Electric propulsion - The future is now

Computer Science – Performance

Scientific paper

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Arc Jet Engines, Electric Propulsion, Propulsion System Performance, Spacecraft Maneuvers, Stationkeeping, Hydrazines, Mars (Planet), Nuclear Electric Propulsion, Payloads, Transfer Orbits

Scientific paper

A comprehensive development status evaluation is presented for the field of electric propulsion. Specific impulses range from 500-800 sec for satellite stationkeeping and 800-1500 sec of earth-earth orbit-raising maneuvers to 2000-5000 sec for trajectories to Mars and as much as 5000-100,000 sec for trajectories to more distant destinations. The successful deployment of low-power arcjet systems for auxilliary propulsion has been critical to the development of designs for higher-performance devices.

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