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Rocketdyne/Westinghouse nuclear thermal rocket engine modelingThe topics are presented in viewgraph form and include the following: systems approach needed for nuclear thermal rocket (NTR) design optimization; generic NTR engine power balance codes; rocketdyne nuclear thermal system code; software capabilities; steady state model; NTR engine optimizer code-logic; reactor power calculation logic; sample multi-component configuration; NTR design code output; generic NTR code at Rocketdyne; Rocketdyne NTR model; and nuclear thermal rocket modeling directions.
Document ID
19930017766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Glass, James F.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: NASA. Lewis Research Center, Nuclear Propulsion Technical Interchange Meeting, Volume 2
Subject Category
Spacecraft Propulsion And Power
Accession Number
93N26955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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