Cover Image

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
Description
Item Description:Title from title screen (viewed on June 22, 2012).
"December 2011."
Electronic resource.
Physical Description:1 online resource (vii, 39 pages) : illustrations (some color).
Bibliography:Includes bibliographical references (page 39).