DocumentCode
932752
Title
HV design of vacuum-insulated power supplies for space applications
Author
Gollor, M. ; Rogalla, K.
Author_Institution
Dornier GmbH, Friedrichshafen, Germany
Volume
28
Issue
4
fYear
1993
fDate
8/1/1993 12:00:00 AM
Firstpage
667
Lastpage
680
Abstract
Space vacuum is considered as an insulation component to achieve constructional and operational advantages over totally enclosed designs for the increasing demand for higher levels of electrical power and voltages in spaceborne electrical systems. The dielectric properties of space vacuum insulations are determined mainly by the space environment and local contaminations of the spacecraft structure. Specific aspects of the insulation, such as temperature, pressure, radiation, charged particle flux, outgassing products, and effluents, are discussed
Keywords
space vehicle power plants; vacuum insulation; HV design; charged particle flux; dielectric properties; effluents; local contaminations; outgassing products; pressure; radiation; space applications; spaceborne electrical systems; spacecraft structure; temperature; vacuum-insulated power supplies; Dielectrics and electrical insulation; Power supplies; Pulse amplifiers; Pulsed power supplies; Remote sensing; Space exploration; Space vehicles; Spaceborne radar; Vacuum systems; Voltage;
fLanguage
English
Journal_Title
Electrical Insulation, IEEE Transactions on
Publisher
ieee
ISSN
0018-9367
Type
jour
DOI
10.1109/14.231550
Filename
231550
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