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Structures for Reentry HeatingThe basic structural approaches for dealing with reentry heating of manned vehicles are summarized. The weight and development status of both radiative and ablative shields are given and the application of these shields to various vehicles is indicated.
Document ID
19980227176
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Anderson, Roger A. (NASA Langley Research Center Hampton, VA United States)
Swann, Robert T. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1960
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-313
Report Number: NASA-TM-X-313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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