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Thermo-structural failure limits for the spacecraft component for an Apollo 1B launch environmentComputer programs for analyzing aerodynamic heating effects on structural failure of Saturn 1 launch vehicle components
Document ID
19700025291
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Faust, C. D. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Gillies, A. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Posgay, R. G. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 2, 2013
Publication Date
April 25, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-64370
TRW-05952-H177-R0-00
MSC-67-FM-50
Report Number: NASA-TM-X-64370
Report Number: TRW-05952-H177-R0-00
Report Number: MSC-67-FM-50
Accession Number
70N34607
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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