The modification of a multi-jackbolt mechanism, Superbolt(TM), for on-orbit release of highly loaded bolts is described. Preload and release test data demonstrate that modification of a commercial product produced a solution for the deployment of the Space Station Remote Manipulator System (SSRMS) that was less expensive, faster, and lighter than other alternatives. Using the Superbolt design, virtually unlimited bolt loads can be applied or released with a standard wrench.


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    Titel :

    EVA assembly and release of highly loaded bolts


    Beteiligte:
    Olmstead, Jim (Autor:in) / Barker, Paul (Autor:in)


    Erscheinungsdatum :

    01.05.1996


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    EVA Assembly and Release of Highly Loaded Bolts

    Olmstead, J. / Barker, P. / United States; National Aeronautics and Space Administration | British Library Conference Proceedings | 1996



    Universal Assembly for Captive Bolts

    Marke, M. L. / Hagopian, B. | NTRS | 1982


    Design and Assembly Considerations for Bolts

    Shugart,J. / Rockford Products,US | Kraftfahrwesen | 1976


    Design and Assembly Considerations for Bolts

    Shugart, Jack | SAE Technical Papers | 1976