A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage 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, [2011]
Series:	NASA technical memorandum ; 2011-216477.
Subjects:	Compressive strength. Impact strength. Honeycomb structures. Launch vehicles. Damage. Tolerances (mechanics) Residual strength.
Online Access:	https://purl.fdlp.gov/GPO/gpo24323