Computer Science – Performance
Scientific paper
Jul 1992
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1992aeam...30...38t&link_type=abstract
Aerospace America (ISSN 0740-722X), vol. 30, no. 7, July 1992, p. 38-41, 49.
Computer Science
Performance
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.
Andrews Joy C.
Beattle John R.
Curran Francis M.
Gilland James
Turchi Peter J.
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