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RTGs - The powering of UlyssesThe radio-isotope thermoelectric generator (RTG) for Ulysses' electronic supply is described noting that lack of sufficient sunlight renders usual solar cell power generation ineffective due to increased distance from sun. The history of the RTG in the U.S.A. is reviewed citing the first RTG launch in 1961 with an electrical output of 2.7 W and the improved Ulysses RTG, which provides 285 W at mission beginning and 250 W at mission end. The RTG concept is discussed including the most recent RTG technology developed by the DOE, the General Purpose Heat Source RTG (GPHS-RTG). The system relies upon heat generated by radioactive decay using radioactive plutonium-238, which is converted directly to energy using the Seebeck method.
Document ID
19900065085
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mastal, E. F.
(DOE, Office of Nuclear Energy, Washington DC, United States)
Campbell, R. W.
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
August 1, 1990
Publication Information
Publication: ESA Bulletin
Issue: 63, A
ISSN: 0376-4265
Subject Category
Spacecraft Propulsion And Power
Accession Number
90A52140
Distribution Limits
Public
Copyright
Other

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