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Summary of SPARC first-phase operations
Daniele Filippetto on behalf of SPARC team
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Outlines Layout (12/06) Laser and cathode Synhcronization
Diagnostic and system commissioning Best results Conclusions
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RF: Waveguide and gun conditioning successful
Conditioning time~2 weeks Eacc~120MV/m Ekin=5.6MeV (e-)
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High complexity system!!
Laser: High complexity system!! oscillator pumps amplifiers Harmonics generator UV stretcher Pulse shaper Daily optimization is required
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Sparc hall: Faraday cup ICT Beam dump Spectrometer Magnets E-meter
cross
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Operation days: RF and timing systems; RF conditioning Beam operation
Flat pulse Beam operation Gauss pulse Installation & characterization LC mask Transfer Line install. New stretcher Normal incidence Diagnostics development Flat top studies
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Layout Laser and cathode operations Synhcronization systems Diagnostic overview and system commissioning Best results Conclusions
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Longitudinal pulse shaping: two stages
Minimum rise time of 3 ps with the dazzler only How to increase the Steepness: simulations
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Two stages pulse shaping:results
With the DAZZLER and the UV stretcher allow to easily change the pulse length and the time shape During the run it was achieved rise time down to ps 15 ps pulse Gaussian pulse 10 ps pulse 6 ps pulse
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Transfer line and imaging:
Circular beam at cathode (>98%) Front tilt compensation (< 200 fs) Work for different spot sizes. High energy losses: 65% Sensitive to lens position (±1 mm) Difficult to be measured Poor transverse uniformity A grating parallel to the cathode was employed to diffract the beam at 72°. A lens was used to compensate the chromatism at the image plane. 72° incidence 90° incidence Better uniformity and lower losses A mirror in vacuum is required
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New laser diagnostic: FESCA 200
Sub-ps resolution streak camera has been recently installed at LNF The measured resolution is about 200 fs in the IR and 500 In the UV Flat top UV measurements A short IR pulse was used as reference in jitter corrected multiple image-acquisistion IR beam UV pulse
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1nC electron bunch with 50 μJ laser energy (~6*10^13 photons @ 266nm)
Quantum efficiency optimization: Laser cleaning with 10 μJ and 100 μm spot size diameter. Mean QE increased from ^-5 to 10^-4 Improved uniformity over a 4 mm square region 1nC electron bunch with 50 μJ laser energy (~6*10^13 266nm)
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Layout Laser and cathode operations Synhcronization systems Diagnostic overview and system commissioning Best results Conclusions
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Time jitter maximum acceptable values: - SPARC phase I (achieved):
Synchronization: Time jitter maximum acceptable values: - SPARC phase I (achieved): ± 2ps between the Laser pulse and the Linac RF (RF gun mainly) - SPARC phase II (on the way): ± 0.5ps between the Laser pulse and the Linac RF (RF gun and RF compressor mainly) - and next-generation experiments (under study): ± 0.1ps control of the bunch longitudinal position Synchronization strategy Laser to RF synchronization: 1-5kHz bandwith piezo-electro-optical feedback (Synchrolock) Standard laser IR oscillator time jitter measurement Innovative UV pulse single shot time arrival measurement RF to RF synchronization: Feedback loops Signal demodulation to monitor the phase of the fields in the RF structures along the machine
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RF to RF synchronization
Slow feedback (BW<<1Hz): Correction of the temperature drifts in the waveguides Motorized phase shifters 0.25ps RMS time jitter measured in the gun (with fast feedback off) Fast feedback (BW~1MHz): Correction performed inside a single 4µs klystron pulse Electronic phase shifters 230fs open loop time jitter 23fs closed loop time jitter
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Laser to RF synchronization
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10Hz final amplified pulse measurement (best result is 400fs)
Agilent SSA (absolute) measurements SPARC monitor system (relative to RF) 350fs RMS 10Hz final amplified pulse measurement (best result is 400fs) New cavity filter used to reject the noise coming from high power RF structures 79.3MHz oscillator measurement (very good agreement with SSA)
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Layout Laser and cathode operations Synhcronization systems Diagnostic overview and system commissioning Best results Conclusions
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Diagnostic overview 60 cm: faraday cup to measure the charge at gun exit, and Cromox screen to see and center the beam; cm: E-meter (slits cross, Yag and CCD cross); Emittance, beam envelope, beam parameters as function of trnsv. coordinates; 270 cm :aerogel + streak camera; beam length; cm :FODO; 370 cm : dipole; 400 cm : spectrometer cross (Yag+ CCD) ; E & ΔE meas. 440 cm : ICT (beam charge) Image of streaked light from Aerogel (UCLA collaboration) T=12 ps } prepare the beam to E & ΔE meas.
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Envelope automatic measure
The emittance-meter moves and stops in several (15-30) positions. Several images are collected at each point, and an algorithm calculates the RMS parameters and the error bars.
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Emittance automatic measure
an automated emittance scan has been developed, making use of the centroids and rms calculated from envelope scan. 30 images each slit position 13 slit positions each z position (sampling the beam with σ/2 step width) 30 z positions 11700 images & ~450 motor movements each ε evolution measurement The high measurement resolution allows to precisely reconstruct not only the second moment but the entire transverse trace space distribution (x-x’ or y-y’)
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Data analysis It has been the first time of direct emittance evolution measurements and experimental study of dynamical behaviour Problems: Need to know exactly the percent of charge used to calculate di emitt. (haloes estimation) Same cut for emitt. meas. at different positions High sensitivity needed to measure small fluctuations As result of collaboration between experimental & BD groups 3 independent alghoritms were developed for emittance calculations: Alg. based on single image analysis and data extrapolation; Alg. Based on trace space plot filtering; Genetic alg. fitting 8 different ellispes with same centers, maximizing the (Intensity/Area) function; All the procedures have been compared with the simulations, and they showed a Very good agreement
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Examples of measurements:
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Layout Laser and cathode operations Synhcronization systems Diagnostic overview and system commissioning Best results Conclusions
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T= 5.6 MeV, I= 92 A, n = 1.6 m ==> B= 7x1013 A/m2
charge 0.83 nC pulse length (FWHM) 8.9 ps rise time 2.6 ps rms spot size 0.36 mm RF phase (-max) -8°
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phase space - simulation and measurements
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Flat-top Vs Gaussian pulse shape
charge 0.74 nC pulse length (FWHM) 8.7 ps rise time 2.6 ps rms spot size 0.31 mm RF phase (-max) -8°
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The double minimum experimental evidence
charge 0.5 nC pulse length (FWHM) 5 ps rise time 1.5 ps rms spot size 0.45 mm RF phase (-max) +12° Emittance scan as function of B in a fixed point Isol=198 A
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Energy spread evolution along the drift
Demonstr. of negligible WF effect due to the bellows Isolation of longitudinal space charge eff. Study of longitudinal dynamics for different charges, RF phases and pulse lengths
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Conclusions Commissioning of the system Flat top generation with UV pulses Nominal beam parameters Good agreement with simulations Phase space evolution Energy spread evolution Flat top Vs Gaussian Emittance oscillation
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