30 cm diameter mercury bombardment low impulse thrustor development for potential space applications, discussing performance and control


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    Title :

    Performance and control of a 30-cm-diam, low-impulse, Kaufman thruster


    Contributors:

    Conference:

    AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, ELECTRIC PROPULSION CONFERENCE, 7TH ; 1969 ; WILLIAMSBURG, VA


    Publication date :

    1970-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English