Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage /

Bibliographic Details
Main Author:	Hodge, A. J.
Corporate Author:	George C. Marshall Space Flight Center
Other Authors:	Nettles, A. T. (Alan T.), Jackson, J. R.
Format:	Government Document eBook
Language:	English
Published:	[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Series:	NASA technical paper ; 216460.
Subjects:	Compressive strength. Sandwich structures. Carbon fibers. Impact strength. Damage. Epoxy matrix composites. Laminates. Fiber composites.
Online Access:	https://purl.fdlp.gov/GPO/gpo11790

Description
Item Description:	Title from title screen (viewed on Aug. 22, 2011). "March 2011." Electronic resource.
Physical Description:	1 online resource (viii, 23 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (pages 22-23).