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Nuclear Thermal Propulsion: Past, Present, and a Look AheadNTR: High thrust high specific impulse (2 x LOXLH2 chemical) engine uses high power density fission reactor with enriched uranium fuel as thermal power source. Reactor heat is removed using H2 propellant which is then exhausted to produce thrust. Conventional chemical engine LH2 tanks, turbo pumps, regenerative nozzles and radiation-cooled shirt extensions used -- NTR is next evolutionary step in high performance liquid rocket engines.
Document ID
20150004422
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Borowski, Stanley K.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
April 3, 2015
Publication Date
October 29, 2014
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GRC-E-DAA-TN18534
Report Number: GRC-E-DAA-TN18534
Meeting Information
Meeting: Wernher von Braun Memorial Symposium
Location: Huntsville, AL
Country: United States
Start Date: October 27, 2014
End Date: October 29, 2014
Sponsors: American Astronautical Society
Funding Number(s)
WBS: WBS 279585.01.99.99.99.99.22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Nuclear rocket engines
Lunar flyby mission
Spacecraft design
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