DocumentCode :
356916
Title :
The power subsystem for the next generation GOES satellite
Author :
Krummann, William
Author_Institution :
Hughes Space & Commun., Los Angeles, CA, USA
Volume :
1
fYear :
2000
fDate :
2000
Firstpage :
207
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 :
DC-DC power convertors; artificial satellites; photovoltaic power systems; power distribution; secondary cells; solar cell arrays; space vehicle power plants; GOES satellite electrical power subsystem; Geostationary Operational Environmental Satellites; NASA; architecture; critical design review; energy balance analysis; hardware; manufacturing; requirements; space power; Artificial satellites; Hardware; Instruments; Magnetic fields; Manufacturing; Monitoring; Payloads; Space vehicles; Temperature distribution; Voltage;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Conversion Engineering Conference and Exhibit, 2000. (IECEC) 35th Intersociety
Conference_Location :
Las Vegas, NV
Print_ISBN :
1-56347-375-5
Type :
conf
DOI :
10.1109/IECEC.2000.870688
Filename :
870688
Link To Document :
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