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EFFECTS OF SHAPE ON TOTAL RADIATIVE AND CONVECTIVE HEAT INPUTS AT HYPERBOLIC ENTRY SPEEDSBody shape, entry angle and velocity, and weight to area ratio effects on radiative heating rates and total heat input of vehicles entering the earths atmosphere at hyperbolic velocities
Document ID
19630027339
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bobbitt, P. J.
Date Acquired
August 1, 2013
Publication Date
January 1, 1963
Subject Category
Geophysics
Accession Number
63A23398
Distribution Limits
Public
Copyright
Other
Keywords
RADIATIVE HEAT TRANSFER
ATMOSPHERIC ENTRY
HEAT TRANSFER
SPACECRAFT REENTRY

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