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Project Plan Root Cause and Risk Analysis Team 2

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Estimate Potential Failures due to Rocket Engine Defects ... Determine Potential for Post-Process defect generation by Launch vibration impact ... – PowerPoint PPT presentation

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Title: Project Plan Root Cause and Risk Analysis Team 2


1
Project PlanRoot Cause and Risk AnalysisTeam 2
  • NASA Henning Leidecker 301-286-9180
  • Boeing Gary W. Bickel 714-372-6820
  • 2/25/00

2
Team 2 Members
  • Project Leads Henning Leidecker-NASA/GSFC
  • Gary W. Bickel-Boeing/HB
  • Team Members Ray
    Prestridge-JSC
  • Pete Mueggler-BHB
  • Carol McDonald-BHOU
  • Anna Cantwell-SEA
  • David Gill-BHB
  • Jeanette Plante-GSFC
  • Dave Rothermel-BICC
  • Dale Zevotek-BICC
  • Martin Seifert-LSFT
  • David Beverly-JSC
  • Craig Mueller-AERO
  • Harold Battaglia-BHOU
  • John Canham-GSFC

3
Task 1-Root Cause Analysis
  • Identify Primary Agent for Rocket Engine
    Defect--complete HF-etch enabled by Polyimide
    void and carbon coating breech
  • Investigate Strength Reduction, 96
    Cable--complete 124/446 samples below
    Proof-Test level Polyimide void consistently
    observed
  • need to complete microphotographs on
    approximately 34 samples
  • Investigate Strength Reduction, 98-9
    Cable--partially complete
  • Determine source of Polyimide coating voids
    (fiber or other process)
  • Determine Agent (or process step) for carbon
    coating breech
  • Resolve Lingering Questions (Polyimide Canyons
    versus voids, SEM)
  • Complete Root Cause Analysis Report

4
Task 1-Root Cause status
  • Microphotos on 34 Samples-deferred
  • Strength Tests 98-9 Cable-on hold
  • Polyimide Coating Voids Source no progress
  • Coating Penetration Test Plan in development
  • SEM to sort variations in Polyimide void
    structure no progress
  • Root Cause Report Major sections left to write

5
Task 2-Risk AnalysisUS Lab and Node 1
  • Estimate Potential Failures due to Rocket Engine
    Defects--
  • Determine Effective n value--failed
    insufficient data
  • Determine alternate model for failure prediction
    of existing defects/flaws
  • Estimate pre-flight and on-orbit failures based
    on strength distribution data
  • Determine Potential for Post-Process defect
    generation by Launch vibration impact
  • Determine Potential for on-orbit defect
    generation by Ionized Radiation
  • Prepare Risk Analysis Report for US Lab and Node
    1

6
Task 2-Risk Analysis StatusUS Lab and Node 1
  • Preliminary Risk Analysis Completed
  • No consensus on Preliminary Risk Analysis based
    on worst case n-value
  • Preparing proposal to do n-value tests for ESD
    attack on uncabled fiber
  • Efforts on vibration/ionizing radiation launch
    on-orbit effects on-going

7
Task 3-Risk Analysis Reduction(Node 1 DT0
Cable, ESA Cable, all 98-9 Cable Use)
  • Determine Low Strength Distribution for 98-9
    cable--
  • Provide Preliminary Strength Tests on ESA Cable
    (representing 97 production)--
  • Determine Effect of additional Proof Testing at
    the Cable level
  • Apply results of above in estimating risk
  • Prepare Risk Analysis Reports as needed for these
    tasks

8
Task 3-Risk Analysis Reduction Status(Node 1
DT0 Cable, ESA Cable, all 98-9 Cable Use)
  • Strength Tests on 98-9 cable on hold
  • Tests on ESA cable pending receipt of cables and
    funding decisions
  • Proof Testing fixture in development

9
Team 2--Schedule
10
Team 2--Resources Required
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