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A Heat Transfer Investigation of Ejector Systems with 90 Deg Turns. NERVA ProgramHeat transfer characteristics of ejector systems for turning rocket exhaust gases through 90 deg
Document ID
19680007817
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mandell, B. (Aerojet-General Corp. Azusa, CA, United States)
Mc Farland, B. L. (Aerojet-General Corp. Azusa, CA, United States)
Nelson, R. E. (Aerojet-General Corp. Azusa, CA, United States)
Patmor, G. O. (Aerojet-General Corp. Azusa, CA, United States)
Date Acquired
August 4, 2013
Publication Date
November 1, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
TID-23652
NASA-CR-91274
RN-DR-0038
Report Number: TID-23652
Report Number: NASA-CR-91274
Report Number: RN-DR-0038
Accession Number
68N17286
Funding Number(s)
CONTRACT_GRANT: SNP-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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