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
Link To Document :
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