Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage /

Comparison of open-hole compression strength and compression after impact strength on carbon fiber/epoxy laminates for the Ares I composite interstage /

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Bibliographic Details
Author / Creator:Hodge, A. J.
Imprint:[Huntsville], Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
Description:1 online resource (viii, 23 p.) : ill. (some col.).
Language:English
Series:NASA/TP ; 2011-216460
NASA technical paper ; 216460.
Subject:
Carbon fibers.
Fibrous composites.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8459580
Hidden Bibliographic Details
Other authors / contributors:Nettles, A. T. (Alan T.)
Jackson, J. R.
George C. Marshall Space Flight Center.
Notes:Title from title screen (viewed on Aug. 22, 2011).
"March 2011."
Includes bibliographical references (p. 22-23).
GPO item no.:0830-H-15 (online)
Govt.docs classification:NAS 1.60:2011-216460

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