Research Catalog

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

Title
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.
Author
Nettles, A. T. (Alan T.)
Publication
Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]

Available Online

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

Details

Additional Authors
George C. Marshall Space Flight Center.
Description
1 online resource (vii, 39 pages) : illustrations (some color).
Series Statement
NASA/TM ; 2011-216477
Uniform Title
NASA technical memorandum ; 2011-216477.
Subject
  • Compressive strength
  • Impact strength
  • Honeycomb structures
  • Launch vehicles
  • Damage
  • Tolerances (mechanics)
  • Residual strength
Note
  • Title from title screen (viewed on June 22, 2012).
  • "December 2011."
Bibliography (note)
  • Includes bibliographical references (page 39).
Funding (note)
  • Sponsored by National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.15:2011-216477
OCLC
marcive796083014
Author
Nettles, A. T. (Alan T.)
Title
A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.
Publisher
Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 2011-216477
NASA technical memorandum ; 2011-216477.
Bibliography
Includes bibliographical references (page 39).
Funding
Sponsored by National Aeronautics and Space Administration M-1326
Connect to:
https://purl.fdlp.gov/GPO/gpo24323
Added Author
George C. Marshall Space Flight Center.
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:2011-216477
View in Legacy Catalog