When a first operating number being the number of thrusters in a first thruster group (115) that are operated and a second operating number being the number of thrusters in a second thruster group (125) that are operated are different, a ratio between a first distance Din a +Y direction from a satellite gravity center (101) to the first thruster group (115) and a second distance Din a -Y direction from the satellite gravity center (101) to the second thruster group (125) becomes inverse to a ratio between the first operating number and the second operating number.


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    Titel :

    SATELLITE, AND SATELLITE PROPULSION METHOD


    Weitere Titelangaben:

    SATELLIT UND SATELLITENANTRIEBSVERFAHREN
    SATELLITE ET PROCÉDÉ DE PROPULSION DE SATELLITE


    Beteiligte:

    Erscheinungsdatum :

    07.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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