Research Catalog

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

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

Available online

Details

Additional authors
  1. George C. Marshall Space Flight Center.
Description
  1. 1 online resource (vii, 39 pages) : illustrations (some color).
Series statement
  1. NASA/TM ; 2011-216477
Uniform title
  1. NASA technical memorandum ; 2011-216477.
Subject
  1. Compressive strength
  2. Impact strength
  3. Honeycomb structures
  4. Launch vehicles
  5. Damage
  6. Tolerances (mechanics)
  7. Residual strength
Call number
  1. GPO Internet NAS 1.15:2011-216477
Note
  1. Title from title screen (viewed on June 22, 2012).
  2. "December 2011."
Bibliography (note)
  1. Includes bibliographical references (page 39).
Funding (note)
  1. Sponsored by National Aeronautics and Space Administration
Author
  1. Nettles, A. T. (Alan T.)
Title
  1. A damage tolerance comparison of composite hat-stiffened and honeycomb sandwich structure for launch vehicle interstage applications / A.T. Nettles.
Publisher
  1. Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Type of content
  1. text
Type of medium
  1. computer
Type of carrier
  1. online resource
Series
  1. NASA/TM ; 2011-216477
  2. NASA technical memorandum ; 2011-216477.
Bibliography
  1. Includes bibliographical references (page 39).
Funding
  1. Sponsored by National Aeronautics and Space Administration M-1326
Connect to:
  1. https://purl.fdlp.gov/GPO/gpo24323
Added author
  1. George C. Marshall Space Flight Center.
Gpo item no.
  1. 0830-D (online)
Sudoc no.
  1. NAS 1.15:2011-216477
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