A prototype docking mechanism for the Space Station was designed and fabricated for NASA. This docking mechanism is actively controlled and uses a set of electromechanical actuators for alignment and load attenuation. Dynamic tests are planned using the Marshall Space Flight Center's 6-DOF Motion Simulator. The proposed tests call for basic functionality verification as well as complete hardware-in-the-loop docking dynamics simulations.


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    Titel :

    Space Station Docking Mechanism Dynamic Testing


    Beteiligte:
    T. G. Howsman (Autor:in) / J. R. Glaese (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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