The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
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Author
Contributions
- Hodge, A. J. - Contributor
- Jackson, J. R. - Contributor
- George C. Marshall Space Flight Center - Contributor
Publication
2011 - National Aeronautics and Space Administration, Marshall Space Flight Center, Huntsville], Ala, Alabama
Language
English
Word Count
5,750 words, Guess
Page Count
23 pages
Physical Format
Electronic resource
Identifiers
- OCLC Control Number744420941
- Open LibraryOL43927159M
Subjects
Series Statement
- NASA/TP -- 2011-216457
- NASA technical paper -- 216457.
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