stephen brooks / ral / may 2004 optimisation of the ral muon front end design

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Stephen Brooks / RAL / May 2004 Optimisation of the RAL Muon Front End Design

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Page 1: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Optimisation of the RAL Muon Front End Design

Page 2: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Contents

• Designs considered– Decay channel with chicane– Decay channel with phase rotation, cooling

• Tracking code

• Optimisation approach

• Results

• Future work– …and issues still to be solved

Page 3: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Design Components

• Pion to muon decay channel– Accepts pions from the target– Uses a series of wide-bore solenoids

• “Phase rotation” systems– FFAG-style dipole bending chicane (2001)

• For short bunch length 400MeV muon linac

– 31.4 MHz RF phase rotation (2003)• For low energy spread ionisation cooling ring

Page 4: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Pion to Muon Decay Channel

• Challenge: high emittance of target pions– Currently come from a 20cm tantalum rod

Page 5: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Pion to Muon Decay Channel

• Challenge: high emittance of target pions– Currently come from a 20cm tantalum rod

Evolution of pions from 2.2GeV proton beam on tantalum rod target

Page 6: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Pion to Muon Decay Channel

• Challenge: high emittance of target pions– Currently come from a 20cm tantalum rod

• Solution: superconducting solenoids– S/C enables a high focussing field– Larger aperture than quadrupoles

• Basic lattice uses regular ~4T focussing– Initial smaller 20T solenoid around target– 30m length = 2.5 pion decay times at 200MeV

Page 7: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Chicane Phase-Rotation

(or rods)

RAL design 2001-02 by Grahame Rees

(…or liquid mercury jet, rotating levitating band, granular water-cooled target, etc…)

4MV/m

Page 8: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

RF Phase-Rotation

• 31.4MHz RF at 1.6MV/m (2003 design)– Reduces the energy spread 180±75MeV to ±23MeV– Cavities within solenoidal focussing structure– Feeds into cooling ring

Page 9: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Muon1 Particle Tracking Code

• Non-linearised 3-dimensional simulation– PARMILA was being used before

• Uses realistic initial + distribution– Monté-Carlo simulation by Paul Drumm

• Particle decays with momentum kicks

• Solenoid end-fields included

• OPERA-3d field maps used for FFAG-like magnets in chicane (Mike Harold)

Page 10: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Muon1 Tracking Code Details

• Typically use 20k-50k particles

• Tracking is done by 4th order classical Runge-Kutta on the 6D phase space– Currently timestep is fixed at 0.01ns

• Solenoids fields and end-fields are a 3rd order power expansion

• Field maps trilinearly interpolated

• Particle decays are stochastic, sampled

Page 11: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Optimiser Architecture

• How do you optimise in a very high-dimensional space?– Hard to calculate derivatives due to stochastic

noise and sheer number of dimensions– Can use a genetic algorithm

• Begins with random designs• Improves with mutation, interpolation, crossover…

– Has been highly successful so far in problems with up to 137 parameters

Page 12: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Decay Channel Parameters

Drifts Length (m)

D1 0.5718 [0.5,1]

D2+ 0.5 [0.5,1]

Solenoids Field (T) Radius (m) Length (m)

S120

[0,20]0.1 [fixed]

0.4066 [0.2,0.45]

S2-4−3.3, 4, −3.3

[-5,5]0.3

[0.1,0.4]0.4

[0.2,0.6]

S5-S24±3.3 (alternating)

[-4,4]

S25+0.15 [0.1,0.4]

Final (S34) 0.15 [fixed]• 12 parameters– Solenoids alternated in field strength

and narrowed according to a pattern

• 137 parameters– Varied everything individually

Tantalum Rod

Length (m) 0.2 [fixed]

Radius (m) 0.01 [fixed]

Angle (radians) 0.1 [0,0.5]

Z displacement (m) from S1 start

0.2033 (S1 centred) [0,0.45]

Original parameters / Optimisation ranges

Page 13: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Phase Rotation Plan

• Chicane is a fixed field map, not varied

• Solenoid channels varied as before– Both sides of chicane– Length up to 0.9m now

• RF voltages 0-4MV/m• Any RF phases• ~580 parameters

• RF phase rotation• Similar solenoids,

phases (no field map)• RF voltages up to

1.6MV/m• ~270 parameters

Page 14: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Results- Improved Transmission• Decay channel:

– Original design: 3.1% + out per + from rod– 12-parameter optimisation 6.5% +/+

• 1.88% through chicane

– 137 parameters 9.7% +/+

• 2.24% through chicane

• Re-optimised for chicane transmission:– Original design got 1.13%– 12 parameters 1.93%– 137 parameters 2.41%

3`900`000 runs so far

1`900`000 runs

330`000 runs

Page 15: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

NuFact Intensity Goals

• “Success” is 1021 /yr in the storage ring

Proton Energy/GeV Intensity/MW Target eff (pi/p) MuEnd eff (mu/pi) Operational mu/year in storage ring Current/uA

8 4 20% 1.0% 30% 5.90497E+19 500 "Not great" scenario

8 1 60% 2.0% 35% 1.03337E+20 125 ISIS MW only to reach 10^20

8 5 60% 3.5% 40% 1.03337E+21 625 "Quite good" 5MW scenario (gets 10^21)

8 5 1.75 8.5% 55% 1.00646E+22 625 Required to reach 10^22

1.75 = PtO2 target inclined at 200mrad, see Mokhov FNAL PiTargets paper 20% = 2.2GeV dataset from Paul Drumm

Page 16: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Distributed Computing System

• How do you run 3`900`000 simulations?• Distributed computing

– Internet-based / FTP– ~450GHz of processing power– ~130 users active, 75`000 results sent in last week– Periodically exchange sample results file – Can test millions of designs

• Accelerator design-range specification language– Includes “C” interpreter– Examples: SolenoidsTo15cm, ChicaneLinacA

Page 17: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Page 18: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Optimised Design for the Decay Channel (137 parameters)

0

5

10

15

20

25

Fie

ld (

Te

sla

)

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

Siz

e (

me

tre

s)

Solenoid Field Solenoid Radius Solenoid Length Drift Length

•Maximum Length

•Minimum Drift

•Maximum Aperture

•Maximum Field

(not before S6)

(mostly)

(except near ends)

(except S4, S6)

Page 19: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Why did it make all the solenoid fields have the same sign?

• Original design had alternating (FODO) solenoids• Optimiser independently chose a FOFO lattice• Has to do with the stability of off-energy particles

FODO lattice

FOFO lattice

Page 20: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Design Optimised for Transmission Through Chicane

• Nontrivial optimum found

• Preferred length?

• Narrowing can only be due to nonlinear end-fields

0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

Length

Radius

0.463 m

0.402−0.003n m

Page 21: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Future Optimisations

• Chicane and RF phase rotation designs are starting to be run now– Initial results promising

• Cooling ring later this year

Page 22: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

RAL Design for Cooling Ring

• 10-20 turns

• Uses H2(l) or graphite absorbers

• Cooling in all 3 planes

• 16% emittance loss per turn (probably)

Page 23: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Stephen Brooks / RAL / May 2004

Unresolved Issues (to-do)

• Solenoid field clipping distance

• Need ‘solid’ solenoids for best accuracy– ICOOL has recently added these

• New target dataset needed for 8GeV– Trying to get MARS– Possibility of target energy optimisation

• Code could do with variable timesteps and/or error control

Page 24: Stephen Brooks / RAL / May 2004  Optimisation of the RAL Muon Front End Design

Target Area Losses

• Muon1 modified to count lost particle energies

• For a 4MW p+ beam:– 35kW deposited in S1 (r=10cm)– Large >1kW amounts deposited up to S5

• Added “collimators” to the simulation– Decreases losses to 10’s of watts in all but S1

and S2– S1 needs enlarging to accommodate an entire

Larmor rotation

• Consistent target-area layout is needed

Microsoft Excel Worksheet