DocumentCode
2116784
Title
Communications satellite power conditioning systems
Author
Dunlop, J.D.
Author_Institution
Communications Satellite Corporation Clarksburg, Maryland
fYear
1970
fDate
20-21 April 1970
Firstpage
5
Lastpage
11
Abstract
Power conditioning systems for each of the four INTELSAT series are reviewed. INTELSAT I through INTELSAT III satellites are currently in operation at synchronous orbit. The INTELSAT IV series is to be launched starting in 1971. Silicon solar cells are the prime source of power for all these satellites; Ni-Cd batteries are used to supply power during eclipse operation. Progressing from INTELSAT I through IV, different methods were used for battery charging, charge control, voltage regulation, and power management. The technical advantages and disadvantages of each of these methods are presented. Suggestions for future satellites include third electrode charge control with a current regulator for battery charging and a boost regulator for battery discharge.
Keywords
Arrays; Batteries; Regulators; Satellites; Space vehicles; Switches; Voltage control;
fLanguage
English
Publisher
ieee
Conference_Titel
Power Electronics Specialists Conference, 1970 IEEE
Conference_Location
Greenlelt, Maryland, USA
ISSN
0275-9306
Type
conf
DOI
10.1109/PECS.1970.7066234
Filename
7066234
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