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EFFECTS OF NONEQUILIBRIUM FLOWS ON AERODYNAMIC HEATING DURING ENTRY INTO THE EARTH'S ATMOSPHERE FROM PARABOLIC ORBITSShallow angle flight paths of high speed reentry vehicles necessitates analysis of the factors controlling the rate of convective heating and the effect of nonequilibrium flow
Document ID
19630026626
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chung, P. M.
Goodwin, G.
Date Acquired
August 1, 2013
Publication Date
January 1, 1962
Subject Category
Space Radiation
Accession Number
63A22685
Distribution Limits
Public
Copyright
Other
Keywords
CONVECTIVE HEAT TRANSFER
SPACECRAFT REENTRY
REENTRY EFFECT
AERODYNAMIC HEATING

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