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Space Applications: Overview

Space Applications: Overview. Robert P. Johnson Santa Cruz Institute for Particle Physics Physics Department University of California at Santa Cruz. Outline. Tracking detectors Pamela AMS Agile GLAST Compton telescopes MEGA ACT Si/CdTe concept (see earlier talk by Shin Watanabe)

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Space Applications: Overview

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  1. Space Applications: Overview Robert P. Johnson Santa Cruz Institute for Particle Physics Physics Department University of California at Santa Cruz R.P. Johnson

  2. Outline • Tracking detectors • Pamela • AMS • Agile • GLAST • Compton telescopes • MEGA • ACT • Si/CdTe concept (see earlier talk by Shin Watanabe) • Focal-plane detectors—well covered later in this session and also in early sessions • Ground based (see talk by Richard Stover in this session) • LSST (see talk by Steve Kahn in this session) • JDEM/SNAP (see talk by Chris Bebek in this session) • MAXI (see talk by Hiroshi Tsunemi in this session) I will restrict this talk to the use of silicon-strip tracking systems in space. There are by now several examples of HEP-like experiments built for operation in orbit. R.P. Johnson

  3. Pamela Cosmic-ray spectrometer; antimatter search. Permanent magnet: ~0.4 T Measure antiprotons up to 190 GeV. Silicon-strip tracker. Launched earlier this summer from Baikonur. R.P. Johnson

  4. Pamela Pamela completed its instrument checkout in early July and is now taking science data. R.P. Johnson

  5. Pamela Silicon-Strip Tracker • Double-sided, double metal, AC-coupled • 6 planes of 3 ladders each • 300 m thick; 7.0×5.3 cm2 area • 50 m readout pitch • 4 m resolution in bending plane, 15 m in the non-bending plane • 90% efficiency per plane for MIP • VA1 chip used for readout • 62 W power consumption • ~ 3 mW/channel R.P. Johnson

  6. Alpha Magnetic Spectrometer • Cosmic-ray spectrometer. • Antimatter search. • Dark matter search. • Superconducting magnet (0.97 T). • Silicon-strip tracker. Complex particle physics detector for operation in orbit! Destined for the completed space station, which makes its schedule very uncertain at this time. R.P. Johnson

  7. AMS Silicon-Strip Tracker • Double-sided, 300 m thick silicon strip detectors. • Arranged in 8 layers on 5 support planes; 192 ladders (6.45 m2 of Si). • AC coupled to VA-hdr9a chips via capacitor chips (700 pF). • (1284+384)×192=320,256 readout channels. • 10 micron resolution in bending plane (30 micron out of plane). • 734 W/320,256=2.3 mW of power per channel (~0.7 mW/ch in the VA chip). • Active cooling with CO2. R.P. Johnson

  8. AMS Silicon-Strip Tracker • Honeycomb support plane with ladders installed on the top side. R.P. Johnson

  9. AGILE • Gamma-ray (pair-conversion tracker), with about 4 m2 of Si strips • Hard X-ray imaging (coded mask) • To be launched on a PSLV rocket from the Sriharikota base in India • Currently held up by U.S. State Dept. (mindless ITAR issue) R.P. Johnson

  10. AGILE Tracker/Converter • Single sided SSDs, AC coupled, 9.5×9.5 cm2, 410 m thick • 121 m strip pitch; 242 m readout pitch; 38-cm long strips in ladders • Analog readout by the 128-channel TAA1 chip (IDEAS) • 0.4 mW/channel in front end • 36,864 readout channels in 24 layers (12 x,y pairs) • Silicon ladders bonded to top and bottom of composite “trays” • 0.7 X0 tungsten converter foils on the bottom surfaces of the top 10 trays R.P. Johnson

  11. Super AGILE • Hard x-rays (15 to 45 keV) • Silicon-strip plane placed 14-cm below a coded tungsten mask • 6 arc-minute angular resolution, from 121 m strip pitch • 19-cm long silicon strips read by XAA1.2 chips; 410 m thick • 6144 channels Coded Mask Collimator SSDs R.P. Johnson

  12. Super AGILE • 30 pF channel • Sensitivity: ~0.01 Crab in a 14-hour exposure • Energy resolution ~5 keV FWHM • 300 cm2 effective area on axis (~20% of the geometric area) R.P. Johnson

  13. GLAST Large Area Telescope Si Strip Tracker/Converter • 36 single-sided Si layers • 228 m pitch; 400 m thick • 8.95 cm square SSDs • AC coupled • 16 tungsten layers • 884,736 channels • 160 W • Self triggering 74 m2 of Si in the flight instrument About $8 per square centimeter Fairly large HEP detector to operate in orbit: • 3 ton mass (allocated) • ~ million channels • 3 detector subsystems • 5 computers • But only 650 Watts (allocated)! R.P. Johnson

  14. GLAST SSD Tracker/Converter 36 Multi-Chip Electronics Modules (MCM) 19 Carbon-Fiber Tray Panels Carbon-Fiber Sidewalls (Aluminum covered) • Carbon-composite structure supports 18 x and 18 y layers of silicon-strip detectors and 16 layers of tungsten converter foils. • 36 custom readout electronics boards, each with 1536 amplifier channels, mount on the sides of the panels to minimize inter-tower dead space. 2 mm gap between x,y SSD layers Flex-Circuit Readout Cables Titanium Flexure Mounts R.P. Johnson

  15. Tracker Mechanical Fabrication Challenges Top view of 4 Tracker Modules Tray X-section of tray edge <18 mm from active Si to active Si! Sidewall 1 Tracker Tray Right-angle interconnect Very tight space for electronics High precision carbon-composite structure to maintain 2.5 mm gaps between modules MCM R.P. Johnson

  16. GLAST Tracker Electronics ASIC based, for minimum power (180 W/ch). Digitize on chip: No coherent noise or pedestal variation! Single threshold (0 or 1). ToT on trigger OR. Internal calibration system. Threshold & Cal DACs. Redundant 20 MHz serial control and readout paths. 4 event buffers at front end  negligible deadtime (few s). Direct descendent of the BaBar ATOM-based FE system (UCSC/LBNL/INFN). 0.5 m CMOS GTRC ASIC GTFE ASIC R.P. Johnson

  17. GLAST Tracker Status 16+2 towers completed. Flight array fully integrated in completed LAT. Environmental testing completed at NRL. Delivery to General Dynamics this month. Two spare towers in beam testing at CERN. R.P. Johnson

  18. Muon time-over-threshold (OR of all channels per layer) GLAST Tracker Performance 1 example readout module Threshold variation <9% rms in all modules (5.2% on average) Hit efficiency from cosmic-ray muons Strip #, 1 to 1536 • Hit efficiency (in active area) >99.4% • Overall Tracker active area fraction: 89.4% • Noise occupancy <5×107 • (with small number of noisy channels masked) • Power consumption 158 W (178 W/ch) • Time-over-threshold 43% FWHM R.P. Johnson

  19. Cosmic-Ray Gamma Conversions in 8 Towers Launch in autumn 2007 R.P. Johnson

  20. Compton Telescopes • Two general concepts have been competing for the next generation detector, to improve upon Comptel: • Classic: measure energy loss, direction, and total energy • e tracking: add measurement of the electron direction • Also capable of fully measuring pair conversions. • 3-Compton: measure 1 scattering angle and 2 energy losses 3-Compton: ACT, NCT, LXeGRIT e tracking: MEGA, TIGRE Classic: Comptel R.P. Johnson

  21. NRL Advanced Compton Telescope • 7 mm thick Si (Li drifted) detectors (alternative to Ge) • ~300 V bias • 1010 cm2 wafers • 4×4 arrays, stacked 24 deep • Cooled to 40C • 4 of these towers are proposed for the complete instrument • Improve on the Comptel sensitivity by factor of ~100 See also the talk in this conference by Mark Amman on the alternative Ge strip detectors. R.P. Johnson

  22. MEGA See also the talk by Shin Watanabe (Si/CdTe Compton telescope concept) in this conference for another interesting example. Prototype: • 11 layers of 3×3 array of 6-cm square wafers, each 500 m thick. • 470 m strip pitch • 1 cm spacing between layers • calorimeters with 0.5-cm square CsI scintillators, 8-cm deep, with PIN diode readout Satellite concept: • 32 silicon layers • 6×6 array of 6-cm wafers in each layer • calorimeter surrounding the lower hemisphere, 8-cm thick on the bottom and 4-cm thick on the sides • drift diode readout • Good sensitivity from 0.5 MeV to ~100 MeV, using both Compton scattering and pair conversion. R.P. Johnson

  23. Conclusion • We are starting to see HEP-like solid-state tracking detectors put into orbit, with 105 to 106 channels. • AMS-1 (shuttle flight) and Pamela (in orbit) • AGILE and GLAST are close to launch • The detector systems and DAQ are relatively simple or small compared with state-of-the-art ground-based detector systems, but the environment (rocket ride, power, thermal, QA) is challenging. • Many lessons learned by these groups that could/should be applied to future projects • There is a lot of scientific and technical interest in a large Compton telescope, but unfortunately no major mission in sight at this time. R.P. Johnson

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