A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications /

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

Internet

https://purl.fdlp.gov/GPO/gpo24323

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Holdings details from Available Online
Call Number: NAS 1.15:2011-216477
 
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NAS 1.15:2011-216477 Available