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
Link To Document :
بازگشت