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Convective and radiative heat transfer to an ablating body.Convective and radiative heat transfer to entry vehicles protected by ablation heat shield, obtaining absorption coefficients
Document ID
19670047312
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoshizaki, H.
Lasher, L. E.
Date Acquired
August 3, 2013
Publication Date
April 1, 1967
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 67-327
Report Number: AIAA PAPER 67-327
Accession Number
67A26041
Funding Number(s)
CONTRACT_GRANT: NAS7-386
Distribution Limits
Public
Copyright
Other
Keywords
ABSORPTION COEFFICIENT
REENTRY PHYSICS
HEAT SHIELD
ABLATING NOSE CONE
HEAT TRANSFER

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