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Aerodynamic heating.Aerodynamic heating of spacecraft during reentry, investigating characteristics for low density rarefied flow and high density continuum flow regimes
Document ID
19650029832
Acquisition Source
Legacy CDMS
Document Type
Book Chapter
Authors
Ried, R. C., Jr.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Aerodynamics
Accession Number
65A12536
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT REENTRY
REENTRY EFFECT
CONVECTIVE HEAT TRANSFER
RADIATIVE HEAT TRANSFER
AERODYNAMIC HEATING

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