Relevance of impacter shape to nonvisible damage and residual tensile strength of a thick graphite/epoxy laminate
By: C.C. Poe, Jr.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 102599.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1990
Place of publication: Hampton, Va
Language: eng
Format: Microform
Number of pages: 48
Subjects: Space shuttles -- Propulsion systems -- Materials -- Impact testing.; Damage assessment.; Graphite-epoxy composites.; Impact damage.; Laminates.; Residual strength.; Tensile strength.
Notes: Cover title.

Shipping list no.: 90-0860-M.

"January 1990."

Includes bibliographical references (p. 21-22).

Also available via Internet from the NASA Technical Report Server web site. Address as of 3/2/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011806%5F1990011806.pdf; current access available via PURL.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative ; 11 x 15 cm.

505-63-01-05.