GLAST Proposal Review - PowerPoint PPT Presentation

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GLAST Proposal Review

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... working but needs some logic corrections for flight (new logic under test in FPGAs) ... the Tracker Peer Review results in numerous flight Tracker procurements ... – PowerPoint PPT presentation

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Title: GLAST Proposal Review


1
GLAST Large Area Telescope Tracker
Subsystem Robert Johnson Santa Cruz Institute
for Particle Physics U.C. Santa Cruz Tracker
Subsystem Manager johnson_at_scipp.ucsc.edu 831-459-
2125
2
Outline
  • Overview
  • Schedule
  • Roadmap to Manufacturing
  • Top Issues and Risks

3
Design Overview
Multi-Chip Electronics Module (MCM)
  • 19 stiff composite tray panels support SSDs on
    both faces with electronics on two sides.
  • Converters are on the bottom face, just above the
    SSD plane
  • 2-mm gap between trays
  • 16 layers of tungsten converter foils.
  • 12 layers of 3 X0 converters
  • Followed by four 18 layers
  • 18 x and 18 y SSD planes.
  • Carbon-fiber sidewalls conduct heat to the base
    and stiffen the module.
  • Electronics are based on 2 ASICs, PC boards, and
    custom flex cables.
  • 31.6 kg mass per module.
  • 10.5 W of power per module.

19 Carbon-Fiber Tray Panels
Carbon-Fiber Wall
2 mm gap
Readout Cable
4
Production Overview
Module Structure (walls, flexures,
thermal-gasket, fasteners) Engineering SLAC,
Hytec Procurement SLAC
SSD Procurement, Testing Japan, Italy, SLAC
SSD Ladder Assembly Italy
10,368
Tracker Module Assembly and Test Italy
2592
18
Tray Assembly and Test Italy
342
342
Electronics Design, Fabrication Test UCSC, SLAC
Composite Panel Converters Engineering SLAC,
Hytec, and Italy Procurement Italy
648
Cable Plant UCSC
5
Near-Term Schedule (?key milestone)
6
Near Term Schedule
7
Tracker Production Flow
SSD Production and Test 11/01-10/03
ASIC Procurement, Test and Dicing 12/02-5/03
PWB Procurement and Flex Attach 1/03-3/03
Ladder Assembly and Test 11/02-10/03
MCM Assembly Test and Burn-in 3/03-10/03
Tray Panel Fab And test 1/03-11/03
Readout Cable Fab and Assembly 2/03-10/03
Tray Assembly And test 7/03-4/04
Sidewall Fabrication 2/03-10/03
Tower Assembly 10/03-5/04
Tower Testing 11/03-8/04
8
Major Procurements
9
Progress Since Delta-PDR
  • ASIC design and test
  • GTFE design is fully functional.
  • GTRC is working but needs some logic corrections
    for flight (new logic under test in FPGAs).
  • 3 complete MCMs (26 chips each) are under test.
  • Mini-MCM connected to full SSD ladder
    demonstrated satisfactory noise performance.
  • Radiation testing in progress.
  • GTFE wafer probing working.
  • MCM production testing is ready for EM
    production.
  • Prototype EGSE test stand exercised with multiple
    MCMs.
  • EM MCM production
  • In progress at Teledyne Electronics Technologies
  • Flex cables
  • Draft spec in place.
  • EM cables nearly finished.
  • SSD procurement total
  • 4600 delivered.
  • 3500 tested by LAT.
  • Ladder assembly
  • EM ladders completed.
  • PRR held for flight ladders.
  • Flight ladder assembly begun at GA Engineering
    (30 in test).
  • Tray fabrication
  • At least 16 EM panels fabricated at Plyform.
  • Satisfy dimensional tolerances.
  • Fixtures are ready for Kapton, tungsten, and SSD
    mounting.

10
Design Status Work Still in Progress
  • Electronics
  • GTRC/GTFE ASIC designs need some small
    modifications to increase timing margin in data
    transfer between the two.
  • Bottom Tray and Tower-Grid Interface
  • Invar closeout has been investigated and is now
    only a backup solution.
  • Reinforcement of the existing design is being
    followed in work with COI and Hytec. Coupon
    testing and preparation of a prototype tray will
    be completed one month from now.
  • Hytec will be updating the tower model,
    completing analysis work, and preparing load and
    vibration tests.
  • Tower Sidewalls
  • Design in the high-conductivity material exists
    and is being prototyped and tested in Italy.
  • Drawings
  • 79 design drawings are in Cyberdocs and on the
    Tracker Web drawing tree.
  • At least 28 are released and under configuration
    control.
  • Assembly Fixtures
  • Tower assembly fixture design is in progress (2nd
    iteration). This work includes study of
    alignment of Grid mounts.
  • All other fixture designs are complete and in use
    for EM fabrication.

11
Tracker Engineering Model
  • Full-scale mechanical-thermal tower
  • 19 Trays, sidewalls, flexures, etc. to the flight
    design.
  • Dummy Si detectors (including some HPK SSD
    rejects).
  • Dummy MCMs loaded with resistors to dissipate the
    expected electronics power load.
  • Functional mini-tower
  • 4 trays loaded with 3 x-y planes of functional
    detectors and electronics and 3 planes of
    tungsten foil.
  • 1 bottom dummy tray without electronics for a
    Grid interface.
  • Aluminum sidewalls.
  • Standard readout cables.
  • Functional qualification tray
  • Another functional tray for additional
    environmental testing.
  • MCMs
  • 8 additional functional MCMs for qualification
    and electronics testing.

12
Tracker EM Test Matrix
13
EGSE and MGSE
  • EGSE
  • MCM acceptance testing and tray-level electronics
    tests
  • Simplified system exists and works well.
  • Some software development still needed to
    simplify use interface.
  • Some recoding from Python to C needed to speed up
    execution.
  • 4 systems needed for production (already exist).
  • Tower-level testing
  • Standard TEM-based test stand.
  • In use already at SLAC with Tracker front-end
    electronics.
  • Work beginning in California Italy to develop
    tower-level test scripts.
  • 8 systems are needed for production!
  • MCM Burn-in
  • Special readout cables are in fabrication.
  • Control and readout will be done by the TEM-based
    test stand.
  • MGSE
  • Tower lifting fixture
  • Design concept exists but detailed design not
    done.
  • Tower vibration fixture
  • Design is complete.
  • Tower shipping containers
  • No design yet.

14
Top Issues and Risks
  • Bottom tray and Tracker-Grid interface design
  • Impact
  • Already has delayed the Tracker Peer Review into
    April 03.
  • Further delays are possible if the present
    development line doesnt work and invar (or
    another material) has to be used.
  • Issue
  • We need specifications for realistic input levels
    to use in designing the tower-Grid interface
    stiffness, to ensure that towers do not touch
    during launch.
  • Mitigation
  • Two engineering firms (COI and Hytec) are engaged
    in the design, analysis, and testing.
  • A program of coupon testing is under way at COI
    to prove the redesigned flexure attachment joint.
  • Mechanical testing will be carried out on a
    prototype (refitting of an existing tray) prior
    to the engineering model.
  • Status
  • Invar development on hold after preliminary
    magnetic measurements.
  • Received report from Hytec on issues with invar
    and other materials.
  • Coupon testing and refitting of the test tray
    will complete by Dec. 15.

15
Bottom Tray Reinforcement
Modified Ti Side Fitting to Bond to Sandwich Panel
Concept under study and test for reinforcing the
bottom tray and the flexure mounts.
Double-Lap-Bond Ti Corner Fitting
Carbon-composite angle brackets
16
Top Issues and Risks
  • ASIC Design and Production
  • Issuesome modifications are still needed for the
    flight run
  • Several logic errors remain in the latest GTRC
    prototype IC, even though it works sufficiently
    well for EM production and testing.
  • Data transfer from GTFE to GTRC works at 2.5V and
    20 MHz, but with no margin to go to lower voltage
    or higher frequency.
  • About 20 of the GTFE-G are unstable at low
    threshold.
  • Impact a failure of the production run would
    delay the Tracker delivery by about 4 months.
  • Mitigation
  • A new board with 2 FPGAs and 2 GTFEs is being
    used to verify the modified VHDL code, including
    our corrections of the logic errors.
  • The timing issues are being intensively studied
    in simulation to be sure that we understand them.
    A small modification will probably be put in to
    correct it (otherwise VDD will have to be raised
    to 2.8V).
  • The GTFE-G stability problem has been understood
    and the correction was tested on actual chips by
    FIB surgery.
  • Status the December submission date is tight but
    can be met.

17
Top Issues and Risks
  • Overlap of Procurements and Tracker Peer Review
    Preparation
  • Issue slippage of the Tracker Peer Review
    results in numerous flight Tracker procurements
    occurring prior to it (see page 8)
  • SSD procurement and ladder production
  • These were always scheduled to occur before CDR
  • CDR and PRR have already been completed for these
    items
  • Mechanical materials and assembly of tray panels
  • ASIC production and other electronics parts
  • Impact
  • Several item-specific CDRs / PRRs need to be held
    prior to the Tracker Peer Review
  • ASIC (December)
  • PWB, pitch-adapter flex (January)
  • Tray panel fabrication, face sheets, bias
    circuits, etc. (January)
  • Flex-circuit readout cables (may be able to delay
    this one beyond CDR)
  • Potential manpower conflicts with EM testing and
    CDR preparation.
  • Mitigation
  • We need to work with management to schedule and
    streamline the PRRs.
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