Mechanical actuation of thrust units has been found to be lightest and most desirable method for stabilizing electrically propelled vehicle during thrusting phase of Jupiter flyby mission; nominal mission, spacecraft disturbances, attitude control options and basic selection criteria are noted; mechanical actuator types are discussed and actuator requirements stated; initial mechanism design for accomplishing necessary movement with required accuracy and reliability is detailed. (31896)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Attitude control of electrically propelled spacecraft utilizing primary thrust system


    Weitere Titelangaben:

    ASME Aviation Space -- Progress Prospects


    Beteiligte:
    Reader, P.D. (Autor:in) / Mankovitz, R.J. (Autor:in)

    Kongress:

    ASME Annual Aviation and Space Conference ; 1968 ; United States , Beverly Hills, CA Control



    Erscheinungsdatum :

    1968


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :