Spacecraft electric propulsion parameters and launching vehicle characteristics in low thrust mission simulation, discussing spacecraft path


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    Title :

    Mission analysis model requirements for electric propulsion.


    Contributors:

    Conference:

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


    Publication date :

    1969-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :