Solar electric propulsion systems - A survey
The Solar Electric Propulsion System (SEPS) currently under development in the United States offers several advantages as a third-stage power system for interplanetary and inter-earth-orbit flights. Its electric propulsion motors (EPM), with the relatively large specific impulse of 30,000 m/sec each, consume less propellant than do chemical rocket motors or compressed-gas engines, and constitute, with the solar batteries, 50% of the SEPS dry mass. Outfitted with 8-10 energy converters with attainable efficiency of 92%, SEPS is being considered for missions that range from the transport of payloads to geosynchronous orbit to an interplanetary rendezvous with Halley's Comet. The paper also presents configuration options and subsystem parameters.
- OSTI ID:
- 5701262
- Journal Information:
- Appl. Solar Energy (Engl. Transl.); (United States), Journal Name: Appl. Solar Energy (Engl. Transl.); (United States) Vol. 16; ISSN ASOEA
- Country of Publication:
- United States
- Language:
- English
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