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Thermionic reactor electric propulsion system requirements.Results of mission analysis, system analysis and mission engineering studies to find a single nuclear electric propulsion (NEP) system which would be applicable for a broad range of unmanned outer planet missions. The NEP system studied uses an in-core nuclear thermionic reactor as the electric power source and mercury bombardment ion engines for propulsion. Many requirements, which are imposed on the NEP system by the mission, were determined from the studies in the process of trying to find a single NEP system for many missions. It is concluded that a single thermionic reactor NEP system could be useful for a broad range of unmanned outer planet missions. The thermionic reactor NEP system should have a power level in the range from 70 to 120 kWe, a system specific weight of approximately 30 kg/kWe, and a full power output capability of 20,000 hr.
Document ID
19720052501
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mondt, J. F.
Sawyer, C. D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Schaupp, R. W.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Propulsion Systems
Meeting Information
Meeting: International Atomic Energy Agency and European Nuclear Energy Agency, International Conference on Thermionic Electrical Power Generation
Location: Juelich
Start Date: June 5, 1972
End Date: June 9, 1972
Sponsors: International Atomic Energy Agency, European Nuclear Energy Agency
Accession Number
72A36167
Distribution Limits
Public
Copyright
Other

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