Recent mission studies have shown that a Hall thruster which operates at relatively constant thrust efficiency (45-55%) over a broad power range (300W - 3kW) is enabling for deep space science missions when compared with slate-of-the-art ion thrusters. While conventional (annular) Hall thrusters can operate at high thrust efficiency at kW power levels, it is difficult to construct one that operates over a broad power envelope down to 0 (100 W) while maintaining relatively high efficiency. In this note we report the measured performance (I(sub sp), thrust and efficiency) of a cylindrical Hall thruster operating at 0 (100 W) input power.


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    Titel :

    Performance of a Low-Power Cylindrical Hall Thruster


    Beteiligte:
    K. A. Polzin (Autor:in) / T. E. Markusic (Autor:in) / B. J. Stanojev (Autor:in) / A. Dehoyos (Autor:in) / Y. Raitses (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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