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