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Thermal strain analysis of advanced manned spacecraft heat shields second quarterly status report, 1 dec. 1963 - 29 feb. 1964Equations on thick and thin walled shell theories for thermal stress analysis of manned spacecraft heat shields
Document ID
19650014059
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cox, W. T. (Aerojet-General Corp. Azusa, CA, United States)
Date Acquired
August 2, 2013
Publication Date
March 1, 1964
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-62661
Q-5654-01-2
Accession Number
65N23660
Funding Number(s)
CONTRACT_GRANT: NAS9-1986
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THICK WALL
THERMAL STRESS
HEAT SHIELD
THIN WALLED SHELL

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