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Title: Oxygen-Propellant Plasma Thrusters for Cis-Lunar Electric Propulsion Missions
Authors: Frisbee, R. H.
Polk, J. E.
Gallimore, A. D.
Marrese, C. M.
Issue Date: 13-Jul-1998
Citation: AIAA Joint Propulsion Conference
Cleveland, OH, U.S.A.
Abstract: This paper presents an analysis of the mission benefits and technology requirements of electric propulsion thrusters designed to use oxygen (O2) as propellant, and an overview of the status of current research in this area.
Appears in Collections:JPL TRS 1992+

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