DocumentCode
1426298
Title
Experimental solar thermionic converter for space use
Author
Oman, Henry ; Street, George
Author_Institution
Boeing Airplane Company, Seattle, Wash.
Volume
79
Issue
12
fYear
1960
Firstpage
967
Lastpage
972
Abstract
A high-pressure cesium-vapor thermionic converter appears to be a promising source of power for space vehicles. On the basis of an analysis described in this article, it was found that a converter with cathode temperatures of 3,000 to 3,500 degrees Rankine will result in low system weight and high over-all efficiency.
Keywords
Anodes; Cathodes; Generators; Mirrors; Space heating; Waste heat;
fLanguage
English
Journal_Title
Electrical Engineering
Publisher
ieee
ISSN
0095-9197
Type
jour
DOI
10.1109/EE.1960.6432959
Filename
6432959
Link To Document