Design Integration and Analysis

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Presentation transcript:

Design Integration and Analysis LAT Monthly Status Review 30 June 2005 Design Integration and Analysis Martin Nordby John Ku Jack Goodman

Design Support Status Flight/fly-away hardware designs (all remaining hardware listed) Accelerometer mount brackets: drawings released Temp Sensor Brackets : drawings released MLI blankets: detailed drawings in-work (ECD: 7/15) External fly-away instrumentation cables: in-work TKR accel mount bracket: in-work Assembly drawings LAT-DS-05210-01 Cable Installation Kit Put in release cycle this month LAT-DS-02561-01 LAT Tower and Electronics Assembly Released this month LAT-DS-06721 External Cable Installation Kit New assembly-level drawing to capture all external cabling details In work: updating external cable routing LAT-DS-02563-01 LAT Instrument Assembly Modeling complete, drafting awaits completion of External Cable Install Kit drawing Interface Drawings LAT-DS-00309-04 ACD-LAT IDD

Integration Planning LAT Integration Sequence (LAT-MD-00676-03) Convened review committee to revise this with current thinking for post-tower integration and test work Configuration drawings LAT Instrument Configuration Assembly Drawing on hold pending completion of ACD lift fixture—waiting design support (need date is Oct) Integration MGSE (all remaining integration MGSE listed) LAT auxiliary cooling Chill Bar assemblies: completed this month Parts, assembly, procedures: completed this month Chiller: delivered and commissioned this month System is in-use on LAT ACD Lift Fixture Design still on the drawing board

Environmental Test Planning LAT Environmental Test Sequence Release held up to resolve LAT functional testing issues In release cycle again—expect release any day Dynamics Test Plan In second review at GSFC/Swales Instrumentation fully specified and purchased Release is imminent EMI/EMC Test Plan Final draft ECD is this week Instrumentation fully specified and available at NRL Still working on updating test parameter requirements with Fred Blanchette T-Vac Test Plan Held follow-on PDR on thermal test plans this month Finalized LAT environmental control plans: cal-rod heater cages and passively cooled sink plates Test Plan has been revised, including updated instrumentation list and test sequence Instrumentation 95% specified: completion waiting on completion of STE design

Environmental Test MGSE/STE Transport Container Source Control Drawings and Statement of Work: completed this month RFP is due back this week—then we will place the order ASAP Test Interface Plate Parts drawings completed this month Parts: out for fabrication Assembly drawing: completed this month; considerable work in spec’ing out Spectrum’s flexure interfaces to the Grid and our test plate (this is not well-documented at Spectrum) Test Stand Conceptual design in structural analysis now—will likely need minor mod’s Specifying hardware now Extension Beam design just started This is critical path for MGSE, since Pathfinder program needs this in mid-October T-Vac Sink Plates and Cal-Rod Cage Conceptual design completed this month: uses existing NRL power supplies with all-passive cooling Detailed thermal and electrical design started Mechanical design to be started in early July Spreader Bars Design started Awaiting structural analysis

Structural Analysis: Accomplishments LAT System Level Continued LAT Static test plan development Continued LAT Environmental test planning Completed draft of Test Plan Completed analysis of TIP (Test Interface Plate) Completed first look at Test Stand (design/analysis iteration stage) Verified ACD Instrumentation set Researched overall allowable cable lengths (s.b. < 100 ft total from accel to computer) Completed LAT10.09 FEA Model Incorporated new ACD model Updated Grid model for changes since delta-CDR Other minor model clean-up LAT Subsystem Level MGSE ACD Lift frame analysis complete Evaluated margins of safety for Observatory lift by the LAT TKR Subsystem Continued support of TKR testing at Alenia Continued to review all TKR vibration test reports from INFN/Bari Mechanical Subsystem Supported radiator test readiness reviews EBOX Subsystem Completed Cable Tray analysis T T I T I T I T T T D = Flight Design = Integration Prep = LAT/SS Test Prep D I T

Structural Analysis: Near-term Milestones and Status LAT System Level LAT Static Testing Visit NTS on Wednesday 6/29/05 Review test philosophy and load cases with mechanical branch on Thursday 6/30/05 LAT Dynamics Testing Define flexure strain gauge locations to facilitate load input calculation – ECD = 7/22/05 Update LAT vibration test predictions – ECD = 9/1/05 Continue planning with I&T and NRL for LAT environmental testing – ECD=ongoing through test MGSE for I&T: augment MGSE analysis with additional I&T needs, as required LAT Test Stand MGSE and associated handling procedures and test environments – ECD = 7/8/05 LAT Subsystem Level TKR Subsystem Continue to support testing in Italy (help from GSFC is lined up) Mechanical Subsystem Get Instron back online in order to proof test flexures – ECD = 7/14/05 Proof Test Spectrum provided flexures TRR – ECD = 7/15/05 Shear plate qualification test report – ECD = 7/15/05 Grid Static Load Test procedures, STE, TRR – ECD = 8/5/05 Support radiator acoustic and sine vibe tests (over the next month) – ECD 7/29/05 EBOX Subsystem Complete TEM/TPS Vibration test report Support GASU and PDU Protoflight tests T I T I T T I T D = Flight Design = Integration Prep = LAT/SS Test Prep I T

Thermal Engineering Activities – Completed Design Engineering and Support Supported test design to measure thermal conductance of HP bonded triple joint. Finalized MLI blanket outer layer design (0.003” Kapton) between SLAC, LM and SAI Supported design and installation of Grid heat exchangers for room temperature cooling LAT Level Thermal Analysis and Tests LAT TVAC S/C bus simulation, ACD and radiator sink plates thermal design finished – heater circuit design will start this week LAT TVAC Test Plan document finished Subsystem Support and Oversight Supported ACD request to eliminate thermal balance testing LAT Thermal Control System Lockheed Thermal Control System Hardware X-LAT Plate Protoqual Test completed Ultrasonic tests of heat pipe bond joints before and after 12 thermal cycles Minor/negligible de-bonds found, MRB planned for discussion of results Radiator Protoqual Test Plan finished

Thermal Engineering Activities – Current Design Engineering and Support Environmental Specification – change Tracker Acceptance Level Tests (35oC to 45oC) Reviewing electrical grounding scheme for MLI blankets with NASA/GSFC LAT Level Thermal Analysis and Tests Thermal math model for LAT TVAC Test almost complete; LAT support stand GSE will be incorporated into model when time becomes available - after radiator/TCS protoqual tests TVAC Test Procedures document started Subsystem Support and Oversight Continued support for TKR TVAC Acceptance Testing; TKR 6 and 7 early July? LAT Thermal Control System Test setup to measure thermal conductance of VCHP triple joint using mold release material in progress; test scheduled to start 7/1 Lockheed Thermal Control System Hardware Radiator/TCS Protoqual Test planned for July 2005 TVAC Test Procedures in progress MGSE design finished; fabrication/assembly to begin early July EGSE to run TCS software/hardware to be finished and delivered to LM early/mid-July

Thermal Engineering Activities - Planned Design Engineering and Support Complete detailed MLI design Review, then fabricate MLI blankets; two sets, one set for tests and other for flight LAT Level Thermal Analysis and Tests Thermal Math Model, Ver. 6.1, reduced node Thermal Math Model, Ver. 6.2, LAT TVAC test configuration Document analysis of LAT transition from Survival to Operating Mode 200 Node Launch Vehicle Thermal Math Model Subsystem Support and Oversight Support TVAC tests of all eboxes Support TVAC tests of TKR 6 -16 Support ACD TVAC test LAT Thermal Control System Preliminary verification during LM Radiator Protoqual Tests TCS verified in LAT TVAC tests at NRL Lockheed Thermal Control System Hardware Ship X-LAT Plate to SLAC