The performance of a 200 W class Hall thruster was evaluated. Performance measurements were taken at power levels between 90 W and 250 W. At the nominal 200 W design point, the measured thrust was 11.3 mN. and the specific impulse was 1170 s excluding cathode flow in the calculation. A laboratory model 3 mm diameter hollow cathode was used for all testing. The engine was operated on laboratory power supplies in addition to a breadboard power processing unit fabricated from commercially available DC to DC converters.


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    Title :

    Test Results of a 200 W Class Hall Thruster


    Contributors:

    Conference:

    Joint Propulsion Conference ; 1998 ; Cleveland, OH, United States


    Publication date :

    1999-12-01


    Type of media :

    Preprint


    Type of material :

    No indication


    Language :

    English




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