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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    Titel :

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


    Beteiligte:
    Marrese, C. M. (Autor:in) / Gallimore, A. D. (Autor:in) / Polk, J. E. (Autor:in) / Frisbee, R. H. (Autor:in)

    Erscheinungsdatum :

    13.07.1998


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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