Electrostatic ion thrustor employing cesium on tungsten contact ionization for satellite attitude control and stationkeeping missions


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental performance of a low-thrust, divergent-flow, contact-ionization electrostatic thrustor


    Contributors:

    Conference:

    PROPULSION JOINT SPECIALIST CONF. ; 1966 ; COLORADO SPRINGS


    Publication date :

    1966-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English