Summary of a study to determine low-velocity impact damage and residual tension strength for a thick graphite/epoxy motor case
By: C.C. Poe, Jr.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 102678.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1990
Place of publication: Hampton, Va
Language: eng
Format: Microform
Number of pages: 34
Subjects: Space shuttles -- Propulsion systems -- Materials -- Impact testing.; Critical pressure.; Graphite-epoxy composites.; Impact damage.; Low speed.; Residual strength.; Rocket engine cases.
Notes: Cover title.

Shipping list no.: 90-1086-M.

"June 1990."

Includes bibliographical references (p. 17-18).

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.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

505-63-01-05.