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GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 1 GLAST Large Area Telescope: Calorimeter (CAL) Subsystem.

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Presentation on theme: "GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 1 GLAST Large Area Telescope: Calorimeter (CAL) Subsystem."— Presentation transcript:

1 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 1 GLAST Large Area Telescope: Calorimeter (CAL) Subsystem WBS: 4.1.5 W. Neil Johnson Naval Research Lab, Washington DC Calorimeter Subsystem Manager neil.johnson@nrl.navy.mil (202)–767–6817 Gamma-ray Large Area Space Telescope

2 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 2 Contents  Technical Status  Schedule  Cost and Budget  Next 6 months  Summary

3 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 3 Technical Status Engineering Model  Completion of the CAL Engineering Model environmental test program (qualification levels)  No problems identified in Vibration or Thermal Vac testing  EMI/EMC issues were identified –Contributing causes – test configuration issues and fidelity of TEM/PS unit used (GSE not flight-like). –Design changes have been applied to flight design to address these problems.  EM CAL supported LAT I&T development at SLAC  EM CAL performance measured at heavy ion beam test at GSI in Darmstadt, Germany. EM Calorimeter installation at heavy ion beam facility EM Energy vs Beam Tagger shows quenching in CsI

4 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 4 Technical Status Crystal Detector Elements  CsI Crystal Procurement essentially complete (~80% delivered from Amcrys-H).  Hamamatsu photodiode procurement is complete.  PIN Diode Assembly process and contract established. Flight production is well under way (> 40% complete).  PIN diode and CDE qualification programs are complete.  Flight CDE production is well under way (>25% complete.) ISSUES: None SCHEDULE:Baseline CDE Bonding at Swales Aerospace PIN Diode Assembly (PDA)

5 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 5 Technical Status Mechanical Structure  All flight machined aluminum, titanium and steel parts have been manufactured and plated as required.  Flight carbon composite structure manufacturing process has been finalized at IN2P3/LLR and qualified with Structural Model 2 (SM2) testing.  First three flight structures have been manufactured, tested. Two have been delivered to NRL. ISSUES:None SCHEDULE: - 35 Day Variance Carbon structure with test Al parts and dummy CDEs Vibration test of FMA structure

6 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 6 Technical Status ASICS  New revision of analog ASIC, GCFE9A, has been manufactured and tested.  Over 11,000 flight parts were received after two month delay in packaging at ASAT in Hong Kong.  SEE Radiation testing is complete. Only TID testing remains.  Functional test screening provided >7,000 parts. Screening and qualification program is on-going. No problems to date. ISSUES: Recovering from 9 week delay in delivery. Use before completion of qualification. SCHEDULE: -53 day variance Radiation Testing at Brookhaven Thermal forcing unit for ASIC functional testing at temperature extremes.

7 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 7 Technical Status Analog Front End Electronics  All EEE parts are approved except ASICs which are in qualification testing.  Radiation testing complete except for Total Dose on ASICs. No problems to date.  Prototype of flight AFEE boards have been manufactured, assembled and tested.  Minor adjustments required to avoid potential mechanical interference with structure for parts added for EMI/EMC filtering.  Flight PCBs are being manufactured.  Contract for assembly of flight AFEE boards is in place. ISSUES: Rework of mechanical interference problems on PCB and pre- production review SCHEDULE: -24 day variance Prototype Flight AFEE Card Assembly

8 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 8 Technical Status Assembly and Test  GLAST CAL assembly and test clean room has been commissioned.  Upgrades for improved control of humidity are underway.  Assembly of the Pre Electronics Module (PEM) for the first flight module is in progress. CDE Insertion into structure #1 ISSUES: None SCHEDULE: -17 day variance

9 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 9 Outstanding Issues  EMI/EMC performance  Design changes have been made to address EMI/EMC problems discovered in CAL EM testing.  Outstanding issues are –Shielding of CAL – TEM cable and box attach points. –Test specification – difficulty in separating CAL and TEM/PS performance issues. –Test configuration – identification of subsystem configuration which represents LAT environment, shielding, etc. First opportunity to close this issue is during testing of FMA.

10 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 10 CAL Risk Summary ID # Risk Rank Risk DescriptionRisk MitigationStatus CAL- 0008 Low IF a problem is found in CAL AFEE board design, SMT manufacturing, testing, PEM assembly and qualification (due to late qualification) THEN redesign of AFEE boards will cause schedule slip. 1.Prototype of board layout was manufactured and hand assembled. Several minor layout changes are required for final flight. 2.First flight article will be assembled, tested and thermal cycled before release to assembly of remainder. Schedule issue, however. On Track CAL- 0010 Low IF CAL ASICs fail qualification testing; THEN the flight CAL AFEE boards in build will be impacted causing schedule impact and loss of flight parts. Boards will be assembled in three lots 1.1st article verification 2.lot of 6 modules 3.lot of 18 modules the assembly of which will not occur until qualification testing is complete. On Track CAL- 0011 Moderate IF CAL problem is found during production; THEN multiple flight units may be impacted due to schedule compression resulting in schedule impact. 1.Verify production processes during EM program 2.Extensive EM environment test program On Track

11 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 11 Schedule Variances  Flight ASIC manufacture (-53 days)  Packaging of CAL ASICs took ~45 days longer than programmed due to vendor work load and priorities.  AFEE Printed Circuit Board (-24 days)  Testing of prototype flight PCB and mechanical verification has taken longer than programmed.  Implementation of layout modifications add additional EMI/EMC filtering, to improve potential mechanical interference issues and to improve reliability were not programmed.  Carbon Composite Structure (-17 days)  Materials problems and over test anomalies delayed the manufacture of the 1 st flight structure. BCWS: 14,632BCWP: 14,171SV: - 462BAC: 22,103

12 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 12 Path to first flight CAL Module (FMA) Dual PIN Photodiode NRL 12/03/03 CsI Crystals Sweden 08/13/03 Crystal Detector Elements (CDE) NRL/Swales 2/09/04 Carbon Composite Structure Al base, closeouts, plastic parts LLR/Ecole Polytechnique, NRL 03/11/04 (-35) Pre Electronics Module NRL 04/12/04 (-17) ASICs SLAC, NRL 03/22/04 (-53) Other EEE parts Parts Qual/Screen NRL 03/22/04 (-53) PCB NRL 03/15/04 (-24) Analog Front End Electronics (AFEE) NRL 04/29/04 (-24) CAL Module NRL 05/24/04 (-24) Calibration Environmental Test NRL 07/22/04 (-24) Ready for Integration (RFI) 08/12/04 (-24) [BL: 07/09/04] Completion Dates (variance to baseline) Critical Path in Red

13 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 13 Path to 16th flight CAL Module (FM14) Dual PIN Photodiode NRL 06/28/04 ( 0) CsI Crystals Sweden 05/05/04 (-45) Crystal Detector Elements (CDE) NRL/Swales 08/09/04 ( 0) Carbon Composite Structure Al base, closeouts, plastic parts LLR/Ecole Polytechnique, NRL 09/20/04 (-35) Pre Electronics Module NRL 10/06/04 (-27) ASICs SLAC, NRL 03/22/04 (-53) Other EEE parts Parts Qual/Screen NRL 04/20/04 (-50) PCB NRL 03/15/04 (-44) Analog Front End Electronics (AFEE) NRL 06/26/04 (-23) CAL Module NRL 11/09/04 (-24) Calibration Environmental Test NRL 12/08/04 (-22) Ready for Integration (RFI) 01/11/05 (-22) [BL: 12/02/04] Completion Dates (variance to baseline) Critical Path in Red

14 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 14 Cost Summary 4.1.5 Baseline, November 03$22,648K Changes: CDE Manuf. Develop. Savings$ (546K) 4.1.5 Baseline, February 04$22,103K Approved Cost Changes since Rebaseline

15 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 15 Cost Variance Cumulative Cost Variance: + $640K  Mgmt, Sys Eng, R&QA: +$259K (6%)  Understaffed (60%)  Travel underrun (40%)  Crystal Detector Elements: +$27K (1%)  PreElectronics Module: +$168K (18%)  Invoicing for delivered material and outstanding commitments  Analog Electronics: +$3K (0%)  Module Assembly and Test: +$161K (9%)  Invoicing for facilities and GSE

16 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 16 Cost Liens Additional duration for Thermal Vacuum Testing  EM Test experience indicated that CAL temperature changes can not be driven as quickly as estimated in baseline: 3 days per cycle rather than baseline 2 days.  Additional TVAC operation time and supporting staff is ~$30K per TVAC. This affects 8 of the 9 TVACs.  Cost increase is partially mitigated by the removal of requirement for 12 cycles of TVAC for FMA/B. This recovers $111K.  Net cost estimate is ~ $130K. Approximately 50K of this is in FY04.

17 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 17 Next 6 months By Oct 1, 2004  Crystal Detector Elements  All CsI crystals delivered from Sweden (by August)  All CDE manufactured and tested (~1850 by Sept)  Pre Electronics Modules  17 of 18 structures delivered to NRL from IN2P3/LLR  15 of 18 PEMs completely assembled and tested.  Analog Front End Electronics  All AFEE circuit cards assembled and tested.  Module Assembly and Test  11 of 18 Modules completely assembled and in test.  6 of 18 Modules delivered to SLAC.

18 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 18 Summary  CAL design and technical issues are well in hand  EM module verified design and assembly processes. Lessons learned incorporated in flight production.  EM subjected to qualification level environmental test program. No problems.  CAL is well into flight module production  All flight hardware drawings are released.  Electronics assembly and test continue to define the critical path to the delivery of the first modules. –Flight parts availability and qualification continue to present schedule vs risk challenges.  The CAL schedule is aggressive  Delivery of 1 st two modules in August will be a significant challenge.

19 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 19 Backup Material Overview Gamma-ray Large Area Space Telescope

20 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 20 Modular Design 4 x 4 Array of Calorimeter Modules LAT GRID with 16 CAL Modules CAL Module with TEM and Power Supply mounted to base plate

21 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 21 CAL Module  Electronics boards attached to each side  Interface connectors to TEM at base of calorimeter  Outer wall is EMI shield and provides structural stiffness as well CDE: CsI Detectors + PIN diodes (both ends) Readout Electronics Carbon Cell Array Al Cell Closeout Al EMI Shield Mounting Baseplate  8 layers of 12 CsI(Tl) crystals  Crystal dimensions –27 x 20 x 326 mm  Hodoscopic stacking –alternating orthogonal layers  Dual PIN photodiode on each end of crystals  Mechanical packaging  Carbon Composite cell structure  Al base plate and side cell closeouts

22 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 22 Calorimeter Assembly Flow Crystal Detector Element (CDE) Assembly NRL PIN Diode (each end) CsI Crystal Optical Wrap Wire leads Mechanical Structure France / NRL Front-End Electronics NRL, SLAC PreElectronics Module (PEM) Assembly NRL Module Assembly and Test, NRL+collab 16 Flight modules + 2 Spare 1728 18 Bond End Cap Dual PIN Diodes (DPD) NRL CsI Crystals Sweden (KTH)

23 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 23 Environmental Test Flow

24 GLAST LAT ProjectDOE/NASA Status Review, March 31 & April 1, 2004 4.1.5 Calorimeter Subsystem 24 CAL Hardware Collaborators

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