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solid propulsion integrity program (spip) for verifiable enhanced solid rocket motor reliabilityTo increase the success rate of U.S. built Rocket Motors (SRM), the approach taken is: (1) set common reliability goals for nozzles, cases, bondline, propellant, and insulation; (2) build a common engineering data base to support standard industry-wide reliability assessment models; (3) structure or enhance existing industry/government/user term to develop the tools, methods needed, and the data to support them; and (4) areas where unreliabilities are found must be improved.
Document ID
19930012915
Document Type
Conference Paper
Authors
Butler, Barry L.
(Science Applications International Corp. San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Space Transportation Materials and Structures Technology Workshop. Volume 2: Proceedings
Subject Category
SPACE TRANSPORTATION
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930012892Analytic PrimarySpace Transportation Materials and Structures Technology Workshop