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Proton Driver b1 R

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Title: Proton Driver b1 R


1
Proton Driver blt1 RD
  • Giorgio Apollinari
  • April 10th - 12th , 2005

2
Outline
  • Ion Source
  • Radio Frequency Quadrupole (RFQ)
  • Medium Energy Beam Transport MEBT
  • Room Temperature Resonators section
  • Superconducting spoke resonators sections
  • Single Spoke, Double Spoke (and Triple Spoke)
    resonators
  • Squeezed Elliptical Superconducting Cavities
  • b(0.47, 0.62) 0.81 resonators
  • Conclusions

3
Goal of the System
  • Increase H- energy from E0 MeV to E1200 MeV.
  • Multiple geometrical bs 0.21, 0.4, ( 0.47, 0.61
    for elliptical cavities or 0.61 for spoke
    cavities) and 0.81

Cavity Accelerating Gradient
(Elliptical Cavity Option for Beta0.47 and 0.61)
Epeak 52 MV/m, Phi_Synch -30 to -15 degrees
30
Accelerating
Beta 1.00
Gradient Eacc
Beta 0.81
25
Eacc TTFCos(f)
Beta
0.61
20
Gradient (MeV/m)
Beta
0.47
15
10
5
0
1
51
101
151
201
251
301
351
Elliptical Cavity Number
4
Front end general layout
  • Ion source H-, LEBT 0.065 MeV
  • Radio Frequency Quadrupole 4-5 m, 3 MeV
  • MEBT (2 bunchers, 4 SC sol., chopper) 4 m
  • RT TSR section (21 resonators, 21 SC solenoid)
    10 m 15.2 Mev
  • SSR section (16 resonators, 16 SC solenoids)
    12.5 m 33.5 MeV
  • DSR section (28 resonators, 14 SC
    solenoids) 17 m 108 MeV
  • TSR section (42 resonators, 42 quads) 64
    m 408 MeV

Frequency 325 MHz Total length 112 m
5
Ion source
  • The ion source is a multicusp, rf-driven, cesium
    enhanced source of H-.
  • Output energy 65 keV, output peak current 12.7
    (38) mA, pulse length 3.0 (1.0) ms, pulse rate
    2.5(10) Hz
  • Design concept - SNS,DESY
  • Design issues in general these
  • sources are well understood.
  • SNS ion source can be used for
  • PD. Longer RF antenna lifetime
  • desirable.

6
Toward Selecting an H- Ion Source
  • Beam tests on the SNS RF H- ion source (Doug
    Moehs)
  • 3.1 ms long pulse, 11.5 mA average, at 5 Hz
  • The SNS routinely runs 1 ms long pulses, 30 mA at
    60 Hz

The SNS Ion Source Test Bench and LEBT
  • Jumpstart with H source with 100 kV 10 mA PS
    and 50 keV output

7
RFQ
  • RFQ accelerates H- from 0.065 to 3 MeV , Ip up
    to 28 mA
  • Now RFQs are standard devices for proton
    machines. There are good designs (J-PARC, SNS)
    available.
  • Our additional requirement for RFQ beam dynamics
    design is an axisymmetric output beam to reduce
    halo formation in MEBT and RT SR section.
    (P.Ostroumovs proposal).

J-PARC 30 mA RFQ
8
RFQ
  • For the RFQ mechanical design the main issues
    are
  • Machining of large parts with high accuracy ( 25
    microns for vane tips)
  • Assembly the RFQ body. Brazing (SNS approach),
    though clamping or laser welding with ring
    contacts works well too (J-PARC).
  • Currently basic RFQ parameters are found. RF
    design and mechanical design are planned to be
    done by ANL-FNAL collaboration.

9
RFQ
  • or AccSys !

10
MEBT
  • MEBT has three main functions
  • matching the beam from the RFQ exit plane into
    the MEBT chopper plane
  • cleanup chopping
  • matching the remaining particles into the RT TSR
    section ( beam diagnostic)


CERN-SPL System Deflecting structure
11
MEBT
  • In our MEBT we have an axisymmetric beam after
    RFQ.
  • 4 SC solenoids are used for focusing and matching
  • 2 RT TSR are used as the rebunchers
  • One chopper
  • This is conceptual design. The detailed design is
    still ahead.

SC solenoid
MEBT
RT SR
TRACK simulation
12
MEBT
  • The MEBT installed at KEK.

13
MEBT SC Solenoids
  • First Prototype be Oct. 05

Stresses at 0 A, 4K
14
RT SR section
  • Why this room temperature section?
  • Beam dynamics at low beta demands adiabatic
    acceleration, smooth transition from RFQ to SC
    sections which have high accelerating rate.
  • That means
  • - variable beta accelerating lattice - gaps
    and distances between them change with particle
    velocity
  • - focusing period should be as short as
    possible
  • - smooth increasing of accelerating rate
  • It is expensive and difficult to design and
    produce beta variable SC cavities. This is not a
    problem for RT cavities

15
RT SR section
  • Our solution is Room Temperature Spoke Resonator
    (aka Cross-bar H-type resonators) section from 3
    MeV to 15 MeV .

Solenoid in individual cryostat
Shape Optimization
16
RT TSR section
  • The main advantage of RT SR is its high shunt
    impedance.
  • For 3-15 MeV losses in copper
  • DTL 1.06 MW
  • RT SR 0.4 MW
  • Diameter of resonator
  • DTL, SDTL 70 cm
  • RT SR 40 cm
  • RT SR expected to be cheaper

RT TSR
SDTL (J-PARC)
DTL (J-PARC)
17
RT SR section
There no prototypes of RT SR and SC solenoids
that meet our requirements , but we can find
similar efforts elsewhere
Cold model of CH resonator (Frankfurt).
SC quadrupole lens in individual cryostat
(Berkley)
18
SC Spoke Resonator
  • SC Spoke Resonator sections provide acceleration
    from 15 MeV up to 400 MeV.
  • RD work to study and optimize all three types of
    resonators

19
SC Spoke Resonator
  • Spoke Cavities and CryoModules
  • Why Spokes
  • Fewer types higher operating T (4 K)
  • Simulation shows that improved beam quality can
    be expected (increased
  • longitudinal acceptance)
  • Superior mechanical stability for blt0.6
  • Decade-old technology (Delayen et al., LINAC 92)
  • Open to Elliptical cavities processing conditions
  • HPR
  • Ultra-clean processing

Argonne, Spring 2001
Q
Argonne Result b0.4 cavity
20
SC Spoke Resonator
Shepard, Kelly, Fuerst, presented at PAC 2003,
SRF 2003
The cavity can operate cw at gradients up to 12
MV/m, producing more than 4.5 MV of accelerating
potential
21
SC Spoke Resonator
ß0.5 and 0.64 triple-spokes (RIA)
  • RD at FNAL/ANL to study and optimize all three
    kinds of resonators

22
SC Spoke Resonator RD
  • Shape Optimization design Collaboration with ANL

23
SC Spoke Resonator RD
Total Deformation at 2 atm.
Total Deformation at 2 atm.
24
SC Spoke Resonator Cryomodules
b0.21 16 Cavities/Cryomodule 1 Cryomodule 16
focusing Solenoids/Cryomodule
b0.4 14 Cavities/Cryomodule 2 Cryomodules 7
focusing Solenoids/Cryomodule
Open Technical Choice
b0.61 6 Cavities/Cryomodule 7 Cryomodules 6
focusing quads/Cryomodule
25
Technical Solutions
Positive Ion Injector Cryomodule
  • Separate Vacuum
  • Efficient, top loading
  • Good alignment capability

26
ANL/RIA Cryomodule Design
Clean Assembly suspended from Top Plate
Clean Room String Assembly
Assembly lowered in vacuum vessel
27
Technical Solutions
  • FNAL idea for Spoke Cavities Cryostat

28
ANL-FNAL Test Cryostat
  • Common approach for PD/RIA test cryostat

29
Elliptical b (0.47, 0.61) 0.81
  • Cryostat based on TESLA design
  • 8 cavities, operating at 2K
  • Focusing cold quads
  • 9 quads in b0.47 (40 T/m)
  • 5 quads in b0.61 (33 T/m)
  • 3 quads in b0.81 (5 T/m)
  • 1 quad in b1 (3 T/m)
  • Expected Heat Loads
  • 5 W in 2 K
  • 20 W in 4.5 K
  • 200 W in 50 K

30
Elliptical b (0.47, 0.61) 0.81
b0.47 8 Cavities, 6 cells/cavity 9 focusing quads
Open Technical Choice
b0.61 8 Cavities, 6 cells/cavity 5 focusing quads
b0.81 8 Cavities, 8 cells/cavity 3 focusing quads
b1.0 8 Cavities, 9 cells/cavity 1 focusing quad
31
Elliptical b (0.47, 0.61) 0.81
  • Build on FNAL/SNS/JLAB/MSU experience and
    collaboration to develop blt1 cavities.

32
CONCLUSIONS
  • blt1 RD activities started
  • Focus on
  • Ion source (H) in SMTF by June
  • Addressed design/development of SS cavities at
    325 MHz
  • Converge on procurement of first Spoke Cavities
    by FNAL
  • Starting RFQ prototyping and development
  • To do
  • Warm Temperature Spoke Resonators
  • Focusing Magnets (Solenoids and Quadrupoles)
  • Well defined plan to address key issues for PD
    RD.
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