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Hot/wet open hole compression strength of carbon/epoxy laminates for launch vehicle applications /

Bibliographic Details
Main Author: Nettles, A. T. (Alan T.)
Corporate Author: George C. Marshall Space Flight Center
Format: Government Document eBook
Language:English
Published: [Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2009]
Series:NASA technical memorandum ; 215900.
Subjects:
Epoxy matrix composites.
Temperature effects.
Compressive strength.
Launch vehicles.
Safety factors.
Online Access:https://purl.fdlp.gov/GPO/gpo11889
Description
Item Description:Title from title screen (viewed on Aug. 25, 2011).
"June 2009."
Electronic resource.
Physical Description:1 online resource (vii, 23 pages) : illustrations (some color).
Bibliography:Includes bibliographical references (page 23).