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