DocumentCode :
1470384
Title :
Next generation GOES satellite power subsystem
Author :
Krummann, William
Author_Institution :
Hughes Space & Commun., Los Angeles, CA, USA
Volume :
16
Issue :
4
fYear :
2001
fDate :
4/1/2001 12:00:00 AM
Firstpage :
23
Lastpage :
28
Abstract :
Hughes space and communications was awarded a contract in January 1998 from NASA´s Goddard Space Flight Center for the design, manufacture, integration and launch of two next generation geostationary operational environmental satellites (GOES) and options for two additional satellites. The satellites measure weather phenomena as the primary mission and X-rays and charged particles as the secondary missions. This paper describes the GOES electrical power subsystem (EPS) requirements, architecture, hardware and energy balance analysis. As of this writing, the design of the EPS has completed the critical design review phase and the hardware has entered the manufacturing phase
Keywords :
artificial satellites; energy storage; power supply circuits; secondary cells; solar cell arrays; space vehicle power plants; GOES electrical power subsystem; GOES satellite power subsystem; Hughes; NASA; X-rays; battery; charged particles; critical design review; geostationary operational environmental satellites; power distribution; secondary missions; solar array; weather; Circuits; Insulation; Satellites; Voltage;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems Magazine, IEEE
Publisher :
ieee
ISSN :
0885-8985
Type :
jour
DOI :
10.1109/62.918023
Filename :
918023
Link To Document :
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