The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles /

Bibliographic Details
Main Author:	Nettles, A. T. (Alan T.)
Corporate Author:	George C. Marshall Space Flight Center
Other Authors:	Hodge, A. J., 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 ; 216457.
Subjects:	Damage assessment. Launch vehicles. Thermal protection. Sandwich structures. Residual strength. Ares 1 launch vehicle. Composite structures. Composite materials. Impact damage.
Online Access:	https://purl.fdlp.gov/GPO/gpo10728

Description
Item Description:	Title from title screen (viewed on Aug. 2, 2011). "February 2011." Electronic resource.
Physical Description:	1 online resource (vii, 23 pages) : illustrations
Bibliography:	Includes bibliographical references (pages 22-23).