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Comparison of entry-body shapes for total equilibrium radiation under Mars entry conditionsTotal equilibrium shock layer radiative heat transfer for entry body configurations in simulated Mars atmosphere
Document ID
19670002780
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stumpf, H. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
August 31, 1966
Subject Category
Structural Mechanics
Accession Number
67N12109
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHOCK LAYER
SPACECRAFT CONFIGURATION
MARS ATMOSPHERE
EQUILIBRIUM
RADIATIVE HEAT TRANSFER
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