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

Description
Item Description:	Cover title. Shipping list number: 90-1086-M. "June 1990." Microform.
Physical Description:	34 pages : illustrations Also available via Internet from the NASA Technical Report Server web site. Address as of 3/3/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900016058%5F1990016058.pdf; current access available via PURL.
Bibliography:	Includes bibliographical references (pages 17-18).