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XTOD Diagnostics for Commissioning the LCLS*. January 19-20, 2003 LCLS Undulator Diagnostics and Commissioning Workshop Richard M. Bionta.
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XTOD Diagnostics for Commissioning the LCLS* January 19-20, 2003 LCLS Undulator Diagnostics and Commissioning Workshop Richard M. Bionta *This work was performed under the auspices of the U.S. Department of Energy by the University of California, Lawrence Livermore National Laboratory under contract No. W-7405-Eng-48 and by Stanford University, Stanford Linear Accelerator Center under contract No. DE-AC03-76SF00515.
Provides unobstructed vacuum path from end of undulator to end of FEH Flux densities in NEH will be the highest available Flux densities in FEH will be similar to synchrotron facilities WBS 1.5 X-Ray Transport, Optics, & Diagnostics (XTOD) FEH - Far Experimental Hall Tunnel NEH - Near Experimental Hall FEE Front End Enclosure LCLS X-Ray Beam R. M. Bionta
X-ray Transport, Optics, and Diagnostics Layout Each 13 m long hutch has two vacuum tanks for experimental and facility hardware NEH FEH FEE Tunnel FEL Measurements & Experiments: Compression Spectra Coherence Pulse Length Experiments Optics Structual Bio Nano-scale Femtochem Front End Enclosure Diagnostics Slits Attenuators Low Energy Order Sorting Mirror Monochrometer Pulse-Split & Delay Diagnostics Experiments: Optics Warm Dense Matter Atomic Physics R. M. Bionta
FEL beam power levels Saturated power Plasma frequency FEL r parameter Gain length parameterization Correct definition of h parameters R. M. Bionta
Spatial-temporal shape FEL can be modeled as a Gaussian beam in optics Phase curvature function Gaussian width Gaussian waist Origin is one Rayleigh length in front of undulator exit Amplitude is given in terms of saturated power level R. M. Bionta
LCLS Fundamental Electric Field and Dose Equations Gaussian Electric Field: Phase Curvature waist With origin Waist at origin matches electron distribution gives Electric field intensity x duration Matches photon distribution with Peak photon density Dose R. M. Bionta
FEL parameters at absorber exit, z = 65 meters And at other locations: R. M. Bionta
0 150 Ginger provides complex Electric Field envelope at undulator exit Data in the form of Each radial distribution has radial distributions of complex numbers representing the envelope of the Electric Field at the undulator exit. radial points. R, mm Electric Field Envelope Power Density vs time at R = 0 Samples are separated in time by wavelengths. watts/cm2 Time between samples is R. M. Bionta
watts c m2 watts c m2 watts c m2 watts c m2 x 1015 x 1017 x 1017 x 1015 Power Density Time Domain Frequency Domain Power Density 1.94 Temporal Transform 1.73 0 0 w0-400/fs w0 w0+400/fs 2 4 0 6 Time, femtoseconds frequency 0 150 Spatial Transform Power Density Power Density 1.94 1.73 0 0 -325 -10 304 -150 0 150 Wavenumber, mm-1 Transverse position, microns Tools for manipulating GINGER output Viewer GINGER output: Tables of electric field values at undulator exit at different times viewer R, mm Transformation to Frequency Domain Propagation to arbitrary z R. M. Bionta
FEL spatial FWHM downstream of undulator exit, l = 0.15 nm Transverse beam profile at undulator exit Ginger (points) Transverse beam profile 15 m downstream of undulator exit Gaussian Beam (line) R. M. Bionta
Total power at undulator exit • 10 Ginger simulations were run at different electron energies but with fixed electron emittance through 100 meter LCLS undulator. Ginger simulations • The Ginger runs at the longer wavelengths were not optimized, resulting in significant post-saturation effects. Results at longer wavelengths carry greater uncertanty. Theoretical FEL saturation level R. M. Bionta
watts c m2 x 1017 3 Power Density 0 w0 = 12558 /fs w0 + 50 /fs w0 - 50 / fs frequency RMS Bandwidth l= 0.15 nm Time Domain l= 0.15 nm Frequency Domain R. M. Bionta
300 meters 75 meters 0 meters FWHM vs. wavelength at 0, 75 and 300 meters R. M. Bionta
We can confidently calculate the dose to transmissive optics. Transmissive Dose Model Reflective Dose Model Low Z materials for transmissive optics can be chosen to survive in the LCLS experimental halls in the simple dose model on the left. The survivability of common high Z reflectors depends on additional assumptions. R. M. Bionta
Dose / Power Considerations Fluence to Melt Energy Density Reduction of a Reflector Be will melt at normal incidence at E < 3 KeV near undulator exit. Using Be as a grazing incidence reflector may gain x 10 in tolerance. R. M. Bionta
Roman’s far Field spontaneous R. M. Bionta
Detailed Spontaneous, in progress R. M. Bionta
E > 400 KeV R. M. Bionta
FEE Instrumentation R. M. Bionta
Front End Enclosure Layout PPS Diagnostics Slits Solid Attenuator 40m WestFace Near Hall Gas Attenuator 33m WestFace Dump Windowless Ion Chamber Diagnostics 10.5 m Slits Slow valve Fast valve Fixed Mask Pump 16.226 m Eastface Last Dump Mag Westface front End Enclosure Valve Pump 0 m End of Undulator R. M. Bionta
Adjustable High-Power Slits • Intended to intercept spontaneous beam, not FEL beam -- but will come very close, so peak power is an issue • Two concepts being pursued for slit jaws • Treat jaw as mirror (high-Z material) • Treat jaw as absorber (low-Z material • Either concept requires long jaws with precision motion • Mechanical design based on SLAC collimator for high-energy electron beam R. M. Bionta
Front End Diagnostic Tank Solid Filter Wheel Assembly ION Chamber Be Isolation valve Space for calorimeter Direct Imager Indirect Imager Turbo pump R. M. Bionta
Prototype LCLS X-Ray imaging camera CCD Camera Microscope Objective X-ray beam X-ray beam LSO or YAG:Ce crystal prism assembly R. M. Bionta
Indirect Imager Be Mirror Be Mirror Reflectivity at 8 KeV 1 Be Mirror angle provides "gain" adjustment over several orders of magnitude 0.1 0.01 0.001 0.0001 R. M. Bionta
Multilayer allows higher angle and higher transmision but high z layer gets high dose Be Mirror needs grazing incidence, camera close to beam Single high Z layer tamped by Be may hold together R. M. Bionta
First check CCD by measuring Response Equation Coefficients Digitized gray level of pixel in row r, column c. Electronic gain in units grays/photo electron. Signal in units photo electrons. Pixel Sensitivity non-uniformity correction. Pixel Dark Current in units photo electrons/msec. Pixel fixed-pattern in units grays. Integration time in units msec. R. M. Bionta
Photon Transfer Curve Temporal mean gray level of pixel r,c. Temporal gray level fluctuations of pixel r,c. R. M. Bionta
Calibration Data for one pixel R. M. Bionta
Calibration Coefficients for All Pixels R. M. Bionta
LSO Monte Carlo Bend Photon Monte Carlo Simulations for predicting lens and camera performance Y, microns X, microns X Ray Photons SPEAR source simulation Visible photons R. M. Bionta
Direct Imager Version 1 efficiency R. M. Bionta
Camera Sensitivity Measurements at SPEAR 10-2 attenuator Ion chamber Imaging camera Ion Chamber Photon rate Sum of gray levels R. M. Bionta
Measured and predicted sensitivities in fair agreement R. M. Bionta
Camera Resolution Model R. M. Bionta
Camera Resolution in qualitative agreement with models 1.1 mm R. M. Bionta 1.5 mm 1.5 mm
Camera Resolution Quantitative Data Analysis in progress R. M. Bionta
Micro Strip Ion Chamber Cathodes Isolation valve with Be window Windowless FEL entry Segmented horizontal and vertical anodes Differential pump Differential pump R. M. Bionta
Gas Attenuator • For use when solid absorber risks damage (low-E FEL, front end) • Windowless, adjustable attenuation • Can provide up to 4 orders of magnitude attenuation R. M. Bionta
Solid Attenuator • B4C attenuators can tolerate FEL beam at E > 4 keV in FEE, and at all energies in experimental hutches • Linear/log configurations • Can be wedged in 2 dimensions for continuously variable attenuation • Translation stages provide precision X and Y motion R. M. Bionta
Missing • Predicted performance of direct and indirect imager for Spontanous vs. I, and FEL vs. Power • Calculations of linearity and signal levels in Ion chamber • Integration with FEE + Beam Dump floor plan R. M. Bionta
Commissioning Diagnostic Tank R. M. Bionta
Commissioning Diagnostics Measurements • Total energy • Pulse length • Photon energy spectra • Spatial coherence • Spatial shape and centroid • Divergence R. M. Bionta
Commissioning diagnostic tank Detector and attenuator Stage Aperture Stage “Optic” Stage Rail alignment Stages Rail R. M. Bionta
Costing based on SSRL 2-3 set up R. M. Bionta
Total Energy Temperature sensor Poor Thermal Conductor absorber Heat Sink Crossed apertures On positioning stages Attenuator Scintillator R. M. Bionta
Photon Spectra Measurement Detector and attenuator Stage Aperture Stage Crystal (8KeV) Grating (0.8 KeV) Stage X ray enhanced linear array and stage R. M. Bionta
Spatial Coherence Measurement Detector and attenuator Stage Slits Stage Array of double slits R. M. Bionta
Spatial shape, centroid , and divergence • A1 • A2 • A4 • FEE: HALL A FFTB Diagnostic Tanks FEE 1 & 3: Commissioning Diagnostic Tank A4-1 Diagnostic Tank A1-1 Spatial shape, centroid , and divergence measured by combining data from the imagers in these tanks. R. M. Bionta
Rad Sensor - a candidate technology for LCLS pulse length measurement and pump probe synchronization Rad sensor is an InGaAs optical wave guide with a band gap near the 1550 nm. X-Rays strike the rad sensor disturbing the waveguide’s electronic structure. This causes a phase change in the interferometer. The process is believed to occur with timescales < 100 fs. SPEAR Single electron bunch mode 1550 nm optical carrier X-Ray Photons X-Ray measurements of the time structure of the SPEAR beam in January and March 2003 confirmed the devices x-ray sensitivity for LCLS applications. Rad sensor is inserted into one leg of a fiber-optic interferometer. phase 1550 nm optical carrier beam splitter Reference leg Detector time Point of interference X-Ray induced phase change observed as an intensity modulation at point of interference Fiber Optic Interferometer Mark Lowry, R. M. Bionta