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Heat and mass-transfer characteristics of an axial-flow liquid-core nuclear rocket employing radiation heat transferHeat and mass transfer characteristics of axial- flow liquid-core nuclear rocket engine employing radiation heat transfer
Document ID
19670024548
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Donovan, L. F. (NASA Lewis Research Center Cleveland, OH, United States)
Kascak, A. F. (NASA Lewis Research Center Cleveland, OH, United States)
Ragsdale, R. G. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1967
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TN-D-4127
Report Number: NASA-TN-D-4127
Accession Number
67N33877
Funding Number(s)
CONTRACT_GRANT: 122-28-02-18-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MASS TRANSFER
RADIATIVE HEAT TRANSFER
NUCLEAR ENGINE FOR ROCKET VEHICLE /NERVA/

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