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Failure Engineering Study and Accelerated Stress Test Results for the Mars Global Surveyor Spacecraft's Power Shunt AssembliesDue to a post launch failure of a part a new plan for the Mars Global Surveyor was developed. This new plan involved the addition of many deep thermal cycles to the Power Shunt Assemblies (PSA's). This new plan exceeds the previous acceptance cold level, and fatigue life on packaging design. This presentation reviews the experiments that were used to test the capabilities of the PSA to function in the new situation. It also reviews the analyses preformed to verify the most likely failure mechanism, and the likelihood that these failures would impact the new mission requirements.
Document ID
20000070483
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
Authors
Gibbel, Mark
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Larson, Tim
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Quality Assurance And Reliability
Meeting Information
Meeting: Interpack 1999
Location: Pasadena, CA
Country: United States
Start Date: June 13, 1999
End Date: June 18, 1999
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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