The SARAF CW 40 MeV Proton/Deuteron AcceleratorRFQ voltage squared vs. forward power 250 300 4-Jul...
Transcript of The SARAF CW 40 MeV Proton/Deuteron AcceleratorRFQ voltage squared vs. forward power 250 300 4-Jul...
The SARAF CW 40 MeV Proton/Deuteron Accelerator
A. Nagler, D. Berkovits, I. Gertz, I. Mardor, J. Rodnizki, L. WeissmanS NRC Y I lSoreq NRC, Yavne, Israel
K. Dunkel, M. Pekeler, F. Kremer, C. Piel, P. vom SteinAccel Instruments, Bergisch Gladbach, Germany
LINAC08, MO203, September 29th, 2008
SARAFSARAF – SSoreq AApplied RResearch AAccelerator FFacilityAAccelerator FFacility
To modernize the source of neutrons atTo modernize the source of neutrons at Soreq and extend neutron based research and applicationsresearch and applications. To develop and produce radioisotopes primarily for bio medical applicationsprimarily for bio-medical applications.To enlarge the experimental nuclear
i i f d hscience infrastructure and promote the research in Israel.
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Accelerator Basic Characteristics
A RF Superconducting Linear Accelerator
ParameterParameter Val eVal e CommentCommentParameterParameter ValueValue CommentCommentIon Species Protons/Deuterons M/q ≤ 2
Energy Range 5 – 40 MeV
Current Range 0.04 – 2 mA Upgradeable to 4 mA
Operation mode CW and Pulsed PW: 0.1-1 ms; rep. rate: 0.1-1000 Hz
Operation 6000 hours/yearOperation 6000 hours/year
Reliability 90%
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Maintenance Hands-On beam loss < 1 nA/m
SARAF Layout
RF Superconducting Linear Accelerator Target Hallp g g
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A. Nagler et al., LINAC 2006
SARAF project organization
Construction and Commissioning of a (Beyond-)State-of-the-Art accelerator within an international business collaboration
Accelerator – Accel Instruments (Germany)Cryogenics Linde Kryotechnik (Switzerland)Cryogenics – Linde Kryotechnik (Switzerland)Building and Infrastructure – U. Doron (Israel)Applications - Soreq
Overall Integration Soreq
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Overall Integration – Soreq
SARAF Phase I – Upstream View
PSM
EIS
RFQMEBT
S
EISLEBT
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SARAF Phase I – Downstream View
PSM
D-Plate
B D 1Beam Dump 1Beam Dump 2
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ECR Ion Source (ECRIS)C Pi l EPAC 2006
Plasma chamber
High voltage
extractor
Magnetic solenoid
Focusingl id
C. Piel EPAC 2006
F. Kremer ICIS 2007
K. Dunkel PAC 2007
beam
Vacuum pump
RF Waveguide& DC-breaker
solenoid
magnetic lipump 5x10-6
mbar
RF power
gcoils on ground
cooling water
gas inlet
p800 W
RF power supply
extraction electrodes
20 kV/u
g1 sccm
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20 kV/u
107 mminsulator
LEBT – emittance measurement
C. Piel EPAC 2006
F. Kremer ICIS 2007
magnetic mass
analyzer
FC
K. Dunkel PAC 2007
P. Forck JUAS 2003ECRaperture
wireslitaperture
2003ECR
5 mA proton beam optics
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beam optics
RFQ entranceECR
EIS: measured emittance values
ε 100% [π mm mrad]Particles
Beam currentProtons
X / YH2+
X / YDeuterons
X / Y
εrms_norm._100% [π mm mrad]
5.0 mA 0.20 / 0.17 0.34 / 0.36 0.13 / 0.12
2 0 mA 0 13 / 0 13 0 30 / 0 34 0 14 / 0 132.0 mA 0.13 / 0.13 0.30 / 0.34 0.14 / 0.13
0.04 mA 0.18 / 0.19 0.05 / 0.05
Specified value = 0.2 / 0.2 [π mm mrad]
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deuterons emittance resultsπ mm mrad2D plot current scale
1 0
3 0
Elliptical Exclusion
0 2
0.25
0.3
Emit. deuterons
2D plot current scale is enhanced in order to present the tail
- 3 0
- 1 0
1 0 x' [mrad]
0.05
0.1
0.15
0.2
Nor
m. R
MS
E
6.1 mAopen
aperture
SCUBEEx Analysis
- 3 0 - 1 0 1 0 3 0- 5 0
x [ m m ]
00 1400 2800 4200 5600 7000
Exclusion Ellipse SAP
B. Bazak
0 06
0.08
0.1
0.12
RM
S Em
it.aperture
1 0
3 0
x' [mrad
JINST 2008
0
0.02
0.04
0.06
0 1400 2800 4200 5600 7000
Nor
m. R cut to
5.0 mA- 3 0
- 1 0
d]
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0 1400 2800 4200 5600 7000Exclusion Ellipse SAP- 3 0 - 1 0 1 0 3 0
- 5 0
x [ m m ]
emittance analysis with the SCUBEEx code by M. P. Stockli and R.F. Welton, Rev. Sci. Instr. 75 (2004) 1646
176 MHz Radio Frequency Quadrupole
On site 2006
In factory 2005
P. Fischer EPAC 2006
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RFQ commissioning resultsSpecifications in parentheses
Protons Parameter 1.5 1.5 (1.5)(1.5)Output energy [MeV/u]4.0 4.0 (4.0)(4.0)Maximal CW current [mA]
Transverse emittance, r.m.s., normalized, 100% [π·mm·mrad]
0.17 0.17 (0.30)(0.30)normalized, 100% [π mm mrad](at 0.5 mA, closed LEBT aperture)
0.25 / 0.29 0.25 / 0.29 (0.30)(0.30)(at 4.0 mA, open LEBT aperture)
30 30 (120)(120)Longitudinal emittance, r.m.s [π·keV·deg/u](at 3.0 mA)
80 80 (90)(90)Transmission [%] (at 0.5 mA) ( )( )[ ] ( )70 70 (90)(90)(at 2.0 mA)65 65 (90)(90)(at 4.0 mA)6262 (55)(55)R i d RF ( ) [kW]
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62 62 (55)(55)Required RF power (protons) [kW]248 248 (220)(220)(deuterons) [kW]
Diagnostic plate (D-Plate) for beam commissioningfor beam commissioning
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Proton energy at RFQ exit by TOFBeam Energy Measurement using TOF
between 2 BPMs sum signals, 145 mm apart, E =E = 11..504504 ±± 00..012012 MeVMeV C. Piel PAC 2007E E 11..504 504 ±± 00..012 012 MeVMeV
Button pickup for 2 mA pulse and
15 mm bore radius gives a
signal high above noise.
Bunch width measured atmeasured at
β=0.056 is larger than the predicted value due to the induced charge
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induced charge broadening.
Current downstream RFQ vs. RFQ forward power for 3 mA injectionforward power for 3 mA injection
sum of 4 BPM2.5
D-Plate MPCT [mA]
Optimum power for p = 61.5 kW
sum of 4 BPM current signals
2.0
D-Plate_MPCT [mA]
A_MBPM1 [V_p]
A_MBPM2 [V_p]
4D-WB simulation [mA]
MPCT current1.5
m c
urre
nt
4D WB simulation [mA]
0.5
1.0
Bea
m
0.0
0.5
45 50 55 60 65 70 75
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45 50 55 60 65 70 75
RFQ power (PS forward) [kW]J. Rodnizki et al. EPAC 2008
RFQ: Bunch profiles measurements
Wire scan profiles0.8
1meanm 0.00 cmFWHMs 0.40 cmFWHMm 0.46 cm
meanm 0.00 cmFWHMs 3.70 cmFWHMm 3.57 cm
M t
C. Piel PAC 2007
0.2
0.4
0.6
coun
ts
32.0 kV
61.5 kW
MEBT Entrance
D-PlateMeasurement
results are backed up by simulations
(TRACK)
-4 -2 0 2 40
position (cm)4 -2 0 2 4
position (cm)1.2
gauss fitsimulated
gauss fitmeasurementFFC1 FFC1
Entrance
(TRACK)
FFC time profiles0.6
0.8
1.0
nt (a
rb.)
simulatedgauss fit
measurement
32.5 kV 63.5 kWSimulation Measured
Rodnizki et al. EPAC 2008
p
0.2
0.4curr
en
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EPAC 20080.0
0 100 200 300proton relative phase (deg)
0 100 200 300proton relative phase (deg)
Approximated rms εZ extracted from bunch width measurementsfrom bunch width measurements
75
90ez (RFQ) [pi deg keV]1s at FFC1 [deg]1s at FFC2 [deg]
C. Piel EPAC 2008
60
75 1s at FFC2 [deg]s_f at RFQ [deg]s_E at RFQ [keV]
30
45 Optimum power for p = 61.5 kW
15
30
055 60 65 70 75
power RFQ [kW]
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p Q [ ]
Specified rms εZ = 120 120 ππ deg keVdeg keV Value for simulations = 74 74 ππ deg keVdeg keV
RFQ voltage squared vs. forward power
250
3004-Jul9July10J l
080808
200
^2(k
W)
10JulyLinear
08
100
150
Pick
up V
^
0
50
00 50 100 150 200 250 300
FPower (kV)Forward power (kW)
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Parting from the linear relation indicates onset of dark current due to poor conditioning
RFQ Conditioning – current statusA few hundred conditioning hours for two yearsA few hundred conditioning hours for two yearsConditioning schemes
Set ma im m po er and increase d t c cleSet maximum power and increase duty cycleSet CW duty cycle and increase power
Special actions to improve conditioning rate:Special actions to improve conditioning rate:Rounding off sharp edges of rods bottom partCleaning of rodsCleaning of rodsInstallation of circuit for fast recovery after sparks
Maximal power reached so far:p195 195 kW CWkW CW280 280 kWkW with duty cycle of 1515%%
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75°C baking performed recently for 3 days. Effect on conditioning tp be measured soon
Prototype SC Module (PSM)General Design:• Houses 6 HWR and 3
superconducting solenoids• Accelerates protons and
deuterons from 1.5 MeV/u on• Very compact design in
longitudinal direction• Cavity vacuum and
insulation vacuum separated
A. Nagler et al., LINAC08, MO203 219/29/2008 21M. Peiniger, LINAC 2004 M. Pekeler, SRF 2003 M. Pekeler, LINAC 2006
HWR – Basic parameters
• f = 176 MHz & bandwidth ~ 130 Hz
height 85 cm high• height ~ 85 cm high
• Optimized forβ=0 09 @ first 12 cavities (2 modules)β=0.09 @ first 12 cavities (2 modules)
β=0.15 @ 32 cavities (4 modules)
B lk Nb 3 @ 4 45 K• Bulk Nb 3 mm @ 4.45 K
• Epeak, max = 25 MV/m & Epeak / Eacc ~ 2.5
• Q0 ~ 109
• Designed cryogenic Load < 10 W (@Emax)
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HWR measured fields and dissipated power
Closed loop operation with a voltage
At Accel (single cavity) At Soreq (inside PSM)max field limit Q at Q at losses at losses at
Closed loop operation with a voltage controlled oscillator (VCO)
20 MV/m 25 MV/m 20 MV/m 25 MV/m[MV/m] [W] [W]
30 8,0E+08 7,0E+08 3,5 6,3
28 l 2 0E 08 1 4E 08 14 1 31 428 coupler temp. 2,0E+08 1,4E+08 14,1 31,4
32 4,0E+08 2,0E+08 7,0 22,0
29 4,0E+08 2,0E+08 7,0 22,0
31 7,0E+08 4,0E+08 4,0 11,0
29 coupler temp. 7,0E+08 3,0E+08 4,0 14,7
Σ 39,7 107,3 , ,
Target values 25 4.7E+08 25 4.7E+08 72
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C. Piel et al. EPAC 2008
Phase and amplitude stability results
SARAF LLRF:Generator driven resonator (GDR)resonator (GDR) cavity tuning loop
• Above results are for operation of one cavity at a time• Stability measurement period was a few minutes for each cavity
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• Stability values are peak-to-peak and are limited by ADC least significant bit Recent commissioning: simultaneous operation of 6 HWRs at ~20 MV/m for several hours
Residual activation from beam loss
A beam loss value of 00 44 nA/mnA/m at 40 MeVA beam loss value of 00..4 4 nA/mnA/m at 40 MeV generates 2 mRem/hr after a 1 year irradiation
30 cm from beam line4 hours after h td
Conditions
shutdownEffects of 40 MeV applied for entire linacAccelerator isAccelerator is operating 365 days per year (~65%)Run deuterons at 40Run deuterons at 40 MeV all the time (25-50%)Accelerator made
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entirely of stainless steel (~50% Nb)40 MeV Linac (22 m) Beam line (10 m)
SARAF Phase II simulations with error analysiswith error analysis
Si l i h iSimulations shown in next slides:• 4 mA deuterons at RFQ entrance.entrance. • Last macro-particle=1 nA
B. Bazak et al., Submitted for Publication
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Errors are double than in: J. Rodnizki et al. LINAC 2006, M. Pekeler HPSL 2005
J. Rodnizki et al., HB2008
Deuteron beam envelope radius at SARAF SC Linacradius at SARAF SC Linac
200 realizations 70 realizationsSolenoids 19 Tail emphasis simulationsTail emphasis simulations
Bore
rmax
rRM
S
nominal
RFQ exit3.4 mA deuterons
32k/193k particles in core/tailLast macro-particle = 1 nA
S
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pGeneral Particle Tracer 2.80 2006, Pulsar Physics S.B. van der Geer, M.J. de Loos http://www.pulsar.nl/
B. Bazak et al., Submitted for PublicationJ. Rodnizki et al., HB2008
Summary and OutlookSARAF Phase I Commissioning status:SARAF Phase I Commissioning status:
Extensive proton beam commissioning through RFQ performedperformedFirst deuteron and H2
+ beams accelerated in RFQOn-going RFQ RF conditioning to enable CW deuteron andOn going RFQ RF conditioning to enable CW deuteron and H2
+ beamsRF commissioning of the PSM to enable beam acceleration through it
Simulations of Phase IIBeam loss criterion for hands-on maintenance is 0.4 nA/m at 40 MeVTail emphasis sim lations indicate beam loss belo 1 nA/m
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Tail emphasis simulations indicate beam loss below 1 nA/m