Ultra high brightness photoinjector for EBTF/CLARA facility at Daresbury B.L. Militsyn on behalf of the ASTeC photoinjector development team Accelerator.

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Presentation transcript:

Ultra high brightness photoinjector for EBTF/CLARA facility at Daresbury B.L. Militsyn on behalf of the ASTeC photoinjector development team Accelerator Science and Technology Centre Science & Technology Facility Council, Daresbury, UK

Daresbury Science and Innovation Campus, Daresbury, Cheshire, UK 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 2/29

Outline High brightness Electron Beam Test Facility (EBTF) EBTF photoinjector –Photocathode gun –Beam dynamic simulations –Metal photocathode research program –Laser system –Beam diagnostic –RF system CLARA – ultra short pulse high brightness research accelerator Conclusion 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 3/29

Electron Beam Test Facility EBTF Objective: To provide a suite of accelerator testing facilities which can be utilised in partnership with industry, academic and scientific collaborators Scope: The provision of a common high performance and flexible injector facility comprising an RF gun, associated RF power systems, beam diagnostics and manipulators, a high power photo-injector drive laser and associated enclosures Costs: £2.5M capital from DBIS has been assigned for this facility. This investment will be supplemented by £447k capital allocation from STFC’s baseline capital allocation for the accelerator test facilities Timescales: Purchase the majority of the equipment in financial year 2011/12, with build in It is planned that first electrons from the facility are delivered in December March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 4/29

EBTF beam parameters Beam Energy 4 ‐ 6.5 MeV Bunch Charge (minimum)~1 pC - 20 pCElectron diffraction CLARA Bunch Charge (max)250 pCIndustrial users Bunch length (rms)40 fsecWith 100 fsec FWHM laser pulse (at low bunch charge) Normalised beam emittance (min – max) 0.1 ‐ 2 mm  mrad Depending on the bunch charge RMS beam size (min ‐ max)0.1 ‐ 3.5 mmLow ‐ high charge Energy spread (maximum)3.3 %changing due to space charge RF repetition rate 1 ‐ 400 Hz Modulator 400 Hz Maximum laser repetition rate 1 kHzLaser will be delivered with a repetition rate of 400 Hz. 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 5/29

General layout 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 6/29

Construction Modules Module 1 Module 2 Module 3 Module 4 Module 5 Module March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 7/29

Photoinjector Module Gun Solenoid Lightbox YAG, H & V Slit Collimators 4 x Ion Pump Transverse Deflecting Cavity YAG, V & H Slit Quadrupole magnets Synthetic Granite Girder WCM Support Pedestal YAG, V Slit 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 8/29

EBTF photoinjector based on the ALPHA-X 2.5-cell S-band gun (TU/e-Strathclyde-LAL) 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 9/29

Photocathode gun cavity ParameterValueUnits Frequency2998.5MHz Bandwidth< 5MHz Maximum beam energy6MeV Maximum accelerating field100MV/m Peak RF Input Power10MW Maximum repetition rate10Hz Maximum bunch charge250pC Operational Temperature °C Input couplingWR March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 10/29

EBTF beam dynamics simulation. Bunch charge1pC, RMS laser pulse length 40fs 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 11/29

EBTF beam dynamics simulation. Bunch charge250 pC, RMS laser pulse length 40fs 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 12/29

Metal Photocathodes Metal cathodes have fast response time to seconds. They are robust and can survive months at high surface fields to produce high brightness beam However due to the high work function an UV drive laser is required to achieve reasonable QE. 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 13/29

Photocathode performance research program Photocathode performance Establish reliable and reproducible sample preparation procedure to minimise the final surface contamination Prepare atomic flat surfaces for single crystal and poly-crystalline copper Produce and investigate engineered rough surface Determine QE for different method of surface regeneration (Ar, H and Ozone cleaning) Determination of surface roughness after each procedure Identify the effect each individual residual gas species(H 2, CO, CO 2, H 2 O and CH 3 ) on QE degradation Optimization of wide band gap coating (CsBr) on copper Study and optimisation of the photocathode operational environment Investigation of the gas atmosphere in the operational gun Definition of the gas spices, responsible for the photocathode degradation Optimisation of the cavity preparation procedure to minimise photocathode degradation Investigation of impact of the back stream bombardment on the photocathode lifetime Design photoctahode transport system a nd study its effectiveness 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 14/29

Commissioning of the Photocathode Preparation and Characterisation Facility 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 15/29

Surface Science Analytical tools Available in-situ in house: X-ray Photoelectron spectroscopy (XPS) : to determine surface and near surface ( 9nm) chemical state Auger Electron spectroscopy (AES)/ Mapping : to determine surface and near surface composition Ion scattering spectroscopy (ISS): to determine surface composition Ultraviolet Photon Spectroscopy (UPS): to determine the electronic structure of solids and the adsorption of relatively simple molecules on metals In-situ UHV Atomic force /Scanning Tunnelling Microscope: to determine the surface topography. Low Magnification (5000) SEM Ar and H ion gun to clean the photocathode by ion bombardment Direct Access at Universities: High Resolution SEM to determine surface and depth structure. Energy dispersive Spectroscopy (EDS): to determine in depth composition Electron Backscattered Diffraction (EBDS) : to determine surface crystal structure and orientation. X-ray Diffraction (XRD): To determine depth crystal structure and orientation, grain size and lattice strain. 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 16/29

Drive laser system Wavelength, nm266 Pulse energy, mJ>1 Pulse duration, fs< 100 FWHM Pulse repetition rate, kHz1 Transverse beam quality M 2 < March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 17/29

RF Requirements ParameterValueUnits Frequency MHz Bandwidth (1 dB points)<10 MHz Total peak output power> 8 MW MW Power gain> 45 dB Nominal efficiency> 45 % Pulse Repetition Rate Range1 – 400 Hz RF Pulse Duration<3.5 µs RF Flat Top Pulse Width>2.5 µs Amplitude stability Phase Stability0.1 ° Noise Power Within the Bandwidth< -60 dB Spurious Noise Power Outside the Bandwidth< -35 dB dB 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 18/29

TH 2157A Data Sheet RF Performance TH 2157 TH 2157A Unit s Frequency MHz Output power: Peak MW Average108 kW RF Pulse Width863.5 μsμsMax Saturated Gain454850dBMin Efficiency48 %Typ Electrical characteristics Cathode Voltage kVTyp Beam Current ATyp Heater Voltage15 VMax Heater Current15 AMax 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 19/29

Tuning studs Input coupler Dummy Load/Vacuum port CF70 entrance flange CF70 exit flange 9 cell Transverse Deflecting Cavity 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 20/29

H-field E-field On-axis fields of the transverse deflecting cavity Estimated peak transverse voltage 5 MV (limited by available RF power) Estimated resolution at 25 MeV beam energy ~30fs 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 21/29

TDC at low beam energy Vertical trajectories Energy No correctors 1 st corrector 2 nd corrector TDC introduces vertical streak along length of bunch allowing bunch length to be measured. However, it also produces unwanted vertical kick Offset beam “sees” longitudinal fields, leading to energy variation. 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 22/29

EBTF layout User Area 1 User Area 2 Laser room Rack room CLARA expansion pathway Accelerator area 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 23/29

Positioning of the first block 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 24/29

CLARA (preliminary layout) Linac 1+2 are 2m S-band modules Linac 3+4 are 5m S-band modules Two stage compression  Velocity bunching  Magnetic chicane Linac 2 Linac 1GunGun Linac 3 Linac 4 5 MeV 10 MeV (bunching) 35 MeV (accelerating) 50 MeV 145 MeV 240MeV Single-spike SASE, EEHG, HGHG, novel short pulse schemes Charge ranges from 10 pC – 250 pC 1 mm mrad and less emittance 300 A current over 300 fs bunch length for seeding schemes 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 25/29

Preliminary Parameters of the CLARA FEL Beam Energy ~250MeV SASE Saturation length <15m Seed with Ti:Sa 800nm, lase up to 8 th harmonic Seeding with HHG at 100nm also possible Single spike SASE driven by electron bunches length ~50fs FWHM and charge <20pC Seeding driven by electron bunches with a peak current ~400A, flat top ~300fs and charge <200pC 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 26/29

Conclusion EBTF high brightness electron photoinjector is funded and under construction –Front end for ongoing project CLARA –Source of electrons for industrial and scientific users –Operation with ultra short bunches –Experiments with electron difraction Photocathode research program –Metal photocathode development program has been started and successfully expanded 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 27/29

Thanks to: D. Angal-Kalinin C. Hill S.P. Jamison J.W. McKenzie K.J. Middleman M.D. Roper R.J. Smith B.J.A. Shepherd R. Valizadeh A.E. Wheelhouse 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 28/29

Thank you for your attention! 5-9 March 2012 B.L. Militsyn, FLS 2012, Newport News, USA 29/29