrometer connection.
Editorial note, tabletop extrapolation: A specific, easily repeated mistake: a grounded shield that projects into the incoming beam path intercepts ions before the collector once its effective radial thickness exceeds the local turn spacing — compute Δr(r) (dg-1740) before designing any probe tip. This machine's solution moved RF rejection out of the vacuum entirely (bare aluminum block collector; -100 dB notch filter plus RF choke in the electrometer line); suitably thin or recessed in-vacuum guarding remains an option the memo simply did not need.
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Turn-to-turn radial spacing in a classical cyclotron follows Delta_r(r) = Delta_E m / (q B^2 r), where Delta_E in eV is just the dee peak-to-peak voltage; for the Rutgers 12-inch at 300 W / 14.8640 MHz / B = 0.977 T with 7,500 Vp-p on the dee this evaluates to Delta_r(r) = 8.2E-5 / r (SI, metres).
Delta_r(r) = Delta_E*m/(q*B^2*r); here = 8.2E-5/r [m]Source quote & editorial note
Operating at 300 Watts of RF power on resonance at 14.8640 MHz (Corresponding to a B-field of 0.977 Tesla), the DEE Vp-p that develops is 7,500 V, thus ∆E is 7,500eV. Taking q=1.6E-19, and m=1.67E-27, so we can expect: ... ∆r(r) = (8.2E-5) 1/r
Editorial note, tabletop extrapolation: The single most useful sizing formula for probe and cup design: turn spacing at any radius from dee voltage and field — it sets how thin an intercepting tip must be and whether turns separate on a screen. Conditions: nonrelativistic ions, approximately uniform B, small per-turn gain, with ΔE the effective energy gain per turn (this machine's single-dee convention takes it as the 7,500 V peak-to-peak; multiple gaps or off-crest phase change it). Caution: the printed substitution line shows the charge as (1.6E-27) in the denominator, a source misprint for 1.6E-19 (the text above states q=1.6E-19); recomputing with 1.6E-19 reproduces the printed 8.2E-5 coefficient.
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The Rutgers 12-inch magnet has flat poles with a maximum B-field of about 1 T, and the field is shaped by pole-tips fixed onto those flat poles; different sets were designed and built to demonstrate weak focusing, radial-sector (Thomas) focusing and spiral-sector focusing on the same magnet.
Source quote & editorial note
The cyclotron magnet features flat poles with a maximum B-field of about 1T. The magnetic field can be shaped using pole-tips that are fixed on the flat poles. ... In particular, different sets of magnet pole-tips have been designed and built. ... These different magnetic configuration illustrate the main aspects of the cyclotron focusing theory: weak focusing, radial sectors (Thomas focusing) and spiral sectors (Kerst and Laslett focusing effects)
Editorial note, tabletop extrapolation: A strong architectural argument for an educational tabletop machine: build the magnet with flat poles and put the field shaping entirely in separate pole-tips, so focusing schemes become swappable experiments rather than a magnet rebuild. This paper documents the sets and their purpose; the mounting/interchange practice is documented in the same program's field-mapping report (lib-006), whose four pole-tip sets were mapped on this magnet.
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On the Rutgers 12-inch cyclotron, radial-sector (Thomas focusing) pole-tips were built but the beam could not be accelerated up to the deflector radius because of poor isochronicity; a new spiral-sector set (Archimedean spirals, four-fold symmetry, 270 degree spiral machined after an iterative design phase using a field solver and ion tracking) was required to get beam out to the chamber radius.
Source quote & editorial note
Radial sectors pole-tips providing the so-called Thomas focusing [2] have been built but the beam could not be accelerated up to the deflector radius due to poor isochronicity. ... To successfully accelerate the beam up to the chamber's radius a new set of pole-tips was designed [5], at the same time providing additional focusing using a spiral sector design. ... An iterative design phase using a field solver and ion tracking lead to the machining of 270°spiral pole-tips
Editorial note, tabletop extrapolation: A documented negative result at exactly this scale: plain radial sectors on a small cyclotron can cost enough isochronism to prevent reaching full radius. If a tabletop builder wants AVF focusing, this collection's experience points to spiral sectors designed with a field solver plus tracking, not radial sectors alone. (The Archimedean-spiral / four-fold-symmetry statement is on p.1.)
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Sector focusing on the Rutgers 12-inch is quantified through the flutter F, defined by F² = ⟨((B(θ)−⟨B⟩)/⟨B⟩)²⟩ — so F itself is the RMS fractional azimuthal field deviation — with the sector CONTRIBUTION to axial tune ν²_sector = F²(1 + 2 tan² ε), ε the spiral angle; in the source's circular-orbit approximation this combines with the weak-focusing field-index term to give the total axial tune. The tune was reconstructed by integrating the measured field map azimuthally to obtain both the field gradient and the flutter.
F^2 = <((B(theta)-<B>)/<B>)^2> (F = RMS fractional deviation); sector contribution nu_sector^2 = F^2 (1 + 2 tan^2 epsilon); total axial tune adds the field-index termSource quote & editorial note
The edge-focusing adds a term to νz2 depending on the "flutter" (mean square deviation of B(θ) ... where <B> is the θ-averaged axial magnetic field. ... The spiraling changes the edge crossing angles and the sector focusing contribution to the axial tune becomes ν2sector = F2 (1 + 2tan2 ε) where F is defined in Eq. 3 and ε is the spiral angle.
Editorial note, tabletop extrapolation: The minimum analysis needed to turn a measured or simulated AVF field map into a predicted axial tune for a tabletop machine. The quoted line reflects the PDF's text-layer rendering of typeset superscripts; the equation as set on the page is nu_sector^2 = F^2 (1 + 2 tan^2 epsilon).
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To run the Rutgers 12-inch (a proton machine) on deuterons for d(d,n)He3 neutron production, the RF was retuned to 7.15 MHz — approximately half the proton frequency, for q/m of one half — which required a new externally coiled tank-circuit inductor to bring the dee's 78 pF capacitance into resonance, with the coupling loop adjusted to present the RF power amplifier a pure 50-ohm load.
Source quote & editorial note
Primarily dedicated to proton acceleration, the cyclotron's Radio Frequency (RF) systems was retuned to 7.15 MHz to satisfy the magnetic resonance acceleration condition for deuterons having a q/m of half that of the single a.m.u. proton. A new, externally coiled, tank circuit inductor was wound to bring the DEE's 78 pF capacitance into resonance. The coupling loop was adjusted to present the RF power amplifier with a pure 50-ohm load.
Koeth, Neutron Production with a 12-Inch Cyclotron (2017) — p. 1
Editorial note, tabletop extrapolation: Species matters and it can change the RF plant, not just a dial: at fixed field, deuterons run at about half the proton frequency, and the resonator plus matching network must reach it — on this machine that meant winding a physically new tank inductor, because the existing tank could not tune an octave down. The 78 pF dee capacitance is this 12-inch machine's measured value; use it as a sanity anchor, not a design number.
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The Rutgers 12-inch neutron work used the d-d reaction, described by the author as having a broadly peaked cross section at a mere 180 keV, with the d(d,n)He3 reaction producing 2.45 MeV neutrons quasi-isotropically for an incident beam in the 180 keV regime. This is a DEUTERON beam on a deuterated target — not a proton reaction.
Source quote & editorial note
Many nuclear reactions produce neutrons, but perhaps the simplest is d-d reaction, with a broadly peaked cross section at a mere 180 keV. With an incident energy beam, in the regime of 180 keV, the reaction d(d,n)He3 reaction produces 2.45 MeV neutrons quasi-isotropically.
Koeth, Neutron Production with a 12-Inch Cyclotron (2017) — p. 1
Editorial note, tabletop extrapolation: The species distinction is the load-bearing radiological fact: deuterons on a deuterated target make fast neutrons at only ~180 keV, while common stable targets have (p,n) thresholds above 1 MeV (7Li(p,n) at ~1.88 MeV is among the lowest) — so a sub-MeV proton machine's neutron picture hinges on verifying the beam really is protons (deuterium contamination opens the D–D channel), what the beam actually strikes, and the truthful maximum energy; no blanket neutron-free claim follows. The cross-section characterization and the quasi-isotropic 2.45 MeV figure are the source's own: at finite beam energy the neutron energy is angle-dependent, and quantitative cross-section shapes should be taken from evaluated data at design time, not from this description. The source states its laboratory move was what provided the radiological controls to permit fast-neutron generation (abstract, p.1).
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The RF chain for neutron runs on the Rutgers 12-inch was a programmable Tektronix AFG3101 100 MHz arbitrary function generator (supplying both RF drive and the timing trigger), a solid state ENI-350L intermediate stage, and an Ameritron AL-82 linear final rated 1500 watts continuous. Lack of active dee cooling limited the RF power to about 1000 watts average, and pulsed RF operation was used to reach the highest dee voltage possible without exceeding thermal tolerances. The RF auto tuner was only usable in CW operation.
Source quote & editorial note
A programmable Tektronix AFG3101 100 MHz arbitrary function generator supplied the RF drive and timing trigger output. The intermediate RF stage utilized a solid state ENI-350L which in turn drove the final power amplifier, an Ameritron AL-82 linear capable of 1500 Watts continuous. Lack of active DEE cooling limited the RF power to about 1000 watts average. When not in CW mode, pulsed RF operation was used to simultaneously achieve the highest DEE voltage possible while not exceeding the thermal tolerances. The RF auto tuner was only employed during CW operation, as provisions have not been installed for pulsed operation.
Koeth, Neutron Production with a 12-Inch Cyclotron (2017) — p. 1
Editorial note, tabletop extrapolation: A demonstrated tabletop RF plant, end to end: arbitrary function generator (drive + timing), solid-state intermediate stage, and an amateur-radio HF linear (AL-82 class, 1500 W continuous) into the matched tank. In THIS installation the uncooled dee — not the amplifier — set the ~1000 W average ceiling, and pulsing bought peak dee voltage inside that thermal budget (the auto-tuner only worked CW). Another machine repeats the analysis: matching range, tank losses, feedthrough heating and duty rating decide where its own ceiling sits.
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Detector choice near a cyclotron magnet is governed by the fringe field: on the Rutgers 12-inch the Ludlum Model 12-4 boron-10 enriched BF3 'rem ball' was the primary diagnostic specifically because its BF3 tube was unaffected by the magnetic field and could be positioned arbitrarily close to the chamber, while the two photomultiplier-based detectors (Ludlum 42-4 LiF(Eu) scintillator and Ludlum 42-2 proton recoil) had their signals greatly reduced or extinguished within about two feet of the magnet gap. A NaI(Tl) gamma spectrometer likewise lost PMT gain to the field and ceased entirely when placed too close, even with a mu-metal shield, so it was sited about three feet from the target.
Source quote & editorial note
While not as sensitive as the other two tubes, the 12-4 was the primary diagnostic as its BF3 tube was unaffected by the magnetic field and could be positioned arbitrarily close to the cyclotron chamber. The second and third detectors were photomultiplier based detectors; one being a Ludlum Model 42-4 LiF(Eu) scintillator, and the third detector a Ludlum Model 42-2 proton recoil detector. When positioned sufficiently far away from the cyclotron magnet, neutrons were detected by both, however, an approach closer than two feet of the magnet gap either greatly reduced or otherwise extinguished the photomultiplier tube signals.
Koeth, Neutron Production with a 12-Inch Cyclotron (2017) — p. 4
Editorial note, tabletop extrapolation: Concrete siting guidance from one instrumented machine: its gas-filled BF3 rem-ball worked arbitrarily close to the chamber, while its two PMT-based instruments (LiF(Eu) scintillator, proton-recoil) lost or degraded signal inside roughly two feet of the magnet gap, and its NaI(Tl) spectrometer failed close-in even with a mu-metal shield (sited ~three feet out; that sentence is on p.6). The pattern — gas tubes tolerate fringe field, PMTs suffer — is a sound prior, not a law: test each complete detector-plus-electronics assembly in the actual fringe field before committing to a layout. (The companion 2020 draft ran a 3He tube close-in, its own separate data point.)
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The Rutgers 12-inch cyclotron's magnet is a 12-inch-diameter H-frame iron-core magnet giving a nominally 1 Tesla vertical field across a 2-inch magnet gap, with interchangeable iron pole tips; the machine is rated 1.2 MeV protons.
Source quote & editorial note
The 12-inch diameter H-frame iron core magnet provides a nominally 1 Tesla vertical field in the 2-inch magnetic gap. … Interchangeable iron pole tips allow for application of various focusing schemes. … The Rutgers 12” Cyclotron (Fig. 1) is a 1.2 MeV particle accelerator dedicated to student education and exploration.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.291. The closest published match to the 8–12 inch class: same pole-diameter band, H-frame topology, a NOMINAL 1 T across a 2-inch gap, interchangeable tips, and a 1.2 MeV rating. Read the parameter set as an existence proof for the class, with one conversion warning: 1 T is roughly double a 0.5–0.6 T amateur magnet, so this machine's energies do not transfer to a weaker field at the same radius (E ∝ B²r²).
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On the Rutgers 12-inch cyclotron the vacuum chamber runs at 10E-5 Torr and holds a 5-inch radius DEE plus dummy DEE, driven at up to 10 kV peak RF over a tunable 2-30 MHz range; protons and 2H+ come from an internal cold-cathode Penning Ion Gauge (PIG) source, and diagnostics are a radial probe and a deflector each carrying a phosphor screen / current collector.
Source quote & editorial note
holds a 5-inch radius DEE and dummy DEE with a peak applied RF voltage of 10 kV and tunable frequency 2 - 30 MHz.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.291. A self-consistent parameter list for a machine at exactly this scale: 5-inch dee radius inside 12-inch poles, "10E-5 Torr" as printed — read as 1×10⁻⁵ Torr, the operating pressure the companion paper WEPPT025 states unambiguously — and a reported 10 kV peak applied dee voltage over a tunable 2–30 MHz range. The single-dee-plus-dummy-dee topology and the every-diagnostic-is-also-a-current-collector pattern are the parts worth copying; the numbers are reference-machine parameters, not targets.
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Precision-ground perfectly parallel pole faces (purely vertical field, no gradient) gave the Rutgers 12-inch cyclotron only a few nanoamps of current at the outer edge of the chamber; replacing them with weak-focusing tapered tips dramatically increased deliverable beam current.
Source quote & editorial note
This solution only delivered a few nanoamps of current at the outer edge of the chamber.
Editorial note, tabletop extrapolation: PDF p.2 = printed p.292 (the "dramatically increase deliverable beam current" phrase is on p.1). The easiest thing to machine — flat, parallel, precision-ground poles — is a documented failure mode at this scale: with a purely vertical field there is no axial restoring force, and this machine delivered only a few nanoamps to the chamber edge until a slight radial taper was cut. What another machine gets from flat poles depends on its own alignment, apertures and source; the transferable instruction is to evaluate axial tune and transmission from your own field map, expecting roughly this fate without a gradient.
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In the Rutgers 12-inch cyclotron's weak-focusing field the field index n = -(r/B)(dB/dr) gives radial and axial stability for 0 < n < 1, but coupling resonances restrict the usable band to 0 < n < 0.2; in the installed tips n = 0.2 occurs beyond the deflector radius, and the vertical tune is nu_z = sqrt(n).
n = -(r/B)(dB/dr); nu_z = sqrt(n)Source quote & editorial note
Coupling resonances further restrict 0 < n < 0.2. In the existing tips, n = 0.2 occurs beyond the deflector radius.
Editorial note, tabletop extrapolation: PDF p.2 = printed p.292. The pole-tip acceptance criterion under the ideal azimuthally-symmetric weak-focusing model (νr = √(1−n), νz = √n, so νr = 2νz at n = 0.2): do not just satisfy 0 < n < 1 — shape the taper so n stays under 0.2 out to the last useful radius, as this machine's tips do (n = 0.2 beyond the deflector radius). Confirm on the actual field map with a tune or tracking analysis; azimuthal variation, fringes and errors move the real resonance picture.
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A set of periodicity-4 radial-sector (non-spiral) AVF pole pieces fabricated at the Rutgers 12-inch cyclotron failed in operation: as simulation had predicted, phase slippage at the standard 8 kV DEE voltage was severe enough that ions never reached the deflector.
Source quote & editorial note
As predicted via simulation, phase slippage at standard DEE voltage (8 kV) was so severe that ions were not delivered to the deflector.
Editorial note, tabletop extrapolation: PDF p.2 = printed p.292. A cautionary data point for anyone tempted by straight radial-sector AVF tips: on this machine the phase slippage was fatal at 8 kV on the dee — and, holding the same field-frequency mismatch and final radius, a machine with LESS energy gain per turn takes more turns and accumulates more slip, so a low-voltage build should expect this failure mode to bite harder, not softer. Check isochronism in the tracker before cutting sectored steel (the spiral redesign that followed is dg-1745's story).
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For spiral-edged AVF sectors the vertical tune obeys nu_z^2 = -k + F(1 + tan^2 xi), where F is the flutter (mean field variation at fixed radius), k the average negative field index, and xi the edge angle; the form is convenient for Archimedean spirals r = a*theta^(1/n), for which the Rutgers paper states tan xi = d(theta)/dr.
nu_z^2 = -k + F(1 + tan^2 xi); Archimedean spiral r = a*theta^(1/n); edge angle (from radial): tan xi = r*d(theta)/dr = n*theta [source prints tan xi = d(theta)/dr, which is not dimensionless — corrected 2026-09-05, site wave-18 audit; verify conventions against Livingood, the paper's ref 10, before numerical use]Source quote & editorial note
This form is convenient for sectors defined by an Archimedean spiral, r = aθ^(1/n), for which tan ξ = dθ/dr.
Editorial note, tabletop extrapolation: PDF p.3 = printed p.293 (the exponent 1/n is printed as a superscript; the quote transcribes it inline). The design equation for trading spiral tightness against vertical tune before cutting steel — with one correction applied: as printed, tan ξ = dθ/dr is not dimensionless; the standard edge-angle relation is tan ξ = r·dθ/dr, which for the stated Archimedean spiral evaluates to nθ. The flutter and approximation conventions are the paper's; verify against Livingood (its own ref [10]) before using the tune expression numerically.
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The Rutgers AVF study states the ideal average field profile for such a machine decreases with radius before flattening at larger radii — the falling inner part supplies weak focusing in the central region where flutter is negligible, the flat outer part supplies isochronism — and that high flutter is separately desirable to raise the vertical tune.
Source quote & editorial note
The ideal average field profile decreases with radial distance from the center before flattening out at larger radii … This is necessary to provide weak focusing at the central region, where flutter is negligible. High flutter values were also desirable, to increase the vertical tune.
Editorial note, tabletop extrapolation: PDF p.3 = printed p.293. The most useful shaping rule in this paper for a small AVF attempt: flutter is essentially zero on axis, so the central region must still weak-focus — the falling inner profile is not optional — and the flat outer region approximates isochronism only in the low-energy nonrelativistic sense (exact fixed-frequency isochronism wants the orbit-averaged field rising as γ; immaterial at this machine's energies, material by 20 MeV). Fig. 4 shows the resulting bump-plus-flat profile for the chosen 270-degree spiral, whose caption marks the isochronous region.
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As a stated future plan (not an achievement) at the time of the 2013 conference, the Rutgers program had secured an H-frame 19-inch magnet — a General Electric magnet delivered to Rutgers in 1947 and run for 35 years for NMR research before storage — for a second-generation educational cyclotron; its coils were awaiting new copper windings.
Source quote & editorial note
The cyclotron facility has already secured an H-frame 19-inch magnet, a special General Electric magnet delivered to Rutgers in 1947 … and operated for 35 years for NMR research before retirement to storage.[13] Upon acquisition, the venerable magnet coils were in need of refurbishing and are currently awaiting new copper windings. … Future plans include the assembly of a second generation 19-inch educational cyclotron.
Editorial note, tabletop extrapolation: PDF p.5 = printed p.295. One documented acquisition route: a decommissioned 1947 GE NMR electromagnet, secured for a planned second-generation educational machine — with the coils needing refurbishment as part of the price. It also records the scale step this program judged worth taking from a proven 12-inch: 19 inches, not 30. Before buying any surplus magnet of that vintage, inspect winding insulation, cooling passages, resistance and field quality; rewinding is a real possibility, not a certainty. This was a plan in 2013; the paper reports no beam from the 19-inch machine.
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On the Rutgers 12-inch cyclotron, early filament-based internal ion sources produced only nanoamps of protons and lasted a few hours; the group replaced them with a cold-cathode Penning Ion Gauge (PIG) source, and describe the ion source as the cyclotron's most challenging component.
Source quote & editorial note
Early filament based designs generated mere nanoamps of protons and would only operate a few hours.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.366. The trade as this program experienced it: their early filament designs gave nanoamps and hours, and the cold-cathode PIG is what made the machine routine. Hot-filament sources are not intrinsically nanoamp devices — output depends on geometry, emission, gas feed and what current is being quoted — so read this as one program's motivated migration plus their judgment that the source is the machine's hardest component, and compare designs on measured current and lifetime.
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For the Rutgers deflector geometry in a 1 Tesla field, a 33 kV potential across the channel's average 0.31 inch gap is required to produce the 4.2 MV/m transverse field that lands protons on the viewing screen's center.
Source quote & editorial note
In a 1 Tesla field, a potential of 33 kV is required to produce a transverse electric field of 4.2 MV/m
Editorial note, tabletop extrapolation: PDF p.2 = printed p.367 (gap on PDF p.3 / printed p.368). The three numbers are mutually consistent on computation — 4.2 MV/m across 0.31 inch (7.9 mm) is 33 kV, and the paper's own formula with ρ1 = 7 in, ρ0 = 4 in, B = 1 T returns 4.2 MV/m for the computed ~494 keV proton at 4 inches — so the set can be trusted as a worked example. Another machine recomputes from its own orbit radii, field and electrode gap; the voltage scales with the gap and the geometry, and can land well above or below this.
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The Rutgers 12-inch cyclotron's H-frame magnet takes removable pole tips up to 1 inch thick, and four interchangeable sets exist — two weak-focusing (one deliberately "good", one intentionally "bad" for teaching), one radial-sector AVF and one spiral-sector AVF — all reaching a maximum central axial field Bz(r=0) of 1.2 Tesla.
Source quote & editorial note
the pole tips can be up to 1-inch thick and are easily removable – to date, we have four sets of pole tips and one of each set is shown in Fig. 2. They consist of two weak focusing (one “good” and one intentionally “bad” for educational purposes), a radial sector AVF and a spiral sector AVF, all with a maximum central axial field, Bz(r=0), of 1.2 Tesla.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.369 (the four sets are photographed in Fig. 2). The key architectural decision for a tabletop machine intended to be experimented on: make the pole tips removable and the same magnet becomes four different machines. Budget the geometry honestly — tips up to 1 inch THICK EACH sit inside the magnet opening, and the clear beam gap that remains is a separate design number this paper does not state. 1.2 T central is the stated ceiling with tips installed, versus the "nominally 1 Tesla" working figure quoted elsewhere in this collection.
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The Rutgers 12-inch cyclotron's upper and lower magnet coils are independently energized so the median plane can be deliberately shifted for axial steering; while holding the average ampere-turns constant, coil currents of 17/12, 14.5/14.5 and 12/17 amps (top/bottom) all still brought beam to the chamber periphery.
Source quote & editorial note
The magnet’s upper and lower coils are independently energized for intentional field imbalance so as to shift the median plane. … Figure 6 shows three standard radial-draw beam images: the left frame top/bottom coil at 17/12 amps, the middle frame at 14.5/14.5 amps, and the right frame at 12/17 amps.
Editorial note, tabletop extrapolation: PDF p.3 = printed p.371 (design intent on PDF p.1 / printed p.369). A genuinely cheap axial-steering mechanism for a small machine: energize the two coils independently and trim the median plane. On this machine a 5 A top-to-bottom imbalance about the 14.5/14.5 A balance point still brought beam to the periphery — a demonstration that the knob has useful range, with transmission, centering and beam quality at each setting still to be measured on any machine that copies it.
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The Rutgers 12-inch cyclotron has a single 5-inch radius DEE with a 0.9 inch vertical aperture facing a matching dummy DEE; the RF supply tunes 2-30 MHz with power adjustable to 1.5 kW, runs continuous or pulsed, and reaches a peak DEE voltage of 10 kV.
Source quote & editorial note
The cyclotron has a single 5-inch radius DEE with a 0.9 inch vertical aperture and a matching dummy DEE. The Radio Frequency (RF) supply is tuneable from 2 to 30 MHz with power adjustable up to 1.5 kW; it can be operated in continuous or pulsed mode and is capable of achieving a peak DEE voltage of 10 kV.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.369. The RF benchmark for the tabletop class as one machine's data point: 1.5 kW of tunable drive and a 10 kV peak dee voltage on a 5-inch dee — noting the two maxima need not be simultaneous, and what a kilowatt buys on another machine depends on its loaded Q, coupling and shunt impedance, which an upgrade should measure rather than scale. The 0.9-inch dee aperture is likewise this machine's choice, not a permitted fraction of any gap.
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The Rutgers 12-inch cyclotron reaches its 1E-5 Torr operating pressure with a standard 4-inch diffusion pump stack.
Source quote & editorial note
The operating pressure of 1E-5 Torr is provided by a standard 4-inch diffusion pump stack.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.369. Calibration context for the tabletop class: this 12-inch chamber with an internal PIG source holds 1E-5 Torr on a standard 4-inch diffusion stack — no turbo or cryo claimed. Size another machine from its own gas throughput: P = Q/S with the EFFECTIVE speed after conductance and baffle losses, with the source's hydrogen feed as the dominant Q. The Rutgers datum says the answer can come out '4-inch diff pump'; it does not say it will.
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In the Rutgers 12-inch cyclotron's weak-focusing field the axial tune is nu_z = sqrt(n) and the radial tune nu_x = sqrt(1-n), with total transverse stability for 0 < n < 1; coupling resonances further exclude n = 0.2, 0.36 and 0.5 (and higher values).
n = -(r/B)(dB/dr); nu_z = sqrt(n); nu_x = sqrt(1-n)Source quote & editorial note
Values of n=0.2, 0.36, 0.5 (and others yet higher) need to be avoided.
Editorial note, tabletop extrapolation: PDF p.2 = printed p.370. The explicit forbidden-n list a weak-focusing pole-tip designer rarely sees written down: inside 0 < n < 1, the taper must also avoid 0.2 (Qx = 2Qz), 0.36 and 0.5. A well-chosen profile keeps n below 0.2 for nearly the whole acceleration (the source's own following prescription); the design questions are where n(r) crosses what, and how fast — compute or map n(r) rather than assuming which resonances are in play.
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Because ions start their spiral at r = 0 where n is necessarily 0 and n only climbs with radius, a weak-focusing cyclotron's field fall-off must be moderated so that n = 0.2 is reached only near the final ion radius.
Source quote & editorial note
Since the ions begin their spiral journey at r=0 necessarily n also starts at 0, and will only climb as the radius increases; if n=0.2 is to be avoided (Qx=2Qz), then the rate at which Bz decreases must be moderated such that n=0.2 only near the final ion radius.
Editorial note, tabletop extrapolation: PDF p.2 = printed p.370. The actionable pole-taper prescription for a small weak-focusing machine, on the source's own premise that n starts at 0 and climbs with radius: moderate the fall-off so n = 0.2 arrives only near the final radius. A taper aggressive enough to buy strong axial focusing early reaches the coupling resonance early, and time spent near it with any driving asymmetry risks resonant amplitude growth — Rutgers built a deliberately bad pole set to demonstrate exactly that (dg-1841).
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The axial betatron period Tz relates to the ion revolution period T0 by Tz = T0/sqrt(n), so it takes 1/sqrt(n) revolutions to complete one vertical betatron oscillation and the betatron phase advances by sqrt(n) of a period per revolution.
T_z = T_0 / sqrt(n)Source quote & editorial note
Thus for a given n it takes 1/√n ion revolutions to complete one vertical betatron oscillation
Editorial note, tabletop extrapolation: PDF p.2 = printed p.370. What converts a photograph into a number: count N revolutions between same-phase vertical maxima and νz ≈ 1/N — and, under the smooth azimuthally-symmetric weak-focusing approximation, n ≈ 1/N². It is an average over the interval, not a point measurement. On this machine's gently tapered poles νz ≈ 0.09 mid-radius (Fig. 3a), i.e. about 11 turns per oscillation, comfortably resolvable on its radial-draw images; treat that as Rutgers calibration context, not a class-typical value.
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A full 3D SIMION model of the Rutgers 12-inch cyclotron has been developed and, the author states, extensively verified with every configuration of the machine.
Source quote & editorial note
A full 3D SIMION model has been developed and extensively verified with every configuration of our cyclotron.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.369. The Rutgers pattern worth copying: one maintained 3-D model kept in step with every hardware configuration, rather than a fresh single-purpose simulation per experiment. Read across this collection, the payoff shows up as predictions that preceded hardware — the radial-sector phase-slippage failure, the AVF operating point, the deflector turn bands (each carried on its own card with its own source). Note the companion paper we1pb04 reports qualitative, not absolute, agreement for phase, so 'verified' is trend-level where checked.
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The Rutgers group state that, reaching a maximum energy of 1.2 MeV protons, their 12-inch cyclotron is not a radiological hazard and is easily approachable while operating; a companion paper adds that because of its low energy the machine does not activate during operation and is incorporated into lab coursework in a laboratory classroom. These are the source's own characterizations of their machine.
Source quote & editorial note
reaching a maximum energy of 1.2 MeV protons, the Rutgers Cyclotron is not a radiological hazard and is easily approachable while operating.
Editorial note, tabletop extrapolation: PDF p.1 = printed p.369; the companion non-activation statement is we1pb02 PDF p.1 / printed p.291. Reported strictly as the authors' assessment of their own machine and setting — neither paper reports survey data, shielding or a licensing basis. Two physics limits on transferring it: a 1.2 MeV proton ceiling is not a universal no-activation threshold (thresholdless capture reactions such as 12C(p,γ)13N and light-element targets produce prompt gammas and activation below it), and the assessment assumes proton beams — deuteron contamination opens neutron channels. A builder in this class should read it as evidence such machines are operated in classrooms, and still do their own commissioning survey, species verification and regulatory review.
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The nine-inch cyclotron of Koeth (1999) was built around a repurposed Varian V-3400 NMR electromagnet of H-frame design, mounted sideways on a table so that its gap became horizontal at a comfortable working height; new pole tips were machined from 1020 rolled steel into cylinders, nine inches in diameter, giving a 2.1875 inch gap and a maximum obtainable field of 1.2 Tesla.
Source quote & editorial note
The most accessible magnet was a Varian V-3400 NMR magnet. It is of the typical H-frame design. Slight modifications were made to utilize the V-3400. Mounting the magnet sideways on a table created a horizontal gap at a reasonable work height. New pole tips were machined from 1020 rolled steel into cylinders, maximizing the diameter. The poles are nine inches in diameter and create a gap of 2.1875 inches. The maximum field obtainable from this geometry is 1.2 Tesla.
Editorial note, tabletop extrapolation: Directly on point for an 8-12 inch tabletop machine. Two transferable moves: a surplus NMR/analytical H-frame magnet is a viable starting core, and re-orienting it so the gap is horizontal turns a vertical-gap instrument into a bench cyclotron with a flat median plane at working height. The 9 in pole / 2.1875 in gap pair (gap ~24% of pole diameter) is a concrete usable aspect ratio at this scale.
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On the nine-inch cyclotron the operating field was chosen from the RF frequency rather than the reverse - with f = qB/2*pi*m and an operating frequency of 13.56 +/- 0.03 MHz the required field was 0.889 Tesla, which is 70 percent of the magnet's 1.2 Tesla maximum; the author treated that margin as a deliberate reliability choice.
f = qB/(2*pi*m); equivalently B = 2*pi*m*f/qSource quote & editorial note
For reasons that will be discussed later the operating frequency is 13.56+0.03 MHz. Using the cyclotron frequency relationship: f = qB/2(pi)m a magnetic field of 0.889 Tesla was determined to be the operating field value. This was a welcome operating value, as the magnet need only be run at 70 percent of its maximum values, reducing the chance of coil failure by pressing the tolerances.
Editorial note, tabletop extrapolation: A builder who inherits a fixed RF frequency (13.56 MHz here — a standard ISM frequency with cheap surplus hardware) can invert the design order and let the magnet operating point follow. Computed: 0.889 T is 74.1% of the 1.2 T ceiling — the author's "70 percent" is his rounding — and he treated the margin as a reliability choice for his coils; what margin buys on another magnet is a thermal/insulation/cooling question to check, not a free good. The quote's "+" before 0.03 MHz is a plus-or-minus sign the scan renders as a plus with an underline.
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Nine-inch cyclotron magnet electrical and cooling budget - the 1780 pound magnet needed 40 volts at 168 amps (7 kilowatts) for the 1.2 Tesla maximum, but only 28 volts at 114 amps (3.2 kW) at the 0.889 Tesla operating point; coil cooling water ran at approximately 38 PSI inlet pressure and no less than 4 GPM, regulated by an inline pressure regulator with an impeller-driven magnetic pick-up digital flow meter.
Source quote & editorial note
The magnet weighs 1780 pounds, it requires 40 volts at 168 amps, 7Kilowatts, to produce the maximum field of 1.2 Tesla. Only 28 volts at 114 amps, 3.2 kW, is required at the operating value of 0.889 Tesla. Water cooling is used to remove the heat generated by the coils, the inlet pressure is approximately 38 PSI and flow rate is no less than 4 GPM. The pressure is controlled with an inline pressure regulator and the flow rate is monitored with an impeller driven magnetic pick-up digital flow meter.
Editorial note, tabletop extrapolation: The most useful sizing datum in the document: backing off from 1.2 T to the 0.889 T operating point cut coil dissipation from 6.7 kW (40 V × 168 A; the author's "7Kilowatts" is rounding) to 3.19 kW — a factor of about 2.1 — while still requiring monitored water cooling (38 PSI, ≥4 GPM, flow meter). The shape of the lesson transfers (field costs quadratic-ish power near saturation; margin is cheap to buy by backing off), the numbers belong to this 1780-pound magnet.
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Field-setting resolution on the nine-inch cyclotron was limited by thermal drift, not by the control electronics - a Fluke 4210 BCD programmable DC source over IEEE-488/HPIB drove the Sorenson DCR-40-250A supply's 0-8.00 V programming input in 1 mV steps, giving a theoretical resolution of one part in six thousand (2 gauss out of 1.2 Tesla), but cooling-water temperature changed the coil resistance and, because the DC supply was voltage regulated, changed the current and therefore the field.
Source quote & editorial note
in six thousand or 2 gauss. Practically though, the field control was less than the theoretical as variations in cooling water temperature would change the resistance of the coils. The DC power system being voltage regulated then caused changes in the magnet current and of course the magnetic field.
Editorial note, tabletop extrapolation: A cautionary rule with a number attached: the DAC chain promised 2-gauss setability (one part in six thousand), and the VOLTAGE-regulated supply handed that away to the chiller — cooling-water temperature moved coil resistance, hence current, hence field. Current regulation removes that specific path; hysteresis, yoke temperature, ripple and calibration remain, so a claimed field stability is demonstrated by measurement (or closed on a Hall/NMR probe), never promised by the DAC's step size. (The sentence begins on p.1: "...theoretically the magnetic field could be adjusted to one part..."; "Telsa" is a source typo.)
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Nine-inch cyclotron vacuum chamber as-built - stainless steel circular wall of 11.00 inch inside diameter and 0.750 inch wall thickness, top and bottom lids of 0.25 inch aluminum sealed to the wall with 451 Viton O-rings, outside height 2.00 inches and inside height 1.50 inches, accessory ports TIG welded and terminated in CF2.75 or CF1.33 metal gasket flanges, with the main vacuum port a standard KF25 Viton O-ring seal.
Source quote & editorial note
The chamber’s construction is of a stainless steel wall, accessory ports, and flanges. The top and bottom lids of the chamber are of 0.25 inch aluminum. The lids make a vacuum tight seal to the circular stainless steel wall with the use of 451 Viton O-rings. The accessory ports were TIG welded and are terminated in either CF2.75 or CF1.33 metal gasket seal flanges. The vacuum port on the chamber is a standard KF25 Viton 0-ring seal. … The chamber has an inside diameter of 11.00 inches and a wall thickness of 0.750 inches. The outside height of the chamber measures 2.00 inches and the inside height measures 1.50 inches. The DEE is 1.00 inch thick allowing for 0.25 inches of clearance between the top and bottom of the lid. The DEE wall is 1/16 inch thick brass. The DEE and chamber are symmetrical about the chamber's median plane.
Editorial note, tabletop extrapolation: A fully specified chamber at exactly this scale, whose internal consistency checks out: 2.00 in outside minus two 0.25 in lids = the stated 1.50 in inside; the 1.00 in dee leaves the stated 0.25 in per side. The elastomer-for-big-seals, metal-gasket-for-instrument-ports split is a pragmatic cost/performance pattern worth copying. Copy the PATTERN and re-derive the numbers: lid deflection under atmosphere, seal compression, and HV clearances are per-design calculations (the magnet gap this chamber fits — 2.1875 in — is on the magnet card, dg-1846-class).
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Dee mounting and high-voltage feed on the nine-inch cyclotron - the dee is carried on a 0.500 inch copper rod mounted to a CF2.75 flange, the whole assembly suspended from the chamber by a ceramic break terminated with CF2.75 flanges at either end, forming a vacuum-tight high-voltage feed-through whose copper stem protrudes several inches outside the flange for direct connection to the RF matching cabinet mounted just outside the magnet coils.
Source quote & editorial note
The DEE is supported by a 0.500 inch copper rod that is mounted to a CF2.75 flange. This whole assembly is then suspended from the chamber by a ceramic brake terminated with CF2.75 flanges at either end. This provides a substantial vacuum tight high voltage feed-though. The copper stem protrudes the vacuum flange by several inches allowing direct connection to the high voltage terminal in the RF matching cabinet, which is mounted just outside of the magnet coils.
Editorial note, tabletop extrapolation: The mechanically simplest dee feed-through arrangement in the amateur literature - the same copper rod is structural support, RF conductor and vacuum feed-through, with a commercially available ceramic break doing the insulating. Keeping the matching cabinet immediately outside the coils keeps the high-impedance high-voltage run short. Note the appendix drawing (PDF p.16) dimensions this copper stem as 0.375 inch with a 0.75 inch brass collar, which disagrees with the 0.500 inch in the text. The source spells "break" as "brake" and "feed-through" as "feed-though".
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On the nine-inch cyclotron the second accelerating electrode is a "Dummy DEE" mounted diametrically in the chamber in direct electrical contact with it, which also serves as the central mounting surface for the ion source; the chamber median plane is adjusted to coincide with the magnetic median plane.
Source quote & editorial note
The chamber's median plane is adjusted to be the same as the magnetic field's median plane. The Dummy DEE is mounted diametrically in the chamber making excellent electrical contact as it provides the aperture of the second accelerating electrode. The dummy DEE also provides a central mounting surface for the ion source.
Editorial note, tabletop extrapolation: A topology that simplifies a small build: one driven dee (one HV feed-through) against a grounded dummy dee that doubles as a rigid, on-axis, at-ground mounting surface for the source — exactly where the source must sit. Whether one dee or two suits a given machine is an RF and symmetry decision, and some sources need bias or insulation rather than grounded mounting. The alignment rule worth copying outright: set the chamber median plane to the MAGNETIC median plane, not to the pole faces.
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Nine-inch cyclotron pumping stack and achieved pumpdown — a Precision direct-drive mechanical pump (ultimate 1E-4 Torr, 195 liters/minute) backing a Veeco 4 inch water-cooled diffusion pump on Dow Corning 704 oil with water-cooled baffles and a liquid nitrogen trap; the source prints the diffusion pump's ultimate as 1E-8 Torr and its speed as "425 liters/minute" [2026-09-05 note, site wave-18 audit: almost certainly a unit slip for 425 liters/SECOND — a 4-inch diffusion pump's rated speed is hundreds of L/s, and 425 L/min would be 7 L/s; unverified against a Veeco datasheet]. After careful clean assembly the chamber routinely reached 1E-5 Torr in about 30 minutes and better than 5E-6 Torr in under 2 hours.
Source quote & editorial note
The Precision mechanical pump has an absolute pressure of 1E-4 Torr, and a pumping speed of 195 liters/minute. The diffusion pump is a Veeco 4 inch water cooled pump that uses Dow Corning 704 oil, with water cooled baffles, and a liquid nitrogen trap. … The ultimate pressure of this four inch pump is 1E-8 Torr and has a pumping speed of 425 liters/minute. Directly after the LN2 trap the plumbing steps down from a four inch flange to a two-inch KF40 Viton flange. A valve manifold and 18 inches of two-inch metal bellows connect the LN2 trap to the chamber. Only at the chamber does the vacuum line reduce to one-inch. After great care in assembling a clean and tight vacuum system the chamber can routinely be evacuated to 1E-5 Torr in approximately 30 minutes, and < 5E-6 Torr in less than 2 hours.
Editorial note, tabletop extrapolation: An achieved pumpdown benchmark for one clean, tight chamber of this size — 30 minutes to 1E-5 Torr, under 2 hours below 5E-6 — a realistic anchor, not a guarantee, since gas load and conductance own the result. The conductance practice embedded here is the copyable part: hold the largest line diameter from the trap and neck down only at the chamber itself (4 in → 2 in → 1 in at the last joint). Pump ultimates are manufacturer specifications, not measured chamber pressures. (The quote begins at the foot of p.2 and concludes on p.3.)
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The nine-inch cyclotron used a MOPA (Master Oscillator Power Amplifier) RF scheme rather than a self-excited oscillator; the author's stated reasons were that MOPA is the most stable and simplest to invoke and oscillates at the driving frequency even under glow discharge conditions, whereas a self-excited oscillator, though more efficient, is very complicated and demands an experienced radio engineer to avoid parasitic oscillations.
Source quote & editorial note
MOPA - Master Oscillator Power Amplifier ideology was decided upon as it is known to be the most stable as well as the simplest to invoke. The MOPA system oscillates at the driving frequency with great stability, even under glow discharge conditions. However, because the cyclotron tank circuit possess a high Q, very careful tuning becomes necessary when ensuring maximum power delivery. Other oscillator systems were considered, such as an SEO - Self Excited Oscillator, where active feed back from a pickup loop in the chamber allows for the natural frequency of the tank circuit to be sought out and oscillate automatically. Another advantage of SEO systems is their characteristic to have a very high efficiency. However, self excited systems are very complicated and require utmost care from an experienced radio engineer to prevent unwanted modes of oscillations, known as parasitic oscillations.
Editorial note, tabletop extrapolation: This is the clearest amateur-scale statement of the MOPA-vs-SEO trade for a cyclotron RF system, and it comes down in favour of MOPA for a first machine. The "known to be the most stable" and "very complicated" framings are the author's claims, presented as such. The key operational point for a tabletop builder is that MOPA holds frequency through a glow discharge, at the cost of needing careful manual tuning into a high-Q tank.
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The nine-inch cyclotron's final RF chain was an HP8165 digital programmable signal source (smallest step 10 kHz, which proved sufficiently fine) driving an ENI 350L 100 watt solid state amplifier, through a Bird 4410 wattmeter, into an impedance matching transformer that converts the 50 ohm line to the very high impedance dee; fine tuning was done at the signal source rather than by mechanically tuning the tank.
Source quote & editorial note
An HP8165 digital programmable RF signal source was used to drive an ENI350L 100 watt solid state amplifier. This method was much more convenient as fine tuning was easily achieved at the signal source rather than by manually tuning the tank circuit. The smallest adjustment capable of the HP8165 is 10kHz, which proved to be sufficiently sensitive. The output of the ENI350L amplifier was then passed through a Bird wattmeter (model 4410) and on to the RF cabinet.
Editorial note, tabletop extrapolation: Calibration data from one resonator, plus one broadly good idea. The data: 100 W of solid-state drive bought ~1700 V peak dee here (16 W forward on the beam run of record), and 10 kHz source steps proved finer than the ~90 kHz loaded bandwidth — comfortable for THIS tank. The idea: fine-tune at the SIGNAL SOURCE, not the tank — it removes mechanical tuning from the operator's inner loop. Size your own amplifier from your dee capacitance, loaded Q, coupling and target voltage, with headroom for mismatch and discharge transients.
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The nine-inch cyclotron's transmatch used the dee's own lumped capacitance (approximately 70 pF) as the tank capacitor, with the tank inductance an 8-turn coil 5 inches long of 2.14 square inch cross-sectional area wound from 1/4 inch copper refrigeration tubing, one end on the protruding dee stem and the other on chamber ground; a larger-cross-section 3-turn outer coil mounted coaxially about it formed the transformer primary, with adjustable taps to find the 50 ohm loading point.
fr = 1/(2*pi*sqrt(LC))Source quote & editorial note
It utilizes the lumped capacitance of the DEE, which is approximately 70pF, to create a tank circuit out of the chamber itself. Using the resonance equation for an inductor in parallel with a capacitor: fr=1/2(pi)sqrt(LC) L, the inductance, was chosen to bring the fr to resonance at 13.56 MHz. Initially, coarse tuning was to create an 8 turn coil of length 5 inches, with a cross sectional area of 2.14 inches^2, out of 1/4-inch copper refrigeration tubing.
Editorial note, tabletop extrapolation: The topology is the copyable part: use the dee-to-lid capacitance itself (~70 pF here) as the tank C, add an air-core tubing inductor, and couple through a coaxial few-turn primary with movable taps to find 50 Ω — no quarter-wave stem, no vacuum variable. Two numbers to reconcile on your bench: resonance at 13.56 MHz with 70 pF wants ≈2.0 µH (computed from the source's own equation), while Wheeler's formula on the printed coil geometry (8 turns, 5 in long, 2.14 in² area) yields only ≈0.8 µH — leads, strays and the actual in-situ capacitance evidently make up the difference, which is precisely why you measure fr in place and provide fine tuning rather than copying dimensions. (The 3-turn coaxial primary, adjustable taps and 50-ohm loading are printed on p.4.)
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On the nine-inch cyclotron the peak dee voltage rose as the square root of applied RF power, reaching approximately 1700 V peak at about 60 W forward RF power (from Fig.6), with roughly 1250 V at about 21 W and 500 V near 4 W; the induced peak voltage on the capacitive pickup was linearly proportional to the peak dee voltage (Fig.7), giving a simple day-to-day dee voltage reference.
Source quote & editorial note
As expected, the peak DEE voltage rises as the square root of the applied RF power, Fig.6, and the peak induced voltage is linearly proportional to the peak DEE voltage, Fig.7.
Editorial note, tabletop extrapolation: The method transfers, the number does not: measure YOUR dee voltage against forward power and expect approximate √P scaling while coupling and loaded Q stay fixed — this resonator's curve ran ~500 V near 4 W to ~1700 V at 60 W (points read from the rendered Fig. 6, 0-2000 V / 0-80 W axes; they bracket, not define, one exact coefficient). The practice worth copying outright: calibrate the cheap capacitive pickup against the rectifier divider once (Fig. 7's linearity), then use the pickup as the day-to-day reference. (The quoted sentence is the last line of p.4 and continues on p.5.)
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Hydrogen feed on the nine-inch cyclotron was a calibrated leak backed by a high pressure regulator taking hydrogen from a lecture bottle at a few thousand PSI down to approximately 10 PSI; the optimum hydrogen pressure in the chamber was found to be 5.5E-5 Torr, with higher pressures cutting collected beam through reduced proton mean free path and lower pressures starving the source of hydrogen to ionize.
Source quote & editorial note
It was found that the optimum hydrogen pressure was 5.5E-5 Torr. Pressures higher would decrease the collected beam due to the protons decreased mean free path, while pressures lower than optimum decreased the available hydrogen of which to create ions from.
Editorial note, tabletop extrapolation: The clearest statement of the pressure trade for a small internal-source machine, with both sides named: too high and the protons scatter (mean free path), too low and the source starves. This machine's optimum was 5.5E-5 Torr (5.1E-5 on the run of record), about an order of magnitude above its base pressure — gauge readings and geometry make the number machine-specific, so transfer the METHOD: establish a clean base, admit hydrogen controllably, sweep pressure against collected beam, and size pumping throughput to hold the optimum you find.
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The nine-inch cyclotron was explicitly a feasibility study for a twelve-inch successor - the author's stated plan at the time of writing was a twelve-inch magnet at 1.2 Tesla with an fr of 18 MHz to reach one million volt protons, with a capillary discharge ion source, and a tangential accessory vacuum port added after the twelve-inch system proved operable in order to extract the proton beam; he also states that a solid state amplifier is precluded once power requirements exceed 500 Watts, pointing instead to a tunable metal-ceramic sealed vacuum tube power amplifier driven by the ENI 350L.
Source quote & editorial note
Sufficient data has been taken with this feasibility-study cyclotron to warrant progression to a twelve inch magnet. It is reasonable to expect one million volt protons with a magnetic field of 1.2 Tesla, and an fr of 18 MHz. Such a magnet system is currently being obtained. ... The use of a solid state amplifier is precluded once power requirements exceed 500 Watts. ... Finally, after the twelve inch system has proved operable, a tangential accessory vacuum port will be added with the intention to extract the proton beam.
Editorial note, tabletop extrapolation: Design intent, not achievement — every number is a plan as of September 1999. What transfers is the staging philosophy: prove the concept on a small borrowed magnet (~184 keV, 9 inches) before committing to the larger machine. The "solid state precluded above 500 W" line is the author's 1999 equipment landscape, not a law — modern LDMOS amplifiers run solid-state into the kilowatts (the same lineage's later 1.5 kW AL-82 tube chain and pulsed operation, dg-1756/dg-1804, show the options both ways). The 1 µA figure on the same page is what "could have been achieved" with more source work — expectation, not measurement. Ellipses mark omitted text. (The first two quoted sentences begin on p.8.)
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The nine-inch cyclotron's accelerating gap is 0.5 inch - the appendix assembly drawing dimensions the separation between the dee edge and the flat "DEE MIRRORED FACE" of the dummy dee at 0.5, with the dee supported at top and bottom on 0.5 inch ceramic stand-offs and the dummy dee held on brackets; the dummy dee drawing carries the note that its inside dimensions mirror the face dimensions of the dee.
Source quote & editorial note
CERAMIC STAND-OFF / DEE MIRRORED FACE / BRACKET / POWER FEED-THROUGH / VACUUM PORT / ASSC. PORT 2 … [p.16 sheet callouts:] CERAMIC STAND-OFF (0.5") / DEE SHOWN WITH TOP PLATE REMOVED / 10.0 / 0.375 / 0.75 / ACTUAL SIZE
Editorial note, tabletop extrapolation: The documented geometry, as drawn: a 0.5-inch accelerating gap between the 1.00-inch dee and the mirrored dummy-dee face, dee on 0.5-inch ceramic stand-offs, inside the 1.50-inch chamber height with 0.25-inch dee-to-lid clearance. Reproduce it as historical reference geometry; whether the gap field is uniform enough and 0.25 inch stands your voltage are per-design questions for a field solve and a breakdown check. The dummy-dee sheet's "inside dimensions to mirror face dimentions of the DEE" note (PDF p.18, spelling as printed) is the fabrication shortcut: dimension the dummy by reference to the dee. (Drawing sheets are printed rotated 90 degrees; the p.15 assembly sheet labels the stand-off without a dimension — the 0.5" is on p.16.)