The attitude control is installed on a space vehicle. A jetting device expels a gas on command from the space ship or from a remote station. A set of the devices are mounted to control the yaw, roll and spin axes. Each control unit is connected to a source of air or gas pressure.


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    Title :

    Attitude Control for Spacecraft


    Contributors:
    F. F. Batsch (author) / J. Laub (author) / F. R. Mitchell (author)

    Publication date :

    1965


    Size :

    1 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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