The evolutionary development of high specific impulse electric thruster technology
James S. Sovey, John A. Hamley, Michael J. Patterson, Vincent K. Rawlin, Roger Myers
Abstract
James S. Sovey, John A. Hamley, Michael J. Patterson, Vincent K. Rawlin, Roger Myers
Abstract
Electric propulsion flight and technology demonstrations conducted in the USA, Europe, Japan, China, and USSR are reviewed with reference to the major flight qualified electric propulsion systems. These include resistojets, ion thrusters, ablative pulsed plasma thrusters, stationary plasma thrusters, pulsed magnetoplasmic thrusters, and arcjets. Evolutionary mission applications are presented for high specific impulse electric thruster systems. The current status of arcjet, ion, and magnetoplasmadynamic thrusters and their associated power processor technologies are summarized.
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Electric propulsion flight and technology demonstrations conducted in the USA, Europe, Japan, China, and USSR are reviewed with reference to the major flight qualified electric propulsion systems. These include resistojets, ion thrusters, ablative pulsed plasma thrusters, stationary plasma thrusters, pulsed magnetoplasmic thrusters, and arcjets. Evolutionary mission applications are presented for high specific impulse electric thruster systems. The current status of arcjet, ion, and magnetoplasmadynamic thrusters and their associated power processor technologies are summarized.
Key concepts: Arcjet rocket, Electrically powered spacecraft propulsion, Specific impulse, Ion thruster, Aerospace engineering, Propulsion, Impulse (physics), Plasma