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Convective and radiative heat transfer to an ablating body, part I Final reportConvective and radiative heat transfer to entry vehicles with ablative heat shield
Document ID
19670007238
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hoshizaki, A. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Lasher, L. E. (Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
August 3, 2013
Publication Date
July 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-73060
LMSC-4-06-66-12
Report Number: NASA-CR-73060
Report Number: LMSC-4-06-66-12
Accession Number
67N16567
Funding Number(s)
CONTRACT_GRANT: NAS7-386
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RADIATIVE HEAT TRANSFER
HEAT SHIELD
CONVECTIVE HEAT TRANSFER
ATMOSPHERIC ENTRY
ABLATION

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