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Thermionic technology infrastructure for space powerAn assessment is made of the potential effectiveness, designs, and technological difficulties involved in the construction of space nuclear reactors coupled to thermionic energy converters (TEC). The TECs can be positioned either inside or outside of the reactor core. The out-of-core design lowers the reactor shielding requirements, as well as removing the need for mechanically pumped coolant for the reactor. R&D is still needed for the heat pipes for the reactor and the collectors, electrical insulation, and to reduce the potential losses in the interelectrode space. A cylindrical converter for the out-of-core configuration consists of a tungsten emitter heated by a tungsten-lithium heat pipe. The collector is a layer of tungsten oxide deposited on a Nb-1%Zr alloy, and has been tested at emitter temperatures of 1300-1850 K and a collector temperature range of 700-850 K. A design of a superheated thermionic converter is described, noting that a prototype has been operated at 1730 K for 12,000 hr.
Document ID
19830046080
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Huffman, F.
(Thermo Electron Corp. Waltham, MA, United States)
Reagan, P.
(Thermo Electron Corp. Waltham, MA, United States)
Miskolczy, G.
(Thermo Electron Corp. Waltham, MA, United States)
Merrill, O.
(Thermo Electron Corp. Waltham, MA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: IECEC ''82; Seventeenth Intersociety Energy Conversion Engineering Conference
Location: Los Angeles, CA
Start Date: August 8, 1982
End Date: August 12, 1982
Accession Number
83A27298
Funding Number(s)
CONTRACT_GRANT: JPL-955009
CONTRACT_GRANT: DE-AC02-76ET-11291
CONTRACT_GRANT: DE-AC02-81CS-90215
CONTRACT_GRANT: NAS3-20270
Distribution Limits
Public
Copyright
Other

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