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.
- Published by
- Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
- Author
- Nettles, A. T. (Alan T.)
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
- Call number
- GPO Internet NAS 1.15:2011-216477
- 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
- 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
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