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Analytical study of moderator wall cooling of gaseous nuclear rocket enginesModerator wall cooling of high thrust cavity type gaseous nuclear rocket engines
Document ID
19650011275
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mc Lafferty, G. H. (United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
August 2, 2013
Publication Date
April 1, 1965
Subject Category
Nuclear Engineering
Report/Patent Number
NASA-CR-214
Report Number: NASA-CR-214
Accession Number
65N20876
Funding Number(s)
CONTRACT_GRANT: NASW-847
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SURFACE COOLING
NUCLEAR ROCKET
MODERATOR
ROCKET ENGINE

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