Design Guide › Extraction
Extraction design rules
84 of the guide’s 1374 rules carry the extraction tag.
Rules for getting beam out: electrostatic deflectors and septa, peelers and regenerators, channel placement at the last turns, and the turn separation the field must supply first.
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 and on the
all-in-one guide.
To combine this tag with another (rules carrying both), use the filterable view: /design-guide/?domain=extraction and add a second chip. Related domains, by how often they share a rule with this one: Beam dynamics (23), RF (19), Fabrication (13), Magnet (10), Materials (10).
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.
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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 & tabletop applicability
the relative radial increase is only half the relative energy increase. However, for a given cyclotron, the turn separation dr0 will double when the dee voltage is doubled.
Kleeven & Zaremba, Cyclotrons: Magnetic Design and Beam Dynamics — CAS 2015, arXiv:1804.08961 (2018) — p. 44
Tabletop: The reference machine (155 keV, 2.6 keV/turn, r=9.65 cm) gets only ~0.8 mm/turn; a 10 kV dee at the same radius gives ~3-6 mm.
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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 & tabletop applicability
for a final energy of T = 30 MeV, dT = 100 keV, and an extraction radius of 0.5 m, we find dr = 0.83 mm. This is a rather small number, e.g. when compared with a radial beam width of for instance 4 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 6
Tabletop: Small machines fare better because dr scales as dE/E; a 350 keV next machine at 10-20 keV/turn beats this 30 MeV machine's fractional separation by ~50x.
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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*|nu_r - 1|*xSource, quote & tabletop applicability
when a coherent oscillation amplitude x of 3 mm has been built up ... and acceleration takes place until vr = 0.8, the maximum turn separation due to precession is 3.8 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 7
Tabletop: A deliberate few-mm source off-centering plus letting the beam run into the fringe (n rising to 0.2-0.4) can triple the next machine's turn spacing for free.
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Size the coherent oscillation to roughly equal the incoherent (emittance) amplitude - larger invites vertical blow-up at nu_r=2*nu_z and nonlinear distortion, smaller wastes separation.
Source, quote & tabletop applicability
In practice, a coherent radial oscillation amplitude of the same size as the incoherent amplitude, is a good criterion for efficient extraction.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 7
Tabletop: If a next machine's radial beam half-width is ~2-3 mm, aim for a ~2-3 mm coherent amplitude, no more.
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Keep the deliberate radial oscillation to a few mm and cross the nu_r=2*nu_z (Walkinshaw, n=0.2) and nu_z=1/2 resonances in as few turns as possible to preserve vertical stability.
Source, quote & tabletop applicability
one has to limit the radial amplitude, induced from the v = 1 resonance, to a few mm.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 18
Tabletop: In a weak-focusing field the last turns sweep n from ~0.1 to ~0.5; keep energy gain high there so n=0.2 is crossed in <~5 turns.
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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 & tabletop applicability
taking eps1 = 10-4, R = 1 m and vr - 1 = 0.01, one finds an orbit centre shift, i.e. a radial oscillation amplitude, of dx = 5 mm.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 9
Tabletop: Gauss-level azimuthal field asymmetry matters at 0.59-0.89 T: it is both the knob (deliberate shim/coil bump) and the hazard (uncontrolled bumps de-center the beam).
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Brute-force first-harmonic extraction needs big bumps: in a 1.7 T field a 1 G bump adds only ~0.2 mm radial gain per turn.
dR/dn(brute force) = 0.5*R*b_N/(N*B0)Source, quote & tabletop applicability
For a typical conventional cyclotron (Bo ~ 1.7 T) a bump of 0.1 mT (1 G) introduces a radial gain of about 0.2 mm.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 14
Tabletop: Scaled to 0.6-0.9 T and r~0.1 m, tens of gauss of first harmonic would be needed to force mm-scale separation - precession is far cheaper than brute force.
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Crossing nu_r=1 with a first harmonic builds coherent amplitude over an effective resonance width of ~10 turns; after crossing, extract where nu_r has fallen to ~0.8.
x_c = pi*sqrt(2)*(b1/B)*R*n_eff (order of magnitude), n_eff = sqrt(1/(2*pi*dnu_r/dn)) ~ 10 turnsSource, quote & tabletop applicability
n_eff is the effective duration of the resonance (typically around ten revolutions). ... Typically the extraction takes place near v = 0.8.
Heikkinen, Injection and Extraction for Cyclotrons — CAS, CERN 94-01 (1994) — p. 14
Tabletop: A classical (weak-focusing) machine never has nu_r>1, so create the amplitude by ion-source off-centering instead and use the same nu_r~0.8 fringe region for precession.
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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 & tabletop applicability
An angle kick of typically 50 to 100 mrad is provided. The inner electrode, septum, is at earth potential. At the entrance it has a thickness of a few tenths of a mm, increasing to several mm at the exit.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 14
Tabletop: At 350 keV a 100 mrad kick over 10 cm of arc needs only ~5.6 kV/cm - about 2.8 kV across a 5 mm gap; at nanoamps the septum needs no cooling (~0.1 mW).
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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 & tabletop applicability
a criterion for the product of electric field E and potential V for a cyclotron deflector in order to avoid electric discharges: VE < 1.5 104 (kV)2/cm. The maximum sustainable voltage in a magnetic field is 20-30% lower.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 14
Tabletop: A 3-5 kV, 5-10 kV/cm tabletop deflector sits ~300x below this limit; the practical amateur ceiling is set by feedthrough and edge-radius engineering (the ~26 kV/cm working rule), not bulk breakdown.
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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 & tabletop applicability
At HV edges, electric field lines become so dense that breakdown becomes a major concern. Aluminum=290 kV/inch ... We settled on a minimum radius of R=.1875 inches ... Emax=170 kV/inch
Tabletop: Direct amateur precedent: a 1 T / 472 keV university tabletop deflector at 28-32 kV; a next machine needs only ~1/10 the voltage, so generous edge radii make sparking a non-issue.
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Limit stored energy into deflector arcs: a 30 kV supply plus cable stores ~0.1-0.4 J, enough to pit electrodes - add series resistance at the feedthrough and keep the HV cable short.
E_arc = 0.5*C_cable*V^2Source, quote & tabletop applicability
~0.1 Joules at 30 kV ... ~0.4 Joules at 30 kV ... The bottom plate and deflector electrode - no pitting on the electrode noticed.
Tabletop: Rutgers arced a 30 kV-rated feedthrough run at 35 kV and had to rebuild with the feedthrough inside vacuum plus a corona adapter - rate a next machine's feedthrough 2-3x over operating voltage.
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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 & tabletop applicability
For DR = 0.1R: Va = 47,000 volts ... A typical figure, used in the MIT cyclotron, is a DR of 0.15R. ... The deflector gap is usually tapered.
Livingston & Blewett, Particle Accelerators (1962) — p. 163-166
Tabletop: Scaling by 2T: a next machine at 350 keV needs ~1/45 of MIT's voltage for the same geometry ratio - about 1-3 kV across a 3-5 mm entry gap, rising if a faster peel (larger DR) is wanted.
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Expected efficiency ladder for turn-separated extraction: ~10% for early synchrocyclotron precessional extraction, up to 25% of internal beam for a well-tuned classical cyclotron deflector, 75-80% for IBA self-extraction, >90% only with well-centred beams and modern precessional/acceleration schemes.
Source, quote & tabletop applicability
Emergent beam intensities up to 25 per cent of the resonant beam intensity have been obtained under optimum conditions; ... practical operating intensities would in this case be limited to 80 or 100 [micro]a.
Livingston & Blewett, Particle Accelerators (1962) — p. 166
Tabletop: Plan a next machine around 10-25% extraction efficiency; with nA internal beam that is 0.1-0.25 nA external - still a countable, PIXE-usable beam. (Ladder rungs: botman p.2, jongen CYC2004 p.1.)
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Multi-turn extraction energy spread is ~2*q*Vdee; single-turn extraction requires RF phase width |phi| < sqrt(2/N) (a few degrees for hundreds of turns) and field stability better than dB/B ~ 2e-4.
|phi| < arccos(N/(N+1)) ~ sqrt(2/N)Source, quote & tabletop applicability
This results in a phase acceptance of only a few degrees for the typical case of a few hundred turns.
Baartman, Cyclotrons: Why/How Are Their Dynamics Different? — JINST 18 T03005 (2023) — p. 10
Tabletop: Do not chase single-turn extraction: accept multi-turn with dE ~ 2*e*Vdee (~20 keV at 10 kV dee), which PIXE tolerates. (Spread and dB/B: botman p.11-14.)
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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 & tabletop applicability
it is mostly the squared ratio of extraction radius and pole gap at extraction which determines the maximal number of turns or the minimal energy gain
Baumgarten, Cyclotron Beam Extraction by Acceleration — arXiv:2205.04124 (2022) — p. 5-6
Tabletop: A next machine with R~10 cm and half-gap 1.27 cm allows only ~9 turns (needs ~17 keV/turn); shrinking the half-gap to 6-7 mm at the edge allows ~30 turns - borderline reachable with a 5-10 kV LDMOS dee.
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H- stripping extraction is 100% efficient with a trivial device (carbon foil 50-200 ug/cm2, lifetime >2e4 uAh) and energy variable by foil radius, at the price of an H- source and stringent vacuum.
dT/T = 2*dr/r sets extracted energy spread from radial beam widthSource, quote & tabletop applicability
the negative hydrogen ion beam simply passes a thin carbon foil (e.g. pyrolytic graphite, typically 50 to 200 ug/cm2), which strips off the electrons.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 3-4
Tabletop: At sub-MeV a 50 ug/cm2 foil costs ~10 keV of energy and some scattering; every other extraction problem (septum, HV, turn separation) vanishes if an internal-source H- beam and <=1e-6 Torr can be achieved.
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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 & tabletop applicability
the cross section of H- interactions with the gas molecules is maximal for the energy range (0.1 - 300) keV of the beam in the central region.
Calvo et al., Beam Stripping Interactions in Compact Cyclotrons — PRAB 24, 090101 (2021) — p. 14
Tabletop: A next machine's H- variant spends its whole life at the cross-section peak: ~25 m of path at 1e-6 Torr loses of order 5-10%, at 1e-5 Torr most of the beam - vacuum, not physics, decides this option. (70 MeV data: cyclotron_vacuum_model p.3.)
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Lorentz (magnetic) stripping of H- has rest-frame lifetime tau = (A1/E)*exp(A2/E) with A1=2.714e-6 s*V/m, A2=4.474e9 V/m, E=gamma*beta*c*B - negligible below a few MeV even at 4 T.
tau = (A1/E)*exp(A2/E), E = gamma*beta*c*BSource, quote & tabletop applicability
a 4 T magnetic field for the maximum achievable energy of 8.5 MeV in the AMIT cyclotron corresponds to a beam-rest-frame electric field of E = 160 MV/m. This entails a marginal beam fraction loss per unit length of 1.42e-6 m-1
Calvo et al., Beam Stripping Interactions in Compact Cyclotrons — PRAB 24, 090101 (2021) — p. 7-8, 14
Tabletop: At 0.889 T and 500 keV the rest-frame field is ~9 MV/m, where the exponential makes the lifetime effectively infinite - Lorentz stripping can be ignored entirely for a next machine.
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Precessional extraction preserves beam quality because few turns separate the nu_r=1 amplitude creation from the septum, so HF phase mixing stays small - put the bump (or off-centering) as late as the field allows.
orbit-centre azimuth spread theta = 2*pi*integral (nu_r-1) dnSource, quote & tabletop applicability
the spreading of orbit centres for different HF phases due to HF mixing, is small for an originally well centreed beam, as in general the number of turns from the vr = 1 resonance till extraction is not so large.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 9
Tabletop: If a next machine uses source off-centering (amplitude created at turn 1), expect full phase mixing over 30-100 turns: the amplitude survives but its direction smears - a trim bump near the extraction region is cleaner.
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Verify turn separation before building the deflector: a differential radial probe with ~2 mm finger spacing resolves the turn pattern and the precessional oscillation near extraction.
Source, quote & tabletop applicability
Figure 11 shows a differential probe measurement for this cyclotron in the extraction region. The separation between the probe fingers is 2 mm. The figure reveals the radial oscillation near extraction.
Botman & Hagedoorn, Extraction from Cyclotrons — CAS, CERN 96-02 (1996) — p. 11-12
Tabletop: The reference machine already probes the internal beam; adding a two-finger (or shadow-bar) differential probe turns the existing radial probe into the diagnostic that decides septum placement.
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Ion bunching by the RF displaces orbit centers by Delta-r = 2D sin(theta), equivalent in the ORNL Analogue I example to ~20 turns, ~2 kV, or ~1% energy spread at the exit radius: keep it small if a monoenergetic extracted beam matters, or remove the need by AVF/flat-topping.
Delta-r = 2*D*sin(theta), D = eV/(2*m*omega^2*d) characteristic bunching displacementSource, quote & tabletop applicability
the radial displacement amplitude is equivalent to about twenty turns, or to about two kilovolts, or about 1% spread in energy at the exit radius
Goodman, A Square-Wave Cyclotron Oscillator — ORNL-2403 (1958) — p. 12
Tabletop: Sets the physics floor on energy spread from central bunching for any future extraction work; at the reference machine's and a next machine's energies the effect is small in absolute mm but the ~1%-class energy-spread scale is exactly what a deflector/slit design must budget for.
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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. Experimentally valid from 0.2 mm to at least 8.5 cm, so it covers any tabletop deflector gap.
V(kV) * E(kV/cm) = const; equivalently V ~ K*d^0.5Source, quote & tabletop applicability
for equal probability of sparking with given materials, the product of gap voltage and cathode gradient is a constant.
Tabletop: Directly. For a next machine's deflector, pick a VE number and the gap/voltage trade falls out; a 3-mm gap at VE=1.5e4 (kV)^2/cm predicts ~67 kV and ~220 kV/cm.
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Derate the deflector to VE = 1.5e4 (kV)^2/cm for day-to-day operation even though 2.25e4 was held in tests: a one-third margin below best-demonstrated holding.
VE_design = 1.5e4 (kV)^2/cm vs 2.25e4 achieved (Fig. 10 design chart)Source, quote & tabletop applicability
In order to provide an adequate margin for day-to-day operation, a design value of 1.5 X 10^4 should be used.
Tabletop: The single most quotable deflector design number, from an operating cyclotron with an in-tank vacuum no cleaner than an amateur's. Design a next machine's electrodes to 1.5e4 and treat anything above as commissioning margin.
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Electrode material ranking by measured spark damage in a magnetic field: 316 stainless, inconel, molybdenum, K-monel, titanium, and nickel comparable and best; copper, tantalum, aluminum intermediate; silver worst. Carbon resists damage but loses its bake-in within minutes of removing voltage. K-monel and nickel spark dust is magnetic (stays in the gap region).
best: 316SS/inconel/Mo/K-monel/Ti/Ni > Cu/Ta/Al > Ag; carbon anomalousSource, quote & tabletop applicability
stainless steel, inconel, molybdenum, K-monel, titanium, and nickel seem to be comparable and were the best materials. Copper, tantalum, and aluminum were intermediate. Silver showed the most severe spark damage.
Tabletop: Make the next machine's deflector electrode 316 stainless (cheap, machinable, on the best-tier list); avoid copper or aluminum HV surfaces even though they are handy shop stock.
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There is a critical magnetic field for each electrode material, ranging 4-15 kG, above which spark damage is severe and below which it is negligible; the field does not lower first-spark voltage, but crater damage accumulated in-field lowers holding voltage. Consider conditioning at reduced magnet current.
B_critical = 4-15 kG depending on material; bake in below it when possibleSource, quote & tabletop applicability
There seemed to be a critical magnetic field for each material beyond which the spark damage was severe and below which the spark damage was negligible. The critical fields ranged from 4 to 15 kG.
Tabletop: The reference machine's field (~6 kG) sits at the low edge of the 4-15 kG damage band, a real advantage. Conditioning the deflector at reduced field, then raising B, is nearly free insurance.
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Spark energy has an optimum, not a minimum: a 24-pF gap baked in to only 10 kV, adding 0.0125 uF raised it six-fold to 60 kV, but 0.5 uF cut it to 5 kV with severe craters. Bake-in is surface heating - too little spark energy leaves sharp pits, too much digs craters.
breakdown 10 kV @ 24 pF -> 60 kV @ 0.0125 uF -> 5 kV @ 0.5 uF (dc, no B field)Source, quote & tabletop applicability
when a 0.0125-uF capacitor was added across the gap, the electrodes baked-in to 60 kV, a six-fold increase. Adding a 0.5-uF capacitor across the gap reduced the breakdown voltage to 5 kV.
Tabletop: Directly sets deflector-supply philosophy - provide an adjustable, limited energy per spark (see UCRL-10655 crowbar) rather than either a stiff low-impedance supply or one that quenches sparks entirely.
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Budget conditioning time at roughly 30 sparks per cm^2 of high-voltage surface, with ~1 s of vacuum recovery per spark, i.e. ~30 s/cm^2 of bake-in; 316 stainless needs about ten times as many sparks as other materials to reach ultimate voltage.
~30 sparks/cm2; ~30 s/cm2 bake-in time; x10 for 316SSSource, quote & tabletop applicability
It takes about 30 sparks per cm2 to bake in high-voltage-electrode surfaces. Since it takes about a second for the vacuum to recover following a spark, the bake-in time of an electrode is about 30 sec/cm2.
Tabletop: A palm-sized tabletop electrode (~100 cm2) conditions in under an hour - or ~10 h if 316SS. Write conditioning into the next machine's ops checklist as a scheduled activity, not a nuisance.
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Minimize high-voltage electrode surface area by tailoring the field to the beam cross-section; less area means less bake-in sparking and less contamination collection. The 88-Inch used a 0.5-in-high field for a 0.25-in-high beam (2x margin for misalignment and median-plane shift).
field height ~ 2x beam height; radial field extent from incoherent oscillations (0.1-0.4 in at the 88-Inch)Source, quote & tabletop applicability
the high-voltage electrode should have the minimum possible surface area. This minimizes the amount of sparking required to bake out the cathode spots and reduces the amount of electrode contamination.
Tabletop: Directly. Measure the next machine's beam height at extraction radius, size the deflector field window ~2x that, and keep the HV bar as small and short as the trajectory allows.
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Keep the minimum radius of curvature of the high-voltage electrode no less than about half the gap, to prevent appreciable field-gradient magnification at edges.
r_min >= gap/2 on all HV electrode edgesSource, quote & tabletop applicability
The minimum radius of curvature of the high-voltage electrode should be large enough to prevent appreciable field-gradient magnification. In practice, the minimum radius should be no less than about half a gap.
Tabletop: Direct machining rule - for a next machine's 3-mm deflector gap, radius every HV edge to at least 1.5 mm and polish.
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Rigidly support the high-voltage electrode at both ends: a cantilevered deflector bar self-oscillates like a tuning fork (dark-current force modulation closes an electromechanical Colpitts loop, observed at 20 cps) and sparks at reduced voltage. Insulator supports raised VE from 1.23e4 to 1.47e4 immediately.
VE 1.23e4 (cantilevered, oscillating) -> 1.47e4 (insulator-supported), same crowbar settingSource, quote & tabletop applicability
At the smaller gaps the electrode vibrated like a tuning fork in a tuning-fork oscillator.
Tabletop: Very much in reach of amateur trouble - a small cantilevered electrode has low mass and compliance. Support a next machine's deflector bar on insulators at both ends and check the deflector voltage on a scope for slow oscillation buildup.
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Face the surfaces sparks land on (the spark "anodes") with tungsten sheet: 15-mil tungsten overlapped so only tungsten is exposed raised the held VE from 1.93e4 to 2.25e4 (+17%), because sparking occurs when electron power density vaporizes the anode, and tungsten vaporizes at the highest power density. Tungsten also resisted spark damage best.
VE 1.93e4 -> 2.25e4 (kV)^2/cm with W anodes (+17%); Table I Rms VE 1.57e4 (mixed metals) vs 1.9e4 (W)Source, quote & tabletop applicability
With the tungsten anodes, the VE number increased to 2.25 X 10^4 (kV)^2/cm, an increase of 17% in VE number. In addition, we found that the tungsten anodes resisted spark damage better.
Tabletop: Cheap upgrade that scales down perfectly - line the grounded surfaces opposite the next machine's HV bar with thin tungsten (or at minimum molybdenum) sheet, edges overlapped.
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With spark-current control at the supply and tungsten anodes, deflector capacitance from 67 to 580 pF made no significant difference in VE; at least 600 pF is tolerable. Lower capacitance wants higher crowbar current and vice versa. VE was also independent of magnet current over the full 167- 2500 A range.
VE independent of C_deflector 67-580 pF and of B over full range, crowbar re-optimized per pointSource, quote & tabletop applicability
we could compensate for deflector capacitance; at lower capacitance we could crowbar at higher spark currents, and vice versa.
Tabletop: Frees the mechanical design - cable runs and feedthrough capacitance in a tabletop deflector (tens of pF) are a non-issue provided the supply has adjustable spark-energy limiting.
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Carbon septa hold ~75% of metal-septum VE with no beam, but beam heating evaporates carbon onto the HV electrode and collapses voltage-holding (to ~25% of normal in the worst case), requiring a vent and solvent cleaning. A 500-uA, 32-MeV deuteron beam did not destroy the carbon septum thermally - contamination, not survival, is the failure mode. Use metal septa.
carbon VE ~1.7e4 = 75% of metal, beam-off only; contamination can cut deflector VE to 25%Source, quote & tabletop applicability
When we increased the beam current, the carbon evaporated from the septum, contaminated the high-voltage electrode, and very little voltage could be held.
Tabletop: A next machine's beam power is watts, not kilowatts, so a carbon septum's activation advantage may yet win at sub-MeV - but the contamination mechanism is temperature-driven, so thin-foil hot spots still apply. Default to tungsten/molybdenum septum, revisit carbon only with septum-temperature data.
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Dark current transports anode material to the cathode (up to 1 copper atom per 2 electrons, by evaporation) even with zero sparks, so a dissimilar anode coats and degrades the cathode; and diffusion-pump oil vapor raises dark current three orders of magnitude by cracking carbon onto electrode surfaces. Hydrogen "ion scrubbing" (200-300 micron H2, ~100 mA glow discharge from a 480-V transformer for ~1 h) reduces deflector dark current about five-fold.
dark current x1000 with oil vapor vs Hg-pumped clean system; ion scrub = 200-300 u H2, ~100 mA, ~1 h -> dark current /5Source, quote & tabletop applicability
Hydrogen is let into the vacuum tank until the pressure becomes 200 to 300 u. ... A discharge current of about 100 mA is maintained for about an hour.
Tabletop: The reference machine and a next machine use oil diffusion pumping, so expect the dirty-system dark-current regime; the ion-scrub recipe needs only a variac, a 480-V transformer, a limiting resistor, and the existing H2 feed - a directly copyable conditioning procedure.
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Diagnose whether a deflector is sparking-limited by plotting voltage vs gap on log-log: if the points follow a VE line, sparking phenomena limit; departures indicate an extraneous cause (supply parasitics, vibration, contamination). Insulate each ground electrode and meter intercepted beam current to align the deflector to the trajectory.
log V vs log d following slope of VE line => spark-limited; insulated ground electrodes as alignment monitorsSource, quote & tabletop applicability
a deflector is limited by sparking phenomena and not from an extraneous cause can be tested simply by a log-log plot of the voltage versus gap to see that it follows a VE line.
Tabletop: Both halves are free instrumentation for a next machine - a three-point V(d) test during commissioning, and an insulated septum/ground-electrode current readout for beam steering (same trick as the reference machine's Faraday-cup practice).
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Design the deflector supply to limit the energy delivered per spark, not to prevent sparks: the 88-Inch supply stores only 2.5 J at 120 kV (distributed across 1200 diodes), sparked virtually every second for 24 h/day for many days without damage, and its spark will not puncture 5-mil aluminum foil.
E_stored = 2.5 J at 120 kV; survives ~1 spark/s continuousSource, quote & tabletop applicability
it stores only 2-1/2 joules and, at most, this is distributed among 1200 diodes. ... There is so little energy in a spark from this rectifier that it will not puncture even a piece of 5-mil aluminum foil.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 28
Tabletop: The governing philosophy for any next machine's deflector supply - low stored energy is also the personnel-safety property. A sub-joule store at 50-100 kV is achievable and sufficient.
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A high-frequency Cockcroft-Walton from cheap parts is the right architecture for a sparking deflector load: six stages of 100 series silicon diodes per board (600 piv, 0.75 A each), each diode shunted by 250 pF/500 V ceramic to grade inverse voltage, 900 pF 30-kV TV-type ceramic capacitors between decks, driven at 100 kc; delivers 120 kV at 5 mA.
6-stage CW, 100 kc, 12.5 kV pk drive -> 120 kV / 5 mA; grading 250 pF per diode; deck caps 900 pF 30 kVSource, quote & tabletop applicability
Each circuit board consists of 100 Unitrode, Type UT71, silicon diodes connected in series. Each diode is shunted by a 250-pF, 500-V, ceramic capacitor to divide the inverse voltages equally.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 10
Tabletop: The 1963 'inexpensive silicon diodes + TV ceramic caps' recipe is today a standard multiplier stack; keep the two design features that matter - per-diode grading capacitors and high drive frequency (small energy per stage, fast regulation).
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Crowbar the oscillator screen grid, not the HV: a 3D22 thyratron grounding the screen stops power flow to the deflector within a few microseconds of spark detection (30-ohm ground-return shunt, capacitively coupled, RC-filtered against rf), recycles in 1 s, and the crowbar bias knob IS the spark-energy control - from invisible sparks to heavy arcs.
crowbar senses I via 30-ohm return shunt; cutoff in a few us; recycle 1 s; spark duration = f(bias setting)Source, quote & tabletop applicability
at the more sensitive positions of the crowbar current setting, the power supply can be turned off before a spark becomes visible.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 28
Tabletop: The feature to replicate in a modern build - a solid-state inverter driving a CW stack gives the same microsecond drive-kill for free (gate shutdown on an overcurrent comparator), and the threshold should be an operator knob used during bake-in, per UCRL-10654.
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Space multiplier decks ~2 in for a nominal maximum design gradient of ~10 kV/in (4 kV/cm) along the open-air column, and arrange the diode pattern so board-level gradients are minimized, with components on opposite board faces where deck-to-deck potential (up to 20 kV) appears.
air-insulated column design gradient ~10 kV/in; 12 boards in 8-in-OD lucite tube, 27 in tallSource, quote & tabletop applicability
The spacing between boards is about 2 in. and provides a nominal maximum design gradient of 10 kV per in.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 10
Tabletop: A conservative, corona-quiet air-gradient number for amateur HV column layout; at 60 kV total a next machine's stack wants ~6 in of creep/clearance headroom or potting/SF6-free oil.
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Silicon-diode storage time does not matter when rectifying into a capacitive load: the ~2-us junction-storage overshoot at 100 kc still charges the load to peak. (For operation above 100 kc, 5-MeV electron irradiation - 400 uA/cm2 for 17 min - improved rectification, cutting apparent back resistance 10x to ~200 Mohm with no change in ~900 V avalanche voltage.)
t_storage ~2 us OK at 100 kc into C-load; irradiated diodes usable >100 kcSource, quote & tabletop applicability
the diode charges a capacitive load to the peak value, and the stored charge does not subtract (appreciably, at any rate) from the output voltage.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 10
Tabletop: Historical for parts choice (modern fast-recovery diodes moot the issue) but the design insight stands - CW stacks feeding capacitive deflector loads tolerate slow diodes; spend money on voltage rating and grading instead.
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High carrier frequency buys regulation: 100-kc drive gives the regulator loop a 2500-c/s unity- gain frequency and 0.01% deflector-voltage stability, ultimately limited by the precision divider - 120 metal-film resistors (<36 ppm/C) need only ~3 C temperature uniformity (forced-air) to hold 0.01%.
f_carrier 100 kc -> f_unity 2500 c/s; 0.01% regulation; divider spec 36 ppm/C, dT < 3 CSource, quote & tabletop applicability
for a stability of 0.01% the temperature difference between resistors must be within about 3 C.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 21
Tabletop: Deflector voltage stability maps directly to extracted-beam steering stability; the lesson - regulation is limited by the divider, so buy/build the divider first - applies at any scale, and 0.01% is far beyond what a next machine needs (1% steers by ~1% of the deflection).
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Filter CW ripple using the deflector itself as the filter capacitor - a series resistor (here 100 kOhm into ~250 pF of deflector) forms a one-pole RC that attenuated 3% ripple by 15x at 100 kc, and the same resistor isolates supply-side stored energy from the spark (energy behind the resistor dissipates in it, not in the arc).
R_series=100 kOhm, C_defl~250 pF -> pole 6.7 kc, x15 attenuation at 100 kc; costs 500 V drop at 5 mASource, quote & tabletop applicability
We can attenuate this ripple by using an RC filter consisting of a series resistance connecting the Cockcroft-Walton to the deflector, and a capacitance which is the deflector capacitance.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 30
Tabletop: Two functions from one cheap HV resistor - ripple filter and spark-energy isolator (the isolation claim was independently tested in UCRL-10654 p.25). Put a 50-100 kOhm non-inductive resistor in the next machine's deflector feed.
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Magnetic shielding of glass tubes near the cyclotron is mundane but mandatory - oscillator and crowbar tubes sitting in the ~150 G stray field at the magnet yoke worked under tight-fitting 1/8-in mild-steel cylindrical caps.
~150 G stray field -> 1/8-in mild steel caps sufficedSource, quote & tabletop applicability
the deflector oscillators are located close to the magnet yoke of the cyclotron in a field of about 150 G, magnetic shields had to be put over the 4CW2000 oscillator tube and the 3D22.
Smith, Deflector Power Supply for Sector-Focused Cyclotrons — UCRL-10655 (1963) — p. 19
Tabletop: Modern solid-state supplies mostly shrug at 150 G, but CRT-style meters, vacuum gauges, photomultipliers, and any remaining tubes near a next machine's yoke need the same treatment; mild steel is enough at this level.
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Derive pulser rise time from turn separation: with ~0.1 in radius gain per rf cycle and deflector bars 1 in apart, ions cross the bar aperture in ~10 rf cycles, so the deflecting voltage must rise 10-90% in ~0.1 us (about one ion transit) and the pulse must fire within +/-5 rf cycles of the exact frequency.
t_rise ~ (bar spacing / radius gain per turn) x T_rf; here 1 in / 0.1 in = 10 cycles at ~10 Mc -> ~0.1 us (verified on page image)Source, quote & tabletop applicability
the increase in radius of the burst of ions per rf cycle is approximately 0.1 inches and the deflector bars are spaced one inch apart, the pulse must occur within +/- 5 rf cycles.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 8
Tabletop: Synchrocyclotron-specific hardware (a next machine's CW deflector needs no pulse), but the requirements chain - turn separation sets element aperture sets timing/rise budget - is the template for sizing ANY extraction element, including the next machine's septum entrance.
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The 184-inch pulsed electric deflector needed ~75,000 V/cm (about 200 kV across bars spaced one inch) to shift the center of rotation of 200-MeV deuterons enough to enter the lowered-field magnetic channel - electric extraction fields at full synchrocyclotron energy are ~10x a CW deflector's gradient, which is why it had to be pulsed.
E ~ 75 kV/cm; V ~ 200 kV across 1-in (2.54 cm) bar spacing (verified on page image)Source, quote & tabletop applicability
The electric field between the deflector bars necessary to shift the particle center of rotation enough to allow it to pass through the magnetic channel is about 75,000 volts per centimeter.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 8
Tabletop: Scale perspective - deflecting-field requirement grows with beam rigidity, and at a next machine's 300 keV-1 MeV the equivalent job needs only tens of kV/cm CW (cf. UCRL-10654's 150-200 kV/cm at 50 MeV). Sub-MeV extraction is in the easy corner of this trade.
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Derate pulsed switches for what operation does to them, not the data sheet: 5C22 thyratrons rated 16 kV arced plate-to-grid and failed above 11 kV because the plate voltage reverses in 0.3 us each shot; and one tube switching 5000 A exceeds its peak current rating ~20x, so 8 tubes were paralleled per transformer (16 total) with small individual plate-lead inductances to force current sharing.
operate 5C22 at <=11 kV (rated 16 kV) under 0.3-us voltage reversal; parallel N tubes with ballast inductance to share 5000 A each bank (verified on page image)Source, quote & tabletop applicability
These tubes cannot be operated at plate voltages above 11,000 volts, even though rated at 16,000 volts, because, in operation, the plate voltage reversed in 0.3 us causing arcing between plate and grid.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 13
Tabletop: The derating discipline (waveform-specific stress, not catalog rating) transfers to every switching element an amateur uses - MOSFET/IGBT avalanche and dV/dt limits in a Marx or inverter play the exact role the 5C22 reversal limit played here.
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To fire many parallel switches simultaneously, feed each from its own artificial transmission line: 1000-V, 20-ohm, 0.2-us triggers brought 16 thyratrons into conduction within 0.1 +/- 0.01 us, provided the trigger source impedance is low enough to charge all lines in parallel.
per-tube pulse-forming line, 1 kV / 20 ohm / 0.2 us; jitter < 0.01 us across 16 tubesSource, quote & tabletop applicability
These lines provide a 1000 volt trigger of 20 ohms impedance for approximately 0.20 microseconds. Applying this trigger to the grids results in positive ionization of all the tubes in 0.1 +/- 0.01 us.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 13
Tabletop: Classic paralleling technique still used in pulsed-power; relevant only if a next machine ever adds a pulsed element (fast chopper, kicker for time-of-flight work), but then it is the reference method.
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Fast-pulse transformer lore: keep leakage inductance down by paralleling coils and minimizing core cross-section (1.5 x 1.5 in Hipersil, 2-mil laminations); at 6 kV/turn, interlaminar insulation arcs - splitting the core into two segments halves per-segment voltage and halved those losses; ~90% of input power ends up as core heat (500 W, cores reach 200-300 C), demanding non-shorting water-cooled jackets; vacuum-fill the lucite case with de-aerated oil to kill corona. Result survived 300 kV = 3x rated output.
2:17 turns, 6 kV/turn, two coils paralleled halve leakage L; core split halves interlaminar V; tested 300 kV vs 100 kV service (verified on page image)Source, quote & tabletop applicability
Approximately ninety percent of the total power input to the system is eventually dissipated in the transformer cores as heat. At rated operating levels this loss is approximately 500 watts.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 12
Tabletop: Not needed for a CW deflector, but the de-aerated-oil corona cure, the 3x overvoltage proof test, and the interlaminar-voltage failure mode are transferable HV-construction craft for any oil-insulated amateur component.
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Specify pulse-discharge capacitors for the real waveform: they had to survive complete charge reversal in 0.3 us, 100 times per second - the best commercial units (GE 0.03 uF / 16 kV, four paralleled per transformer) still failed every 10-20 hours at 11 kV, and their ~0.13 uH internal inductance ate the rise-time budget (total allowance ~0.1 uH referred to the primary). A one-ohm line of 50 paralleled RG-8U cables worked electrically but was abandoned as bulky (6000 ft of cable).
reversal stress 0.3 us full reversal at 100 pps; L_internal 0.13 uH vs 0.1 uH total budget; MTBF 10-20 h (verified on page image)Source, quote & tabletop applicability
the capacitor must withstand a complete reversal of charge in 0.3 us 100 times a second without failure.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 14
Tabletop: The two lessons that outlive the hardware - charge-reversal duty is what kills capacitors (modern pulse caps are still specced by % reversal), and ESL budgets, not just C and V, set rise time. Cable-as-capacitor remains a legitimate cheap trick for one-off pulse work.
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DC resonance charging through the pulse capacitors' voltage reversal gives a free voltage step-up: an 11,000-V thyratron plate voltage was maintained from a 2,750-V supply (4:1, vs the textbook 2:1), because each shot leaves the capacitor reversed; ratios up to 10:1 were observed, the value depending on system losses.
V_plate/V_supply = 4:1 typical (10:1 observed) with post-pulse reversal, vs 2:1 classical resonant chargingSource, quote & tabletop applicability
a plate voltage of 11,000 volts on the thyratrons can be maintained with a power supply voltage of 2,750 volts, a step up ratio of four to one.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 15
Tabletop: Pulsed-modulator craft, not CW-deflector material; file under 'if a next machine ever needs a kicker' - it means the HV DC supply can be a quarter of the switch voltage.
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Report and accept the shortfall: measured 10-90% rise was 0.15 us against the 0.1-us requirement (blamed on capacitor internal inductance), and the fix in operation was raising peak voltage rather than rebuilding - increasing the drive compensates for a slower edge.
t_rise achieved 0.15 us vs 0.1 us spec (+50%); compensate with higher V_peak (verified on page image)Source, quote & tabletop applicability
the effective rise time is about 0.15 us, 50 percent more than that desired. ... it is felt that increasing the peak voltage compensates for the longer rise time of the pulse.
Kerns et al., High Voltage Pulser for 184-inch Cyclotron Electric Deflector — UCRL-95 (1948) — p. 16
Tabletop: A general commissioning lesson - extraction elements have one strong knob (voltage/field) that can buy back deficiencies in the others; design in voltage headroom (UCRL-10654's derating serves the same end from the other side).
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Any resonant/regenerative extraction scheme must satisfy three requirements: (a) arrest the precession so the radial-oscillation maximum recurs at one azimuth, (b) build enough radial gain per turn to step over the channel/septum wall, (c) keep axial blowup losses acceptable.
requirements: precession arrested; gain/turn > septum wall + entrance margin; axial losses boundedSource, quote & tabletop applicability
The extraction requirements, simply stated, are: (a) The precession must be arrested (b) Sufficient gain per turn must be obtained (c) Losses owing to axial blowup must be minimized.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 7
Tabletop: The cleanest checklist in this collection for what a next machine's precessional-assist extraction must accomplish - phase-lock the precession to place orbit maxima at the septum azimuth, then count gain-per-turn against septum thickness. Machine-class independent.
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Start the extraction perturbation at a "synchronous radius" defined as where the perturbation field begins and where unperturbed particles would circulate with zero radial amplitude - chosen just inside the radius of normal beam destruction (for the 184-inch, n = 0.155 at 79.8 in, just inside the n = 0.2 point). Reducing this radius eases extraction but costs extracted energy.
184-inch example n(79.8 in) = 0.155; dn/dr ~ 0.055/in inside, 0.138/in outsideSource, quote & tabletop applicability
The synchronous radius suitable for deflection in the cyclotron is just inside the radius at which normal beam destruction occurs.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 7
Tabletop: The siting logic transfers even though the numbers are synchrocyclotron pole-edge values - put the next machine's septum/regenerator equivalent just inside where the field map says the beam dies (n -> 0.2 walkout or resonance), and know that every mm inward is energy given away.
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Design a regenerator by the seven-step procedure: nonlinear equations of motion -> amplitude- dependent radial/axial frequencies from the measured field (Krylov-Bogoliubov) -> matrix analysis of radial amplitude growth and required momentum kick -> field perturbation from the kick -> resulting axial kick -> axial growth -> pick position from the family of solutions. Gain per turn follows a = -sin(wr*th1)/sin(wr*(th2-th1)); a smaller crossing interval means more gain but a stronger regenerator.
a = -sin(wr*th1)/sin(wr*(th2-th1)), wr = wr(r>R); delta(p') = -p0''*sin(wr*th2)/ sin(wr*(th2-th1))Source, quote & tabletop applicability
The determination of the required perturbation for extracting the beam of a synchrocyclotron is made in seven steps.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 6
Tabletop: The workflow (measured field -> amplitude-dependent tunes -> impulse-matrix tracking -> element strength) is exactly the CYCLOPS-lite pipeline planned for a next machine; the specific peeler-regenerator field shapes are synchrocyclotron machinery and need not transfer.
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Express regenerator strength as integrated field-times-angle: B*theta = delta(p')*B0/(1+p) gauss-radians. Worked 184-inch example (B0 = 21,730 G): 5.6 kG-deg at 0.5 in radial displacement rising to 25.6 kG-deg at 2.5 in - i.e., bump fields of order 1% of B0 over tens of degrees suffice.
B*theta = delta(p')*B0/(1+p); table 0.5->5.58, 1->11.0, 1.5->16.5, 2->22.3, 2.5->25.6 kG-deg at B0 = 21.73 kGSource, quote & tabletop applicability
When B0 is in gauss, B-theta is in gauss-radians.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 17
Tabletop: The gauss-radian bookkeeping is a handy unit for ANY azimuthally-localized field bump (harmonic coils, shims, channel compensation) on a next machine; the percent-of-B0 scale of effective perturbations is a useful sanity anchor. The specific values are 100+ MeV synchrocyclotron numbers.
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A regenerator kicks the axial motion about twice as hard as the radial motion (for 1-in axial amplitude), and particles with large axial amplitude are lost; the beam survives because the impulse period and axial period differ and the radially-falling field damps axial amplitude - so regenerator azimuth and starting radius are the free knobs to optimize extraction efficiency.
delta(z') ~ 2x radial disturbance at 1-in axial amplitude; d(axial)/dr of Br from curl B = 0 -> Br = (dBz/dr)*zSource, quote & tabletop applicability
For a 1-in. axial amplitude this disturbance is about twice as strong as that occurring in the radial motion from the same field perturbation.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 18
Tabletop: The general warning transfers - any radial-field-gradient extraction element has an off-midplane Br that pumps vertical motion, so check axial kicks in the next machine's tracker for the deflector fringe and any field bump, and expect to lose the large-axial-amplitude tail first.
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The magnetic channel's own uncorrected fringe field perturbs the beam BEFORE it enters: compute that impulse like the regenerator's and fold its compensation into the regenerator field, rather than relying on maximum-effort corrective shimming of the channel (shimming is difficult and degrades the channel).
treat channel fringe as a fourth orbit region; adjust regenerator to compensateSource, quote & tabletop applicability
The computation enables one to modify the regenerator field to account for the channel effect, and, thus, the maximum effort of corrective shimming for the channel is not required.
Stubbins, Extraction of Synchrocyclotron Beams Near the Maximum Energy — UCRL-3476 (1956) — p. 20
Tabletop: Direct analog for a next machine - the septum and exit-channel iron (or the deflector entrance fringe) perturbs the last internal turns; model that perturbation in the tracker and compensate upstream (harmonic coil/shim) instead of trying to null the channel's leakage to zero.
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RF resonant extraction: apply a radial electric field with a linear gradient (force proportional to outward displacement) over a limited azimuth, at frequency omega = 2*omega0*sqrt(1-n)/l; the radial Hill equation then becomes absolutely unstable and amplitudes grow. Choose l = 1 - it needs the least precise frequency match, which matters where the edge field (and hence radial tune) changes rapidly.
omega = omega0*2*sqrt(1-n)/l, l = 1,2,3...; perturbation F = A*rho*cos(omega*t) for rho>0 in a 60-deg sectorSource, quote & tabletop applicability
It is an advantage to choose the smallest value of l, since the choice allows the least sensitivity in matching the perturbing frequency to the particle motion.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 7
Tabletop: A genuinely tabletop-compatible extraction assist - an electrode pair driven by a small independent oscillator. For a next machine (nu_r ~ 1) the required frequency is near the orbital frequency's sidebands; worth a tracker experiment before committing hardware.
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The rf gradient needed is modest: 4.3 kV/cm (design ceiling "less than 5 kV/cm") over a 60-deg azimuth sector was enough, in IBM 650 orbit calculations for 50-MeV deuterons at 17 kG (n = 0.1), to produce substantial turn separation - and such a field is easily made by an oscillator independent of the main dee rf, tunable in frequency and amplitude.
E_rf = 4.3 kV/cm, 60-deg sector, two parabolic + one flat electrode; 50-MeV deuterons, B = 17 kG, r0 = 33.68 in, n = 0.1Source, quote & tabletop applicability
This rf electrical-field gradient, less than 5 kv/cm, is believed to be easily obtainable by an oscillator which is independent of the cyclotron oscillator and which can be tuned to the optimum frequency and amplitude.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 8
Tabletop: kV/cm-class rf on a small electrode is trivially available at a next machine's scale (hundreds of volts across a few mm). The scheme was never demonstrated on hardware in this report - treat as a promising computed option, not proven practice.
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The variable-energy argument for electric extraction elements: fixed magnetic perturbations (peeler/regenerator, channel iron) are set into the pole geometry and cannot follow a machine whose energy and field change, whereas an electrical perturbation's frequency and gradient are knobs - so variable-energy machines should extract with tunable electric systems.
tunable (f, E) replaces fixed (B-bump geometry) for variable-energy operationSource, quote & tabletop applicability
The possibility of changing the electrical frequency and gradient to match operating conditions eliminates difficulties arising in magnetic extraction systems for variable-energy machines.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 4
Tabletop: Directly supports the next machine's plan-of-record (electrostatic deflector, no fixed magnetic channel) - an educational machine that will run at more than one field/energy point wants its extraction strength on a knob, not in iron.
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Vertical beat-frequency (VBF) loss is the destructive dual of rf extraction: when the axial- oscillation frequency satisfies the resonance relation with rotation and dee frequency AND a vertical electric-field component proportional to z exists (even the weak vertical component of the accelerating gap field), the axial equation is absolutely unstable and the beam is destroyed impressively fast.
resonance f_z = |h*f_osc - k*f0|-type condition + E_z proportional to z -> absolute axial instabilitySource, quote & tabletop applicability
In the weak vertical field component of the accelerating voltage in the 184-inch cyclotron the beam loss was impressively fast.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 5
Tabletop: A real design caution at any scale - dee misalignment or asymmetric liners give exactly the z-proportional E_z this resonance needs. Keep a next machine's dee/dummy-dee vertically symmetric and check whether nu_z resonates with any strong rf harmonic at operating field.
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Do not expect an rf perturbation to kick particles out in one pass: orbits precess, take a few influential encounters, drift off the perturbation for several turns, then re-engage - but precession ultimately drives ALL particles to large radial amplitude, including those started with zero oscillation amplitude (some orbits are even temporarily damped).
amplitude growth is episodic over many turns; ultimately all phases perturbed to large amplitudeSource, quote & tabletop applicability
because of the precession of orbits all particles are ultimately perturbed to larger radial oscillation amplitudes.
Stubbins, Radiofrequency System for Extracting Particles from a Cyclotron — UCRL-8578 (1958) — p. 9
Tabletop: Sets expectations for any resonant/precessional scheme on a next machine - extraction is a many-turn statistical process, so judge schemes in the tracker by turns-to-extraction and septum-hit fraction, not single-pass kick size.
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Split a deflector/extraction trigger into two stages: a frequency-sensitive circuit that GATES, and a phase-sensitive circuit that TRIGGERS - because no frequency measurement can be accurate enough to also fix the RF phase of the firing instant.
Source, quote & tabletop applicability
The frequency-sensitive circuit "gates" the phase-sensitive circuit, and the phase-sensitive circuit triggers the deflector.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 168
Tabletop: The architecture for any timed kick against an extraction gap, on a next machine or a small synchrotron - a coarse condition (frequency, turn count, integrated field) opens a window, and the RF itself supplies the fine phase. Two easy measurements replace one impossible one.
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To detect when a swept RF reaches a chosen frequency, do not build a stable tunable RF filter (it cannot be built stably enough); heterodyne the RF against a crystal local oscillator and detect the transient through a FIXED low-frequency band-pass filter, making the trigger point variable via the low-frequency side and crystal switching.
trigger when f_dee - f_crystal = f_filter (~1 Mc); variable 1-1.25 Mc filter + switched crystals covered 19-21.5 McSource, quote & tabletop applicability
Block 4 is a local oscillator with a frequency about 1 megacycle below the desired deflection frequency P. When the dee-oscillator signal sweeps through point P, the 1-megacycle filter passes an a-c transient.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 168-169
Tabletop: Classic measurement doctrine - move precision to a fixed low frequency where stability is cheap. The same trick (mix dee RF down, detect at fixed IF) is how a modern amateur frequency/turn marker gets crystal accuracy with junk-box filters.
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It is theoretically impossible to filter a transient without introducing time delay - so do not fight detection delay, MEASURE it and compensate at the trigger threshold (they bias the trigger to fire earlier on the pulse rise).
Source, quote & tabletop applicability
Unfortunately it is theoretically impossible to filter a transient without introducing time delay. The time delay thus introduced was kept to a minimum.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 170-171
Tabletop: General fast-timing wisdom for beam-pulse and kick timing chains - every smoothing stage costs latency; calibrate the chain end-to-end and remove the constant part in the threshold or delay setting rather than chasing zero-delay filters.
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A swept signal peaks in a band-pass filter LATER than the moment it crosses the filter's center frequency, by a delay depending on filter bandwidth and sweep rate - so trigger calibration must be repeated per sweep rate (they provide a per-repetition-rate bias switch).
peak delay = f(filter bandwidth, df/dt of sweep); their sweep ~2500 Mc/sSource, quote & tabletop applicability
the time at which the transient is at a peak is somewhat later than the time at which the dee-oscillator frequency is in the center of the filter pass band.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 171-172
Tabletop: Matters wherever a resonant pickup watches a changing frequency - including a synchrotron RF ramp or an FM-tuned marker on a cyclotron; if the ramp rate changes, the timing calibration silently moves.
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Reference a trigger threshold to the MEASURED critical firing voltage of the actual trigger device, not to ground - find the just-fires bias experimentally ("slide" it up until firing starts), lock it, and make all compensating adjustments relative to that point, so device aging drops out.
Source, quote & tabletop applicability
the bias adjustment is made with reference to the actual critical firing voltage.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 172
Tabletop: A self-calibration idiom worth copying into any comparator/discriminator in the DAQ - trim to observed threshold at session start (their multivibrator = today's comparator with drifting offset), and slow drift stops moving the physics timing.
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Gain-stabilize a sparse narrow-pulse chain with a PEAK-reading automatic level control (average- reading AGC fails because the duty cycle is tiny), and put its detector at the FINAL trigger point so the loop compensates every gain stage at once, whatever the drift source.
Source, quote & tabletop applicability
the automatic pulse-height circuit had to work on a peak-reading principle.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 171
Tabletop: Directly applicable to pulse chains fed by beam pickups or PMTs at low rep rate - stabilize on detected peak height at the discriminator input, and amplitude drift stops translating into time walk.
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Suppress an unwanted (image) response by DISABLING the circuit during the time window when it occurs, rather than by building sharp switchable filters - simple time-gating was chosen precisely because high-frequency switching circuits invite unforeseen trouble.
Source, quote & tabletop applicability
That alternative was abandoned in view of the susceptibility of high-frequency switching circuits to unforeseen difficulties.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 172
Tabletop: A complexity-avoidance rule with 2026 force - blanking a known-bad time window (one line of firmware now) beats analog cleverness whenever the artifact's timing is predictable.
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Benchmark for a home-built trigger discriminator, vacuum-tube era: from a 3 mV rms sample of the dee RF (50 ohm), fire within <1 microsecond of the chosen frequency on a 2500 Mc/s sweep, delivering 7 V / 1.2 us / 0.2 us-rise pulses into 73 ohms - achieved with 27 ordinary tubes.
input 0.003 V rms/50 ohm; output 7 V pk, 1.2 us, 0.2 us rise, 73 ohm; probable firing error <1 us; range 19-21.5 McSource, quote & tabletop applicability
Probable error in firing time, <1 microsecond. Range of firing frequency, 19 to 21-1/2 megacycles, with provision for changing this.
Foss et al., Cyclotron Component Design Technical Reports — TID-454 (1952) — p. 174
Tabletop: Calibrates ambition - microsecond-class event timing off a tiny RF sample needed no exotic parts in 1952; any modern comparator + MCU implementation should beat it by orders of magnitude, so the architecture (not the hardware) is the thing to copy.
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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 & tabletop applicability
A very effective adjustable beam deflector has been developed; under the best conditions, 38% of a 1000 ua internal beam has been deflected.
Tabletop: Sets expectations for any future extraction gate on a next machine - design the septum/deflector with in-vacuum adjustability and count a 30-40% extracted fraction as success on a first small machine.
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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 & tabletop applicability
The extreme radioactivity induced in type 304 stainless steel makes its use undesirable, the use of an aluminum alloy is now being investigated.
Tabletop: At reference-machine and next-machine energies activation is negligible, but the selection logic transfers to the planned higher-power machines and to the business plan's licensing story - prefer aluminum/graphite for probes, septa, and slits anywhere protons above a few MeV are contemplated.
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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 & tabletop applicability
in order to produce a suitable object for the analyzing magnet, we introduce a second magnet whose sole function is to focus as much of the beam as possible on a precision slit.
Tabletop: DIRECT - this is the canonical two-stage architecture for any external line on a next machine. The optical condenser/analyzer analogy (illuminated slit as object) is the cleanest possible statement of why "focus first, analyze second" beats one clever magnet.
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Resonant extraction works by making the stable center of phase space jump: the first-harmonic bump causes the equilibrium orbit and an unstable fixed point to merge and vanish as energy rises, so the surviving stable point is elsewhere (S1) — the beam suddenly finds itself executing a large-amplitude oscillation, and that amplitude is the turn separation.
Source, quote & tabletop applicability
introduction of the field bump has caused a discontinuous jump in the location of the central stable orbit in the phase diagram
Tabletop: The conceptual mechanism to have in hand before any extraction attempt on a next machine; it needs nu_r to pass unity with a controlled first harmonic — both quantities a FEMM-fed tracker can compute for a candidate pole design.
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State the beam-optics acceptance criterion in phase-space language: performance is good if a beam-sized ellipse remains an ellipse through the system — stretching and rotation are acceptable (downstream lenses accommodate them), twisting and filamentation are not (they mix filled and empty phase space irreversibly).
Source, quote & tabletop applicability
stretching and rotation are fine but not twisting, filamentation, etc.
Tabletop: The right figure of merit for any next machine's beamline or extraction simulation — track a small grid of particles and judge the deformed shape, not just the centroid; five to two dozen particles sufficed in 1961.
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Distortion bookkeeping: motion of the beam spot driven by flow-rate gradients on a fixed static plot (the "static effect") stretches, bends, shears, and filaments the beam; motion driven by the plot itself shifting with energy (the "acceleration effect") moves the beam without deforming it. Design rule: program the turns to avoid flow-gradient regions — especially near unstable fixed points.
Source, quote & tabletop applicability
The essential design requirement of such a system is a turn program which avoids regions of large flow rate gradient in the static phase space.
Tabletop: The doctrine transfers whole to any resonance-crossing scheme on a small machine — cross fast where the map is ugly; the diagnostic (superimpose the accelerated beam path on static phase plots) is a cheap tracker post-processing step.
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Energy gain per turn is the master knob of resonant extraction quality: rerunning the same beam at half (140), design (280), and double (560) kV per turn showed the high-voltage case notably well behaved and the conclusion that substantially lower volts/turn sharply degrades BOTH extraction efficiency and optical quality — the beam must cross the bad region of phase space quickly.
turn separation achieved: 0.006 cyc units between the 14th and 15th turns (hand-corrected figures) for a 0.002 cyc-unit beam at 280 kV/turnSource, quote & tabletop applicability
volts per turn substantially lower than the designed 280 kev/turn would result in sharp reduction of both extraction efficiency and optical quality.
Tabletop: The quantitative ancestor of "dee volts buy extraction" — the reference machine's ~800 V nominal dee is why it is internal-beam-only, and the next machine's 5-13 kV target is what would make any future extraction scheme even thinkable.
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Let the computation overrule the folklore: tracking showed beams entering the extraction region centered on the equilibrium orbit behave as well or better than deliberately displaced beams — contradicting the group's own earlier qualitative proposal (MSUCP-2) that displacement would help.
Source, quote & tabletop applicability
beams entering the extraction region approximately centered on the equilibrium orbit behave as well or better than beams entering with substantial displacement.
Tabletop: The project-level lesson for a next machine — run the cheap simulation before committing hardware to any orbit-dynamics intuition, including intuitions published by people as good as Blosser and Gordon.
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Taper an extraction-channel septum from thin at the entrance to thick downstream — once turn separation grows, thickness is free — cutting resistive power severalfold and multiplying coolant flow at the same supply pressure.
Nevis: 0.125 in. entrance -> 0.600 in. by 16 in. along channel; power 160 kW-equivalent -> 40 kW (4x)Source, quote & tabletop applicability
This septum will use only 40 kW of power, a factor of four smaller than if the original thickness were kept to the end
Tabletop: A current-septum channel is beyond tabletop needs, but the geometric principle — septum thickness need only be minimal on the first intercepting turn — applies to any deflector septum or foil design on a next machine.
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Interlock actively cooled beam-intercepting conductors individually: give each element its own temperature sensor on the coolant that trips the supply, plus continuously filtered and de-ionized water, because a cooled conductor melts within seconds of flow loss.
per-wire thermocouple -> fast current trip; filtered + de-ionized cooling loopSource, quote & tabletop applicability
each wire will have its own thermocouple to sense any rise in the cooling water temperature which will shut off the current in the channel
Tabletop: Per-element thermal interlocks scale down perfectly — the same philosophy belongs on the next machine's RF amplifier dummy load, water-cooled dee stubs, and any powered septum, and matches the fail-safe interlock doctrine in the 1974 ORNL safety survey.
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Magnetic forces on current-carrying structures deform them in service: the iron channel's internal copper walls collapsed whenever coil current exceeded 2000 A (found by remote instrumentation, costing ~60% of the extracted beam); the fix - G-10 glass-epoxy stiffeners - was verified by MEASURING deflection (0.002 inch at 3500 A) against the material elastic limit, and the balky drive motors were moved from 50 to 80 inches from the source, out of the field.
verify a structural fix by measuring deflection at above-operating excitation and comparing induced stress to elastic limitSource, quote & tabletop applicability
with the coils energized to 3500 amperes, revealed a negligible deflection of the inner walls (about 0.002 inch) which eliminated the possibility of future collapse
Tabletop: Every conductor near the pole gap feels J x B; thin walls, septa, and coil leads need either stiffening or a measured demonstration that deflection at full excitation stays elastic - and motors, encoders, and anything with a magnetic circuit belong outside the fringe field.
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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 & tabletop applicability
Machining work will begin after the oscillator is operating and an internal beam produced.
Tabletop: The corpus's commissioning-order lesson (internal beam -> then extraction) stated as an explicit 1951 schedule decision. For a next machine, budget the probe and its lock as first-beam hardware and hold extraction hardware at the drawing stage until the field and RF are proven.
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Deflector design choices from the UW study: shorten from 90 to 70 degrees (starting 60 degrees beyond the dee gap) for mechanical stability of the control mechanism; keep the deflector plate at RF GROUND and use the RF field between plate and grounded dee edge for deflection, supplementing with DC only when dee voltage runs below ~120 kV; phase analysis sets a floor — at least 80 kV dee-to-ground RF so ions "do not enter the region of decelerating phase at any time within the dees" (with ~34 kV of DC then needed); channel width remotely variable (1/4 to 1 in, 60 kV / 20 mA supply), widen for flux or narrow to a constant 0.90 cm for energy selectivity — expected spread ~1.5 MeV about 21 MeV, with the useful-intensity core ~1 MeV.
UW: 70-deg deflector from 60 deg past gap; >=80 kV RF floor; DC supplement below ~120 kV dee; selective channel 0.90 cm -> ~1.5 MeV spread at 21 MeVSource, quote & tabletop applicability
a minimum of 80 kv dee to ground r.f. potential is necessary in order that the ions do not enter the region of decelerating phase at any time within the dees.
Tabletop: The RF-ground deflector-plate trick (steal the existing dee field, add DC only as a supplement) and the adjustable-channel flux-vs-resolution trade are scale-free ideas for any future extraction study on a next machine; the phase-floor analysis is the kind of computation this collection's deflector cluster (nyo-9360 etc.) expects before metal is cut.