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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    Titel :

    Attitude Control for Spacecraft


    Beteiligte:
    F. F. Batsch (Autor:in) / J. Laub (Autor:in) / F. R. Mitchell (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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