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SNTP propellant management systemViewgraphs on the following are presented: (1) space nuclear thermal propulsion (SNTP) propellant management system; (2) SNTP cycle selection; (3) NTP system components unique design constraints; (4) bleed cycle unique design requirement for turbopump; (5) bleed cycle turbopump; (6) SNTP carbon-carbon turbine wheel; and (7) turbine development program.
Document ID
19930017748
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tippetts, Tom (Allied-Signal Corp. Morristown, NJ, 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 1
Subject Category
Spacecraft Propulsion And Power
Accession Number
93N26937
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930017719Collected WorksNuclear Propulsion Technical Interchange Meeting, volume 119930017719Collected WorksNuclear Propulsion Technical Interchange Meeting, volume 1
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