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Effect of shock precursor absorption on superorbital entry heating.Quantitative determination of reentry shock precursor absorption level and effect on surface radiation heating, calculating radiative flux from shock layer enthalpy distribution
Document ID
19690034539
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lasher, L. E.
Wilson, K. H.
Date Acquired
August 5, 2013
Publication Date
December 1, 1968
Subject Category
Thermodynamics And Combustion
Accession Number
69A12528
Funding Number(s)
CONTRACT_GRANT: NAS7-509
Distribution Limits
Public
Copyright
Other

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