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The effects of foam thermal protection system on the damage tolerance characteristics of composite sandwich structures for launch vehicles
2011, National Aeronautics and Space Administration, Marshall Space Flight Center
electronic resource /
in English
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Edition Notes
Title from title screen (viewed on Aug. 2, 2011).
"February 2011."
Includes bibliographical references (p. 22-23).
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- Created December 13, 2022
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December 13, 2022 | Created by MARC Bot | Imported from harvard_bibliographic_metadata record |