DocumentCode
1229832
Title
Radioisotope Fueled Thermionic Space Power Systems
Author
Gingrich, J.E.
Author_Institution
Atomics International a Division of North American Aviation, Inc. Canoga Park, California
Volume
2
Issue
2
fYear
1964
fDate
4/1/1964 12:00:00 AM
Firstpage
669
Lastpage
674
Abstract
In order to understand better the interacting variables of the radioisotope fuel properties and the operating conditions for thermionic converters a parametric study was made of the heat source and system variables. Fuel bodies and converters of various geometric shapes were studied with planar, cylindrical, and spherical emitter surfaces. The problems relating to radiological safety and shielding of the isotope fuel were reviewed. Cost and availability information was obtained for some of the more promising isotope fuels. The results of this study show that there is no completely ideal radioisotope heat source for thermionic space power systems and that the more promising isotope fuels will require important compromises between system specific weight, radiation shielding, system efficiency, and isotope containment to produce usable space power systems.
Keywords
Fuels; Isotopes; Photovoltaic cells; Plasma temperature; Power engineering and energy; Power systems; Radioactive materials; Space heating; Sun; Thermoelectric devices;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1964.4319652
Filename
4319652
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