Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage
By: A.J. Hodge, A.T. Nettles, and J.R. Jackson
Contributors: Nettles, A. T. (Alan T.); Jackson, J. R.; George C. Marshall Space Flight Center
Series: NASA/TP -- 2011-216460; NASA technical paper -- 216460.
Publisher: National Aeronautics and Space Administration, Marshall Space Flight Center
Published: 2011
Place of publication: Huntsville], Ala
Language: eng
Format: [electronic resource] /
Number of pages: 23
Subjects: Compressive strength; Sandwich structures; Carbon fibers; Impact strength; Damage; Epoxy matrix composites; Laminates; Fiber composites
Notes: Title from title screen (viewed on Aug. 22, 2011).

"March 2011."

Includes bibliographical references (p. 22-23).