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.


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    Title :

    Oxygen-Propellant Plasma Thrusters for Cis-Lunar Electric Propulsion Missions


    Contributors:

    Publication date :

    1998-07-13


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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