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 D1 in a +Y direction from a satellite gravity center (101) to the first thruster group and a second distance D2 in a −Y direction from the satellite gravity center to the second thruster group becomes inverse to a ratio between the first operating number and the second operating number.


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    Title :

    ARTIFICIAL SATELLITE AND SATELLITE PROPULSION METHOD


    Contributors:

    Publication date :

    2019-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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