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Nuclear Thermal Rocket by 2000: a DOE PerspectiveIt is asserted that a Nuclear Propulsion Space Transportation System is required for the Manned Mars Mission. Additionally, it is felt that a Nuclear Propulsion Space Transportation System can support a wide variety of future space missions, including lunar base implementation and support. The Rover/NERVA program demonstrated that a safe, reliable Nuclear Thermal Rocket (NTR) can be developed and operated for sufficient run times, at desirable temperatures, and with multiple restarts. The discussion is presented in viewgraph form.
Document ID
19920024091
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Howe, Steven D.
(Los Alamos National Lab. NM, United States)
Stanley, Marland
(Idaho National Engineering Lab. Idaho Falls., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Publication Information
Publication: NASA. Lyndon B. Johnson Space Center, Third SEI Technical Interchange: Proceedings
Subject Category
Nuclear And High-Energy Physics
Accession Number
92N33335
Distribution Limits
Public
Copyright
Public Use Permitted.
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