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NTP system simulation and detailed nuclear engine modelingThe topics are presented in viewgraph form and include the following: nuclear thermal propulsion (NTP) & detailed nuclear engine modeling; modeling and engineering simulation of nuclear thermal rocket systems; nuclear thermal rocket simulation system; INSPI-NTVR core axial flow profiles; INSPI-NTRV core axial flow profiles; specific impulse vs. chamber pressure; turbine pressure ratio vs. chamber pressure; NERVA core axial flow profiles; P&W XNR2000 core axial flow profiles; pump pressure rise vs. chamber pressure; streamline of jet-induced flow in cylindrical chamber; flow pattern of a jet-induced flow in a chamber; and radiative heat transfer models.
Document ID
19930017768
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anghaie, Samim
(Florida Univ. Gainesville, FL, 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
93N26957
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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