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An assessment of radiative metallic thermal protection systems for space shuttleThe metallic thermal protection system technology program for the space shuttle is reviewed for the areas of environmental uncertainties, materials data base, TPS design concepts and heat-shield panel configurations, testing and evaluation of materials, panels, and complete systems.
Document ID
19720023226
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stein, B. A. (NASA Langley Research Center Hampton, VA, United States)
Bohon, H. L. (NASA Langley Research Center Hampton, VA, United States)
Rummler, D. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publication: NASA Space Shuttle Technol. Conf.
Subject Category
Thermodynamics And Combustion
Accession Number
72N30876
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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