Transcript Slide 1
High power RF capabilities With two 50MW XL4 klystrons ASTA can produce: 100MW @ 1.5 μs --> 550MW @ 63 ns at X-band and feed two experimental outputs in the enclosure. Gate Valves Variable iris Variable Delay line length through variable mode converter From Two 50 MW Klystrons Two experimental stations inside the enclosure, one with compressed pulse and the other without the benefit of the pulse compressor. Courtesy of Valery Dolgashev components to support the experimental facilities Gate valve Tee for variable iris Bends for low loss transmission and reliable RF systems Dual moded delay lines with variable delay for a flexible pulse width Courtesy of Sami Tantawi llrf configuration Power meters Dark current signals DUT FE/RE Klystron RE Vacuum I&Q MIXER TWT K 4 port combiner SRS 60 Hz AFG SRS DG645 AFG I&Q MIXER TWT K no SLED SLED Pulse compression and pulse shaping Pulse compressor forward power Each bin of has independent I&Q modulation via two channel AFGs Forward power RF signals are I&Q demodulated and can be used in pulse shape feedback Delay line tuning is handled by feedback Breakdown rates vs gradient Breakdwn Probability [1/pulse/m] forward power reflected power faraday cup 1 faraday cup 2 Breakdown rate vs. pulse length for C10-VG07 0.1 260 ns 0.001 10 -5 10 -7 130 ns 50 100 Gradient [MV/m] Faraday cup signals register breakdowns and inhibit further pulses Gradient is calculated. Several weeks for typical structure characterization GS/s acquisition rates Breakdown traces are saved Automated processing 150 200 CERN CLIC PETS3 Testing 133 ns 266 ns Peak power Avg power Energy BD Drive beam Main beam Courtesy of Alessandro Cappelletti PETS Accelerating structures RF power Recirculation Implementation Revised: April 7, 2010 Jake Haimson Some ongoing and planned HG studies BreakdownProbability 1 pulsemeter Test of a Vacuum Brazed CuZr and CuCr Structures 100 10 1 10 2 10 3 10 4 10 5 10 6 10 7 80 Normal copper a a a 90 100 110 120 Gradient MV m High Gradient Structures--AAC 2010 Page 11 0.215, t 4.6mm, Frascati 2 0.215, t 4.6mm, CuZr SLAC 0.215, t 4.6mm, CuCr SLAC 130 140 150 1 1 Clamped Structure Diffusion bonding and brazing of copper zirconium are being researched at SLAC. Clamping Structure for testing copper alloys accelerator structure •The clamped structure will provide a method for testing materials without the need to develop all the necessary technologies for bonding and brazing them. •Once a material is identified, we can spend the effort in processing it. •Furthermore, it will provide us the opportunity to test hard materials without annealing which typically accompany the brazing process Test of Hard Copper Clamped Structure with Hard Copper cells Hard Copper showed an observable improvements of annealed brazed structures BreakdownProbability 1 pulsemeter 100 10 1 10 2 10 3 10 4 10 5 10 6 10 7 80 90 100 110 a 0.215, t 4.6mm, Frascati a 0.215, t 4.6mm, Clamped SLAC 1 120 Gradient MV m High Gradient Structures--AAC 2010 Page 13 130 140 2 150 Cryogenic RF material testing at SLAC • Test bed for novel SRF materials – Finding materials with higher quenching RF magnetic field • Leading to higher gradient in SRF accelerator structures • Samples in different forms, thin film or bulk, multilayer, etc – Unique X-band system with compact size and short pulses, resulting lower pulsed heating – Quick testing cycles with small samples – Surface resistance characterization Cavity design High-Q cavity under TE013 like mode H E • High-Q hemispheric cavity under a TE013 like mode – Zero E-field on sample – Maximize H-field on the sample, peak on bottom is 2.5 times of peak on dome – Maximize loss on the sample, 36% of cavity total – No radial current on bottom • Copper cavity body Sample Fres, design=~11.399GHz Fres, 290K=~11.424GHz Fres, 4K=~11.46GHz Tc~3.6µs(using Q value for copper at 4K) – Stable, no transition or quenching – Higher surface impedance – Coupling sensitive to iris radius R=0.95” Q0,4K=~224,000 Q0,290K=~50,000 (measured from bulk Cu samples) Qe~310,000 Q0,4K=~350,000 (Estimated for zero resistivity samples, using measured Cu sample results) • Nb cavity body being designed – Lower loss for more accurate surface impedance characterization – Qext is much higher with smaller iris 300nm MgB2 thinfilm on Sapphire Q vs T H=10mT vs low power 04082010 4 10 5 5 3.5 10 5 5 3 10 5 3 10 2.5 10 5 2.5 10 5 2 10 5 2 10 5 1.5 10 5 1.5 10 5 1 10 5 1 10 5 5 10 4 5 10 4 4 10 5 3.5 10 Q0 from scope w/ Qe_NW Q0 from scope w/ Qe_NW Selected test results: MgB2 on Sapphire Q0 from scope w/ Qe_NW Q0(MgB2_LP_04062010_corr) MgB2 thinfilm on Sapphire QvsH T=3K, 04082010 Q0 from scope w/ Qe_NW 10 15 20 0 0 5 10 15 20 TSample(K) 25 30 35 40 Hpeak from Pf/Ue(mT) 25 30 Experimental Evaluation of Magnetic Field role in Breakdown Rate Experiments with short standing wave structures and specifically with structures where magnetic field is increased due input slots or field-confining rods (PBG) showed that magnetic field plays an important role in determining the gradient limit. Before we studied effect of rf magnetic fields on rf breakdown high-magnetic-field and low-magnetic-field waveguide tests (V.A. Dolgashev, S.G. Tantawi, RF Breakdown in X-band Waveguides, EPAC02) Here we suggest a test that separately controls electric and magnetic fields using the TE01 and the TM02 modes A standing wave accelerator cell with iris dimensions similar to standing wave accelerator structure Feed with TM01 mode converter Electric Field along the surface TM02 Mode with resonance frequency 11.443GHz S. Tantawi A standing wave accelerator cell with iris dimensions similar to standing wave accelerator structure Magnetic Field along the surface TE01 Mode with resonance frequency 11.4244GHz Feed with TE01 mode converter S. Tantawi Rf Breakdown at Cryogenic Temperatures at ASTA We plant to test hypotheses that connect statistical properties of rf breakdowns to dislocation dynamics in metals: this dynamics dramatically changes at cryogenic temperatures Cryostat “Cold head” of refrigerator Single-Cell-SW structure TM01 input waveguide S. Tantawi et al. In-Situ Observation of Metal Surface (KEK, SLAC) • Crystal migration due to pulse heating ― Interferometer ― High resolution microscopy • Pulse temperature measurement by High-Speed Radiation Thermometer • Particles observation by Laser scattering SW structure New pulse heating cavity Future plans for ASTA • • • • • EPICS for remote monitoring and control Spectrometer to measure gradient Phase measurements and breakdown localization 24 hour unattended operation Move cryostat to ASTA Thanks for your attention