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Engineering Method to Predict Saturn V Vehicle and Launch Complex Environments Due to Rocket Jet Impingement Quarterly Progress Report No. 2, 1 Oct. - 31 Dec. 1964Prediction of Saturn V vehicle and launch complex force and heat load environments due to rocket jet impingement - impact pressure and radiation and convective heat transfer
Document ID
19660020050
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Africano, A. (North American Aviation, Inc. Downey, CA, United States)
Date Acquired
August 3, 2013
Publication Date
January 15, 1965
Subject Category
Facilities, Research, And Support
Report/Patent Number
SID-65-44
NASA-CR-57601
Report Number: SID-65-44
Report Number: NASA-CR-57601
Accession Number
66N29340
Funding Number(s)
CONTRACT_GRANT: NAS8-11407
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JET IMPINGEMENT
IMPACT PRESSURE
PLUME
SATURN V LAUNCH VEHICLE
CONVECTIVE HEAT TRANSFER

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