Electric thruster performance for orbit raising and maneuvering

Several electric thrusters are compared to chemical rockets for orbit raising and in-orbit maneuvering applications. For power-intensive payloads and satellites, electric propulsion can show substantial performance advantages over chemical propulsion. The arcjet is promising for near-future applicat...

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Veröffentlicht in:	Journal of spacecraft and rockets 1984-01, Vol.21 (2), p.180-186
Hauptverfasser:	Kaufman, Harold R, Robinson, Raymond S
Format:	Artikel
Sprache:	eng
Schlagworte:	chemical variables control energy conservation Orbital maneuvers propulsion spacecraft
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description	Several electric thrusters are compared to chemical rockets for orbit raising and in-orbit maneuvering applications. For power-intensive payloads and satellites, electric propulsion can show substantial performance advantages over chemical propulsion. The arcjet is promising for near-future applications because of its low power requirements. The electrostatic thruster offers additional performance advantages over the arcjet, but with added power requirements. The performance of the electrostatic thruster can be enhanced considerably if the power processing requirements can be reached.
doi_str_mv	10.2514/3.8631
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ispartof	Journal of spacecraft and rockets, 1984-01, Vol.21 (2), p.180-186
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language	eng
recordid	cdi_aiaa_journals_10_2514_3_8631
source	Alma/SFX Local Collection
subjects	chemical variables control energy conservation Orbital maneuvers propulsion spacecraft
title	Electric thruster performance for orbit raising and maneuvering
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