RCS design RCS design Valeri Lebedev AAC Meeting November 16-17, - - PowerPoint PPT Presentation

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RCS design RCS design Valeri Lebedev AAC Meeting November 16-17, - - PowerPoint PPT Presentation

RCS design RCS design Valeri Lebedev AAC Meeting November 16-17, 2009 Outline Outline Objectives for RCS design Logic behind parameter choices Technical description AAC, November 16-17, 2009 Valeri Lebedev 2 Objectives &


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SLIDE 1

RCS design RCS design

Valeri Lebedev AAC Meeting November 16-17, 2009

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SLIDE 2

Outline Outline

  • Objectives for RCS design
  • Logic behind parameter choices
  • Technical description

AAC, November 16-17, 2009 – Valeri Lebedev 2

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SLIDE 3

Objectives & Challenges Objectives & Challenges

  • Objectives

– Beam acceleration from 2 to 8 GeV – Support

  • 2 MW in MI at 60 to 120 GeV (140 – 280 kW)
  • 8 GeV program with fast extracted beam (≥100 kW)

– Look for a solution being less expensive than pulsed SC linac – Look into possible future upgrades p pg

  • Challenges

– Beam current is ~5 times of Booster  Space charge, instabilities, RF, ep

  • Booster problems to be avoided

Booster problems to be avoided

– No transition crossing – No laminations seen by beam  smaller Z||, Z – Zero Disp in cavities  No SB resonance Zero Disp. in cavities  No SB resonance

AAC, November 16-17, 2009 – Valeri Lebedev Page 3

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SLIDE 4

RCS Design Choices RCS Design Choices

  • Circumference, C = CMI/6

6 i j ti t fill MI Energy, min/max, GeV

2/8

– 6 injections to fill MI

  • High periodicity FODO
  • Racetrack

– Two long straights Energy, m n/max, GeV

2/8

Repetition rate, Hz

10

Circumference, m (MI/6)

553.2

Tunes

18.43

T siti G V

13 36

g g – Dispersion zeroing with missed dipole

  • Acceptance matches MI acceptance

– 10% allowance for  growth Transition energy, GeV

13.36

Beam current at injection, A

2.2

Harmonic number

98

  • Max. RF voltage, (V98/V196) MV

1.6/0.7

10% allowance for  growth

  • 2 harmonics RF system

– Space charge mitigation – Beam stability

  • Hi h i j

ti h l ith

g (

98 196)

95% n. emittance, mm mrad

22

Space charge tune shift, inj.

0.07†

  • Norm. acceptance, mm mrad

40

Injection time for 1 mA ms

4 3

  • High injection energy helps with

Space Charge and Instabilities

– Small size of vacuum chamber † KV-like distribution, BF=2.2 Injection time for 1 mA, ms

4.3

Linac energy cor. at inject.

1.2%

RF bucket size, eV s

0.38

AAC, November 16-17, 2009 – Valeri Lebedev Page 4

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SLIDE 5

Optics Optics

  • -functions are blown-up in injection region – reduction of foil heating

– 6 half cells are used for injection region

  • Two types of quadrupoles with the same integral strength

– Large aperture quads for injection & extraction g p q j

Thu Sep 17 14:51:49 2009 OptiM - MAIN: - C:\VAL\Optics\MuonCollider\Synchrotron\RCS_withFoil_Inj.opt 40 1 BETA_X&Y[m] DISP_X&Y[m] 276.616 BETA_X BETA_Y DISP_X DISP_Y

AAC, November 16-17, 2009 – Valeri Lebedev Page 5

Twiss parameters for the first half of the ring

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SLIDE 6

Optics (continue) Optics (continue)

  • Straight line assignments

I j ti t ti i – Injection, extraction, scraping – RF

  • Vacuum chamber radius, a = 21.3 mm (internal)

7 mm allowance for orbit correction – 7 mm allowance for orbit correction

Thu Sep 17 14:55:45 2009 OptiM - MAIN: - C:\VAL\Optics\MuonCollider\Synchrotron\RCS_withFoil_Inj.opt 2.5 2.5 Size_X[cm] Size_Y[cm] 276.616 Ax_bet Ay_bet Ax_disp Ay_disp

AAC, November 16-17, 2009 – Valeri Lebedev Page 6

Beam envelopes; acceptance - n=40 mm mrad, Ek = 2 GeV, p/p = 5 x 10-3.

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SLIDE 7

Vacuum Chamber Vacuum Chamber

  • Competing effects are

– Shielding and distortion of dipole bending field by eddy currents excited in the vacuum chamber – Vacuum chamber stability under atmospheric pressure – Vacuum chamber heating by eddy currents Vacuum chamber heating by eddy currents – Transverse impedance due to wall resistivity – Ring acceptance

  • The compromise resulted in

– Round stainless steel vacuum chamber with radius of a=22 mm and wall thickness of d = 0.7 mm – Inside quads of injection and extraction regions: a=43 mm d = 1 mm – No limitations on the chamber thickness outside dipoles and quads No limitations on the chamber thickness outside dipoles and quads

  • Ring acceptances and beam emittance:

– 85 mm mrad - limited by vacuum chamber size – 40 mm mrad – limited by scrapers – 22 mm mrad – 95% norm. beam emittance

AAC, November 16-17, 2009 – Valeri Lebedev Page 7

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SLIDE 8

Limitations on Vacuum Ch b D i Chamber Design

  • Shielding and distortion of the dipole bending field by eddy currents

excited in the vacuum chamber

– Dipoles: |B/B|max=8.5 x 10-4 @16 ms – Quads – approximately half of the dipole effect

c ad a y iB y B

AC y

                 , ... 240 12 1 ) , (

2 2 2 4 2

– Delayed quad wave form by ~70 s

  • Vacuum chamber stability under atmospheric pressure

– Compression: 3.1 N/mm2

a c

ramp

    2

a P

p – Bend for a/a=0.02: 8.9 N/mm2 – Yield stress : 200 N/mm2

  • Vacuum chamber heating by eddy currents (~a3)

2

4 9         d a a a P

atm bend

d P

atm cmpr 

Vacuum chamber heating by eddy currents ( a )

– dP/dz=10 W/m – T=15 K for convective air cooling with heat transfer of 10-3 W/cm2/K

2 2 2 3 AC ramp B

c da dz dP   

AAC, November 16-17, 2009 – Valeri Lebedev Page 8

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SLIDE 9

Vacuum Chamber I d Impedance

  • Transverse impedance due to wall resistivity (~a-3)

) (

3 2 2

c Z Z 

– Z and dP/dz are related inversely proportional

  • No dependence on vacuum

chamber parameters

2 2

4 ) (

AC ramp B

Z dz dP Z     

    2 4 ) (

3 2

c d ad d a   

 10 Qf0

Ztr [O/cm2] Laminated dipole

 2

0 1 1

Solid dipole

1 103  1 104  1 105  1 106  1 107  1 108  1 109  0.01 0.1

Stainless steel

AAC, November 16-17, 2009 – Valeri Lebedev Page 9

1 10  1 10  1 10  1 10  1 10  1 10  1 10 

f [Hz]

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SLIDE 10

Dipoles Dipoles

  • Small aperture

Parameter Unit Value Number of magnets 100

 Compact dipole

  • Sagitta – 1.7 cm

g Peak field T 0.87375 Field at injection T 0.2184 Magnet gap mm 44 Good field area diameter mm 40 Field homogeneity 0.02 % Effective length m 2.13216 Peak current A 667 A Number of turns/pole 24 Copper conductor mm x mm 12.5 x 12.5 Conductor cooling hole diameter mm 7 N b f k il / l 2 Number of pancake coils/pole 2 Lamination material M17 Lamination thickness mm 0.35 Inductance mH 25 DC resistance Ohm 0.021 Stored energy kJ 5 47 Stored energy kJ 5.47

  • Av. Power losses (no eddy current)

kW 4.3 Peak inductive voltage V 390 Number of cooling circuits/magnet 1 Water pressure drop MPa 0.5 Water flow l/min 2.8 AAC, November 16-17, 2009 – Valeri Lebedev Page 10 Water temperature rise Cº 22

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SLIDE 11

Quadrupoles Quadrupoles

Parameter Unit Normal quad Large quad Number of magnets 122 8

  • Large and small quads

have the same field

Number of magnets 122 8 Peak field gradient T/m 17.65 14.65 Field gradient at injection T/m 5.528 4.589 Pole tip radius mm 25 45 Good field area diameter mm 40 75 Field nonlinearity (2D) 0.03 % 0.03 %

have the same field integral

  • Large quads

– 4 in injection region

Effective length M 0.69 0.794 Peak current A 672 A Number of turns/pole 7 19 Copper conductor mm x mm 10 x 10 10 x 10 Conductor cooling hole diameter mm 5 5 N b f il / l 1 1

– 4 in extraction region

Number of coils/pole 1 1 Lamination material M17 M17 Lamination thickness mm 0.35 0.35 Inductance mH 1.15 3.12 DC resistance m 12 40 Stored energy J 260 700 Stored energy J 260 700

  • Av. power losses (no eddy currents))

kW 2.0 6.7 Peak voltage V 40 110 Number of cooling circuits/magnet 1 4 Water pressure drop Mpa 0.5 0.5 Water flow l/min 1.9 1.6

AAC, November 16-17, 2009 – Valeri Lebedev Page 11

Water temperature rise Cº 16 11

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SLIDE 12

Resonance Driving of Di l d Q d Dipoles and Quads

  • Dipoles and quads of each cell have a resonance

circuit compensating their inductive impedance

– 50 standard + 2 special cells (one for each straight line)

  • each is tuned to 10 Hz

– Total power ~1.5 MW – Maximum voltage to ground 600 V

  • Similar to the Booster

AAC, November 16-17, 2009 – Valeri Lebedev Page 12

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SLIDE 13

Beam Acceleration Beam Acceleration

AAC, November 16-17, 2009 – Valeri Lebedev Page 13

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SLIDE 14

RF System RF System

  • Dual Harmonic RF system,

– At injection V2=0.5 V1

  • 10 Bunches extraction gap

– Set by required length of MI extraction gap

  • Beam loading is serious issue
  • Beam loading is serious issue

– 1.6 MV beam induced voltage (at resonance)

  • Longitudinal emittance is blown up to ~0.6 eV s to match to MI RF bucket

– Can be excited by quadrupole damper (same as in Booster) Can be excited by quadrupole damper (same as in Booster)

1-st harmonic 2-nd harmonic Harmonic number 98 196 Maximum voltage, MV 1.6 0.7 Minimum voltage, kV 20 10 Frequency sweep, MHz 50.33-52.81 100.66 – 105.62 Number of cavities 16 10 Sh t i d k 100 100

AAC, November 16-17, 2009 – Valeri Lebedev Page 14

Shunt impedance, k 100 100

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SLIDE 15

Injection-Extraction St i ht Straight

Cell N Assignment 132 TBD

  • Doublet focusing for injection

132 TBD 4 Injection 6 Primary collimators 7 Vertical and Horizontal collimators 8 TBD

  • Doublet focusing for injection

straight

  • It takes space of 6 FODO half cells
  • Increased aperture for 8 quads

9 Vertical and Horizontal collimators 10-11 Extraction kickers 12 TBD 13 Extraction septum

  • Increased aperture for 8 quads
  • 4 in injection
  • 4 in extraction

Thu Sep 24 13:53:25 2009 O ptiM

  • M

AIN:

  • C:\VAL\Opti

cs\M uonColli der\Synchrotron\RCS_with Foil_Inj.

  • pt

5 s _X & Y[ c m ] 66

  • 5

C

  • r

d in ate s X& Ax Y& Ay

AAC, November 16-17, 2009 – Valeri Lebedev Page 15

y

Q 132 Q 3 Q4 Q 5 Q 6 Q 7 Q 8 Q 9 Q 10 Q 11 Q12 Q13 Q14

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SLIDE 16

Injection Injection

  • Strip injection through 600 g/cm2 graphite foil
  • Small linac current (1 mA)
  • Small linac current (1 mA)

 2200 turn injection (11 for Booster, 1000 for SNS)

  • B2 – small field to avoid H- stripping (2 kG)
  • B3 – Large field to strip H- to H0 (-8.3 kG)
  • Stripped electrons carry

100 W beam power and have to be directed to the

  • Stripped electrons carry ~100 W beam power and have to be directed to the

electron dump

20 septum foil

x

[cm]

2 8 10

x [cm] B(z) [kG] x(z)

10

Injected H- p

6  4  2  4 6 8

[cm] [kG] x(z) B(z)

5 10 20  10 

H0 Survived H- B3 B2 B1

25  20  15  10  10  8  2

AAC, November 16-17, 2009 – Valeri Lebedev Page 16

5 10

s [m]

25 20 15 10

z [cm]

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SLIDE 17

Transverse Painting Transverse Painting

  • Transverse painting objectives

P i t K V lik di t ib ti – Paint K-V like distribution – Minimize number of secondary passages through foil

  • Major parameters

– Linac emittance – 0.5 mm mrad (rms, norm.) ( ) – RCS beam emittance – 22 mm mrad (95%, norm.) – Linac - and - functions are 0.345 of RCS ones

  • X-Y painting by CO displacement

– Closed 4 corrector bumps in each plane

50

Closed 4 corrector bumps in each plane

  • Independent control for X &  on foil

50 50

H

b c

50  50

a AAC, November 16-17, 2009 – Valeri Lebedev Page 17

50 

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SLIDE 18

Simulation Results for T P i ti Transverse Painting

  • Final distribution is close to the KV-distribution

800

fy(y) fx(x)

  • 50 secondary passages per particle

– 2.2 mm-2 per particle

  • 420 g/cm2 foil is tilted

b 45 d t i

200 400 600

by 45 deg. to increase cooling due to black body radiation

– Tmax = 1500 K

1  1 200

x, y [cm]

1

F(I)

max

– -electrons remove ~25% of heating

0.5

Iy Ix I4D

1 10 20 30 40 25 30 35 40 0.96 0.98 1

AAC, November 16-17, 2009 – Valeri Lebedev Page 18

I [mm mrad]

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SLIDE 19

Injection Loss Injection Loss

  • Total injection loss ~4%

– ~2% miss the foil – ~0.5% are not completely stripped in the foil – 0.15% are single scattered in the foil – ~1% are outside of 40 mm mrad RCS acceptance

  • In normal operating conditions it results in the heat load

– injection beam dump ~3 kW j p – collimation system ~1.5 kW

  • Prudent design (confirmed by SNS experience) would have both the

injection waste beam absorber and the collimation system designed injection waste beam absorber and the collimation system designed to handle 10% or 8.5 kW

AAC, November 16-17, 2009 – Valeri Lebedev Page 19

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SLIDE 20

Injection Dump Injection Dump

  • Injection dump is located in the tunnel
  • It requires considerable radiation shielding

AAC, November 16-17, 2009 – Valeri Lebedev Page 20

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SLIDE 21

Longitudinal Painting Longitudinal Painting

  • Longitudinal painting is

performed by momentum

  • ffset of linac beam

– p=5·10-4, – p/p=7·10-4, – Tinj=14.6 ns (73%)

  • Additionally, Linac has to

compensate the RCS energy variation during injection (4.3 ms)

– E/E =1.2%

 Bunching factor = 2.2

AAC, November 16-17, 2009 – Valeri Lebedev Page 21

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SLIDE 22

Extraction Extraction

  • Two kickers of 2.3 mrad each (±25kV, filling time 90 ns)
  • Quads displacements make vertical closed bump

– Q11 = -4.8 mm, Q12 = -6.39 mm, Q14 = 9.84 mm

AAC, November 16-17, 2009 – Valeri Lebedev Page 22

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SLIDE 23

RCS versus Pulsed Linac RCS versus Pulsed Linac

  • RCS

L i – Less expensive – Injection at smaller energy  Easier to manage injection loss – Limited upgrade potential U t 1 MW @15 H & 2 3 (MC) f ibl ith i d

  • Up to ~1 MW @15 Hz & 2-3 ns (MC) feasible with increased

acceptance

  • Linac

– Easier to upgrade

  • to 4 MW power proton driver for MC
  • + to ~20 GeV recirculator for neutrino factory

– Many injections per cycle if foil strip-injection is used (10 Hz)

  • Requires Recycler

q y  8 GeV final energy – An upgrade will require beam current increase: 1  ≥20 mA 2 GeV program discontinue or building another 2 GeV frontend!!!

AAC, November 16-17, 2009 – Valeri Lebedev Page 23

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SLIDE 24

Conclusions Conclusions

  • RCS looks as a good choice to accelerate from 2 to 8 GeV

– Less expensive than pulsed SC linac

  • ~287 M$ versus ~355 M$ (no escalations)
  • It has considerable upgrade potential but cannot meet 4 MW

pg p required by Muon Collider

  • Choice between RCS and Pulsed linac need to be done. It will be

driven by

– Cost & Upgradability

AAC, November 16-17, 2009 – Valeri Lebedev Page 24

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SLIDE 25

Backup Viewgraphs Viewgraphs

AAC, November 16-17, 2009 – Valeri Lebedev Page 25

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SLIDE 26

Vacuum Vacuum

  • Vacuum chamber

– 10-7 Torr or better (beam loss, ep instabolity)

  • No baking

– Secondary emission suppression (TiN or carbon film)

AAC, November 16-17, 2009 – Valeri Lebedev Page 26

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SLIDE 27

Optics and Orbit Correction Correction

  • Corrector pack near each quad: S and D coils

Di l t h d (h F D) – Dipole corrector near each quad (h – F, v – D)

  • 4 fast correctors in each plane for injection painting

– Two families of sextupoles

  • Partial chromaticity correction: from -25 to -(10 ÷ 15 )
  • No dynamic aperture limitation
  • Optics correction

– Additional coils in all quads for optics correction – F and D families (±0.25 tune correction ) (∫GdL=1.1 kG) F and D families (±0.25 tune correction ) (∫GdL 1.1 kG) + 36 separate optics correction quads (∫GdL=2.2 kG) – 12 Skew-quads (coupling & vertical dispersion)

Name Quantity L[cm] BH[G] BV[G] S[G/cm2] Name Quantity L[cm] BH[G] BV[G] S[G/cm ] Regular H 50 20 550

  • 200

Regular V 48 20

  • 550

200 Straight line H 12 20 550

  • Straight line V

14 20

  • 550
  • I j

i 4 30 1000 1000

AAC, November 16-17, 2009 – Valeri Lebedev Page 27

Injection 4 30 1000 1000

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SLIDE 28

Optics Cell Optics Cell

Name S[cm] L[cm] B[kG] G[kG/cm] S[kG/cm/cm] qF 65.9 65.9 1.7675 q

  • 2

85.9 20 sF 105.9 20 0.185

  • 1

135.9 30 bD 349.116 213.216 8.7375

  • 419.116

70 qD 485.016 65.9

  • 1.7634
  • 2

505.016 20 sD 525.016 20

  • 0.324
  • 1

555.016 30 bD 768.232 213.216 8.7375

  • 838.232

70

Mon May 18 16:48:54 2009 OptiM - MAIN: - C:\VAL\Optics\MuonCollider\Synchrotron\ACD_)Syn 30 5 Y[m] Y[m] 8 38232 BETA_X&Y DISP_X&Y BETA X BETA Y DISP X DISP Y

AAC, November 16-17, 2009 – Valeri Lebedev Page 28

8.38232 BETA_X BETA_Y DISP_X DISP_Y

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SLIDE 29

Collimation and I t t ti Instrumentation

  • Collimators

– Two stage – Located in the injection-extraction straight line

  • Positioning in the other line is also discussed

– Choice is determined by loss scenario

  • Instrumentation

– Standard set of FNAL instrumentation (BPMs, BLMs, … ) ( , , ) – Instrumentation for the injection region

  • Will be based on SNS experience

AAC, November 16-17, 2009 – Valeri Lebedev Page 29

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SLIDE 30

Stripping on Carbon Foil Stripping on Carbon Foil

AAC, November 16-17, 2009 – Valeri Lebedev Page 30