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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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