The TESLA Dogbone Damping Ring

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Transcription:

The TESLA Dogbone Damping Ring Winfried Decking for the TESLA Collaboration April 6 th 2004

Outline The Dogbone Issues: Kicker Design Dynamic Aperture Emittance Dilution due to Stray-Fields Collective Effects Space Charge Impedance Ion effects Electron Cloud

The TESLA Bunch Train SC Technology: long RF pulses and thus long bunch trains low frequencies and thus small wake-fields Benefits: High power transfer efficiency Straight forward intra-train feedback Relaxed LINAC tolerances Requires a damping ring (system) which is capable of damping the approximately 1 ms long bunch train at once.

The TESLA Bunch Train TESLA bunch train 2820 337 ns = 950 µs 285 km long Extract every bunch separately, bunch spacing given by shortest kicker rise/fall time 20 ns 2820 56 µs 17 km long Save tunnel cost: DR in main linac tunnel and short return arcs dogbone

Dogbone Design Arc lattice defines momentum compaction (bunch length), chromaticity correction, small emittance Wiggler section to provide damping Long straight as simple transport line Very flexible design: more wigglers, collimation, length chicane, Large energy (5 GeV) to mitigate space charge effects No Intra-beam scattering Touschek-lifetime 30 min

Kicker R&D (1) Kicker specifications 0.05% amplitude stability 3MHz pulses, 5Hz repetition 40 ns 337 ns Kicker pulse 0.6 mrad ±0.05% 0.01 Tm Residual: 0.5% Damping ring bunches Kicker technology available Strip-line Ferrite loaded C-yoke Pulser development based on commercial available MOSFET switches (Behlke)

Kicker R&D (2) Kicker system measurements with beam at TTF 1 measurement of kicker strength with BPM scan of the kicker pulse width with a timing step of 0.5 ns 30 pulses for each data point Measured amplitude jitter (1 Kicker) : 1.2% 30 Kicker : 0.2 % Pulser results 79 µm 105 µm 5.8 mm Full power test with two switches and 1000 pulses at 1 µs spacing each. 337 ns 40 ns I max = 100 A Residual: 2.75 % 100 pulse average

Kicker R&D (3) System Kicker Next Steps Specification Measured Pulse length 40 ns 30 ns Rise time (10%- 90%) 8 ns 4.9ns Micro pulse 3 MHz 2 MHz 3 switches parallel Macro pulse 5 Hz 5 Hz Amplitude stability (1/10 σ x ) 0.05 % 1.2 % (0.2% for 30 kickers) No effort so far Apply clipping techniques Apply 180deg kicker Residual kick 0.5 % 2.75% Beam based correction Fast kicker prototype successfully tested

Dynamic Aperture Incoming positron beam emittance requires large acceptance Possibility to over produce e + and collimate Dynamic aperture limited by wiggler insert Optimize wiggler parameters Optimisation of wiggler field shape has never been done Increase of wiggler period length (>40cm) possible Optimize lattice design Smaller beta-functions Insert non-linear elements (octupoles) Rings with lots of wiggler damping are operating (CESR) or will come into operation (PETRA III, 2008)

190 cm 125 cm 275 cm 30 cm Time Varying Stray Fields (1) 520 cm 445 cm 80 cm 300 cm T car 1 151 cm Klystron & Pulse Transformer 310 cm Damping Ring 90 cm 125 cm 0.5 ms DR Ejection Magnetic Field Probe Magnetic fields arising from LINAC pulse cause orbit/dispersion perturbation at ejection Measurement of magnetic field at TTF 1µTm => 4 µm quad misalignment Ground motion power density spectrum 10 3

Time Varying Stray Fields (2) Simulation of ejection process Orbit correction at Ejection Point No correction Orbit & Dispersion correction at EP Worst case scenario: average factor 2.5 in ε y <30% lumi loss

Time Varying Stray Fields (3) Cures: Shielding (magnetic shielding difficult but eddy current shielding possible (2cm Cu/Al)) Repetitive component (most?) can be compensated by fast kicker scheme (2 fast dispersive bumps in/at extraction) Second tunnel solution for DR (adds roughly ~150 MEuro)

Space Charge Tune Shift (1) Longitudinal position within bunch: Synchrotron oscillations z = cos( 2π # ν ) Circumference: large Q γ 2 CN ε e x ε y z o z 2 e σ σ z 2 Energy: small Emittance: small z 2 turns z Nominal tune Tune spread with fully damped beam Direct space charge force large because C/γ 2 is unusual large Synchroton oscillations vary the particle position within the bunch, leading to incoherent tune spread, increasing while the beam is damped Particle amplitude growth when crossing resonances

Space Charge Tune Shift (2) Proton synchrotrons operate with incoherent tune spread around 0.5 Experience from PETRA II proton synchrotron: Proton beam energy 7 GeV Incoherent tune spread 0.1 Lifetime about 5 10 minutes A tune spread below 0.1 prevents amplitude increase Decrease the space charge tune shift: Increase ε y by factor 4 (always works) This is worst case scenario, leads to 40 % lumi loss Increase energy (difficult arc lattice, more RF,.) Decrease ring length (kicker, e-cloud, ions) Increase beam size locally

Space Charge Local Coupling 1. Skew quadrupole triplet 2. Straight section (Linear Optics) Inverse skew quadrupole triplet 3. Inverse skew quadrupole triplet Simple, tunable linear optics ν x - ν y < 0.02 gives 10% emittance increase Solenoid compensation in colliders more advanced, nevertheless betatron coupling ratios of well bellow 0.5% reached (DAφNE, LEP, ) Orbit/Dispersion correction requires 4 4 algorithm Red: No local coupling Blue: Local coupling

Space Charge - Tracking Results Application of coupling bump keeps space charge tune shift below 0.1 No amplitude increase observed in tracking Nominal tune With coupling bump No coupling bump Particle tune versus initial longitudinal amplitude

Collective Effects-Single Bunch longitudinal microwave instability factor 5 below threshold from tracking bunch lengthening not observed in tracking simulations Bunch length Design current Energy Spread Design current Z / n is the effective impedance (machine impedance averaged with bunch spectrum) per unit length transverse mode-coupling threshold 96,000 KΩ, Z 4,000 KΩ

Ion Effects TDR design pressure of 10-9 mbar Ion Trapping: Train gap of 600 ns needed to clear ions Tune Shift: In straight accumulated ions produce a tune shift of 0.28 at end of bunch train. Fast Ion Instability: Calculated growth time of the order of 100 µs (for all DR). More studies needed. Cures: Vacuum pressure of 10-10 mbar in straight, 10-9 mbar in arc More pumps, ante-chamber in arc Cost increase Intra-train clearing gaps Ion effects can be mitigated by proper vacuum system design

Electron Cloud E-cloud is a world-wide observed and studied effect (next ICFA workshop April, part of EuroTeV proposal), with controversy results Issue for all DR, large TESLA Dogbone bunch-spacing helps preventing the e-cloud build-up Machines which suffered from e-clouds found ways to mitigate the effect E-cloud effects studied in collaboration with CERN Build up of the electron cloud occurs depending on Vacuum chamber layout (geometry, ante-chamber, ) Vacuum chamber material (Secondary emission yield)

Electron Cloud Build Up Electron Cloud Build Up in Arc Electron Cloud in Straight Al chamber Wiggler Section Al chamber Neutralization Cu platted Line Density Al chamber Cu platted Ante-chamber Ante-chamber design in the TDR Trapping of electrons in some sections of the wiggler observed in some simulations

Electron-Cloud Induced Instabilities Effective wake leading to strong head-tail instability calculated assuming various e-cloud densities Arc Straight Wiggler TEASLA DR Length / m 1900 14560 540 17000 Scenario 1: neutralization density everywhere cloud charge density / 10 12 m -3 2.7 0.4 5.8 0.85 effective wake field / threshold wake 0.577 0.59 0.359 1.526 Scenario 2: neutralization density in wiggler cloud charge density / 10 12 m -3 0.75 0.01 5.8 0.28 effective wake field / threshold wake 0.161 0.014 0.359 0.521 50 % above threshold 100 % bellow threshold Single bunch head-tail instability threshold not reached even with neutralization in wiggler Multi-bunch growth rate within damping capabilities of MBFB system E-cloud effects in the TESLA e + DR can be mitigated by proper design of the vacuum system

ILCTRC Ranking 2 All DR Simulation studies and experiments to understand the magnitude of electron cloud effects Worldwide effort going on (ICFA, EuroTeV, ) Further simulations and experiments of the fast ion instability To be performed Damping ring extraction kicker stability (at level of <10-3) requires continued studies including experiments Prototype build, test at TTF or PETRA possible Additional simulations of emittance correction in the damping rings are needed as well as experiments in existing machines Continuing effort, experiments at light sources, ATF, PETRA and HERA possible

ILCTRC Ranking 2 TESLA Specific Development of a damping ring kicker with very fast rise and fall times Prototype build and successfully tested Further dynamic aperture optimization of the ring Optimization of wiggler etc. to be performed ( This issue requires an aggressive effort to optimize the TESLA DR wiggler and/or lattice design. Such an effort is expected to produce a satisfactory solution, ILCTRC) Energy and luminosity upgrade to 800 GeV puts tighter requirements on DR alignment tolerances, and on suppression of electron and ion instabilities. Further studies are required. 800 GeV parameter set to be adjusted

Summary TESLA Dogbone is a cost-effective solution for the TESLA damping ring Mature design including industrial studies for many components Based on world-wide experience with storage rings Unique features attract attention of many accelerator physicists world-wide ILCTRC has not identified any showstoppers