Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case /

Bibliographic Details
Main Author:	Poe, C. C.
Corporate Author:	Langley Research Center
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Series:	NASA technical memorandum ; 102678.
Subjects:	Space shuttles > Propulsion systems > Materials > Impact testing. Critical pressure. Graphite-epoxy composites. Impact damage. Low speed. Residual strength. Rocket engine cases.
Online Access:	https://purl.fdlp.gov/GPO/LPS58426

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