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Solid Propellant Grain Structural Integrity AnalysisThe structural properties of solid propellant rocket grains were studied to determine the propellant resistance to stresses. Grain geometry, thermal properties, mechanical properties, and failure modes are discussed along with design criteria and recommended practices.
Document ID
19740011276
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 3, 2013
Publication Date
June 1, 1973
Subject Category
Propellants
Report/Patent Number
NASA-SP-8073
Accession Number
74N19389
Funding Number(s)
CONTRACT_GRANT: NAS3-12046
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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