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Engineering method to predict saturn v vehicle and launch complex environments due to rocket jet impingement final reportPrediction of forces and heat loads induced by rocket jet plume impingement on Saturn V launch vehicle and launch complex structures
Document ID
19650024273
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Africano, A. (North American Aviation, Inc. Downey, CA, United States)
Date Acquired
August 2, 2013
Publication Date
July 29, 1965
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-67017
SID-65-816
Report Number: NASA-CR-67017
Report Number: SID-65-816
Accession Number
65N33874
Funding Number(s)
CONTRACT_GRANT: NAS8-11407
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JET IMPINGEMENT
RADIATIVE HEAT TRANSFER
LAUNCH COMPLEX
CONVECTIVE HEAT TRANSFER
SATURN V LAUNCH VEHICLE

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