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Thermoelectric and Thermionic Conversion TechnologyApplied research and technology efforts in thermoelectric and thermionic programs were recommended that will enable space power systems for the nation's future space missions. Specifically it was argued that the effort in thermoelectric materials technology be broadened with the objective of obtaining a material with a Figure of Merit greater than 1.0 x 10(-3)/K for hot junction temperatures of 1100 to 1500 K. The recommended effort in thermionics is to pursue technology programs that will result in an understanding and lifetime prediction methodologies for fuel-emitter and sheath-insulator behavior as a function of operating time and temperature. Also it is recommended that an effort be initiated that combines the thermoelectric, thermionic and power electronic technologies into a program to develop the technology for high temperature, high radiation resistant, and high current electronic switches.
Document ID
19850005596
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mondt, J. F.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ambrus, J. H.
(NASA Headquarters Washington, DC United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Space Power
Subject Category
Spacecraft Propulsion And Power
Accession Number
85N13905
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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