DocumentCode
1230076
Title
SNAP-8 Electrical System
Author
Nice, A.W. ; Bradley, S.L.
Author_Institution
National Aeronautics and Space Administration Lewis Research Center
Volume
2
Issue
2
fYear
1964
fDate
4/1/1964 12:00:00 AM
Firstpage
867
Lastpage
873
Abstract
This paper presents a brief description of the SNAP-8 electrical-system design changes and provides a broad perspective of the overall system changes incorporated early in 1963. These modifications made feasible a modular approach to component and subsystem development, provided greater system development flexibility, and permitted the application of much presently available electrical technology. The rotating speed was changed from 20,000 to 12,000 revolutions per minute (rpm) resulting in a change of system frequency from 1,000 to 400 cycles per second (cps). The alternator and the regulator were removed from the high-temperature and mercury-vapor environment. The mercury lubrication and cooling concept was replaced with organic-fluid lubrication and a low-temperature cooling loop was added to the system. Significant development problems still exist, however. There remains the requirement for 10,000-hours minimum life in the space and nuclear environment, coupled with extremely high reliability objectives.
Keywords
Alternators; Coolants; Cooling; Electromagnetic heating; Frequency; Heat pumps; Heat transfer; Inductors; Lubrication; Space heating;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1964.4319677
Filename
4319677
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