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Entry systems technology assessmentThe objectives are: (1) to establish aerothermal environments for hypersonic aerospace vehicles; (2) to develop thermostructural design concepts; (3) to obtain optimum thermostructural designs by performing trade studies; and (4) to identify areas for further development.
Document ID
19930012929
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gay, Archie
(General Dynamics Corp. San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Publication Information
Publication: NASA. Langley Research Center, Space Transportation Materials and Structures Technology Workshop. Volume 2: Proceedings
Subject Category
Space Transportation
Accession Number
93N22118
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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