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Coupled convective and radiative heating to superorbital entry vehiclesCoupled convective and radiative heating of suborbital entry vehicles
Document ID
19660007089
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Buckingham, A. C. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Hoshizaki, H. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
October 1, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
LMSC-4-43-65-1
NASA-CR-69869
Report Number: LMSC-4-43-65-1
Report Number: NASA-CR-69869
Accession Number
66N16378
Funding Number(s)
CONTRACT_GRANT: NAS7-295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUBORBITAL FLIGHT
REENTRY VEHICLE
RADIANT HEATING
CONVECTIVE HEAT TRANSFER

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