Calorimeter Subsystem. Status and Issues. W. Neil Johnson Naval Research Laboratory. Gamma-ray Large Area Space Telescope
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1 Gamma-ray Large Area Space Telescope Calorimeter Subsystem Status and Issues W. Neil Johnson Naval Research Laboratory W N Johnson Calorimeter Subsystem Status
2 Outline Introduction Engineering Model GSI Beam Test Flight Manufacturing Status The Future Issues and Concerns Summary W N Johnson 2 Calorimeter Subsystem Status
3 Calorimeter Module Carbon Composite Structure CsI Detectors + PIN diodes (CDE) Al Cell Closeout Readout Electronics First Flight CAL FM A Mounting Baseplate Al EMI Shield 16 Identical Flight CAL Modules + 2 Spare Modules EM2 TEM/TPS (T&DF SLAC) W N Johnson 3 Calorimeter Subsystem Status
4 CAL EM - Heavy Ion Beam Test Proposal PI: Benoît Lott, CEN Bordeaux-Gradignan Gesellschaft für Schwerionenforschung, Darmstadt, Germany Relativistic heavy ions Pure and Cocktail beams of A = 2Z daughters Tagged with t, Z, A, E, direction Goals of test Develop CAL cosmic ray calibration algorithms Measure scintillation saturation, quenching in CsI(Tl) Develop algorithms to identify charge, mass-changing nuclear interactions Test performance of EM CAL Compare performance with MiniCAL Analyses: IN2P3/CENBG (Benoît, et al.) IN2P3/GAM (Frédéric Piron, et al.) W N Johnson 4 Calorimeter Subsystem Status
5 EM Calorimeter at GSI GLAST setup in FRS cave EM CAL on translation, lift, and pitch table looking up at muons Beam direction 58 Ni, 28 Si, 12 C up to 1.7 GeV/n MiniCAL on lift table W N Johnson 5 Calorimeter Subsystem Status
6 GSI s Fragment Separator (FRS) 58 Ni Beam Degrader EM minical Target Fragments Cocktail beam at 1.7 GeV/nucleon Tagged with t, Z, A, E, direction W N Johnson 6 Calorimeter Subsystem Status
7 Ion selection No Z selectionapplied Z selectionapplied (Z=14) W N Johnson 7 Calorimeter Subsystem Status
8 Quenching factors minical EM dl/de = 1 for protons, muons, electrons. Quenching factor = measured/calculated deposited energy= dl/de Z=6 (C): dl/de=1.23 Z=14 (Si): dl/de=1.08 Z=26 (Fe): dl/de=0.90 «Quenching»: dl/de <1 «Antiquenching»: dl/de>1 W N Johnson 8 Calorimeter Subsystem Status
9 Flight Hardware Manufacture and Test W N Johnson 9 Calorimeter Subsystem Status
10 Crystal Detector Elements (CDE) Swales Aerospace CDE Components Tooling for 72 CDEs bonded per week Crystal jig and diode mask and seal Finished CDEs 1 layer of 1 module W N Johnson 10 Calorimeter Subsystem Status
11 Mandrel wrapping w/ prepreg Carbon Composite Structures IN2P3 Ecole Polytechnique One layer at a time Hot out of the oven a completed structure Stack layers in alignment tooling Vacuum bag assembly for autoclave curing Each one is assembled w/ dummy CDE for vibration strength testing W N Johnson 11 Calorimeter Subsystem Status
12 PreElectronics Module (PEM) Assembly Naval Research Lab CDE Insertion into structure Finished PEM awaiting test Closeout plates keep CDEs in place Even Eric can do it Connect test electronics for muon testing 7 PEM awaiting AFEE installation W N Johnson 12 Calorimeter Subsystem Status
13 PEM Checkout Light Yield 200 Flight CDEs (first 8 PEMs) 200 Flight CDEs (first 8 PEMs) Min. Rqmt Big PIN ~7000 e/mev 50 Min. Rqmt Small PIN ~1200 e/mev Light Yield (e/mev), big PIN Light Yield (e/mev), small PIN Using cosmic muons Verify PIN diode bonds end vs end, big vs small Check light yield Map light asymmetry W N Johnson 13 Calorimeter Subsystem Status
14 CAL Front End Electronics Naval Research Lab Over 12,000 ASICs packaged and tested AFEE circuit board 4 per CAL module The evil eye of QA inspector AFEE burn-in and T cycling 8 at once AFEE soldering 192 wires per side W N Johnson 14 Calorimeter Subsystem Status
15 CAL FMA Final Assembly Naval Research Lab Installation of SLAC s EM2 TEM/TPS Installation of EMI Side Panels lots of fasteners FMA CAL tower complete! CAL clean room and shipping containers W N Johnson 15 Calorimeter Subsystem Status
16 FMA in EMI/EMC Testing FMA Environmental Testing Naval Research Lab Remove FMA from shipping container for vibration testing Comprehensive performance test takes careful monitoring FMA on vibe slip table for lateral test W N Johnson 16 Calorimeter Subsystem Status
17 Light Asymmetry Cosmic Muons Light Asymmetry layer=5, crystal= longitudinal position, cm light asymmetry nonlinearity light asymmetry nonlinearity layer=5, crystal=3 layer 5, crystal longitudinal position, cm longitudinal position, cm W N Johnson 17 Calorimeter Subsystem Status
18 FMA Cosmic Muon Testing W N Johnson 18 Calorimeter Subsystem Status
19 GLAST LAT Project Collaboration Meeting Sep 27 29, 2004 LEX8 Noise Measurement CAL FM LEX8 pedestal rms (MeV) Distribution of 192 pedestal widths (rms) LEX8 noise determines data sparsification energy threshold (Log Accept) Log Accept Threshold will impact energy resolution at low energies. 192 Pedestal width measurements w/ Cosmic muons s ~ 0.2 MeV Log Accept Threshold Need ~ 3 s threshold to limit event size Quantization of Log Accept setting is 0.75 (1.5) MeV For ground testing, log accept threshold of MeV is achievable. In orbit, higher noise is expected. W N Johnson 19 Calorimeter Subsystem Status
20 Calorimeter Assembly Flow and Build Status Dual PIN Diodes 4800 / 4380 Crystal Detector Element (CDE) Assembly 1424 / 1830 Optical Wrap CsI Crystals 1755 / 1830 Mechanical Structure 12 / 18 Front-End Electronics 24 / 110 PIN Diode (each end) Bond CsI Crystal End Cap Wire leads PreElectronics Module (PEM) 8 / 18 # complete # planned Module Assembly & Test 1 / 16 W N Johnson 20 Calorimeter Subsystem Status
21 Near Term Schedule Flight Module A 2 week Thermal Vacuum Test Final Calibration and Performance Tests Ship to SLAC I&T Ready for Integration Completion 13-Oct Oct Nov Nov-2004 Flight Module B Assembly Complete Environmental Tests Complete Ready for Integration 1-Oct Nov Dec-2004 Flight Module 1 Assembly Complete Environmental Tests Complete Ready for Integration 8-Oct Nov Dec-2004 W N Johnson 21 Calorimeter Subsystem Status
22 Issues Performance Higher than expected CDE Light Yield Too much gain, max energy measurement in single Crystal ~50 GeV rather than required 100 GeV Power consumption at -30 deg C is ~ 8 watts over allocation of 65 watts. Manufacturing and Test CAL ASICs have significant ESD vulnerabilities Care in handling and interconnect of AFEE cards is needed to avoid electrostatic discharge damage to board interface signal lines. W N Johnson 22 Calorimeter Subsystem Status
23 Summary CAL subsystem is well into production of flight hardware. The first flight module has been completely assembled and is in environmental test. No issues to date. First delivery to SLAC I&T is scheduled for early November. W N Johnson 23 Calorimeter Subsystem Status
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