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Digital codes for design and evaluation of convectively cooled rocket nozzle with application to nuclear-type rocketComputer programs for design of convectively cooled rocket nozzle with application to nuclear type rocket
Document ID
19670004777
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Derderian, G. (NASA Lewis Research Center Cleveland, OH, United States)
Duscha, R. A. (NASA Lewis Research Center Cleveland, OH, United States)
Rohde, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-TN-D-3798
Report Number: NASA-TN-D-3798
Accession Number
67N14106
Funding Number(s)
CONTRACT_GRANT: 122-29-07-07-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPUTER PROGRAM
COOLANT
ROCKET NOZZLE

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