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    Titel :

    Near Exit Plane Velocity Field of 200 W Hall Thruster


    Beteiligte:

    Kongress:

    39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit



    Erscheinungsdatum :

    01.01.2003




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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