In response to the Columbia Accident Investigation Board report, a plug repair kit has been developed to enable astronauts to repair the space shuttle's wing leading edge (WLE) during orbit. The plug repair kit consists of several 17.78- cm-diameter carbon/silicon carbide (C/SiC) cover plates of various curvatures that can be attached to the refractory carbon-carbon WLE panels using a TZM refractory metal attach mechanism. The attach mechanism is inserted through the damage in the WLE panel and, as it is tightened, the cover plate flexes to conform to the curvature of the WLE panel within 0.050 mm. An astronaut installs the repair during an extravehicular activity (EVA). After installing the plug repair, edge gaps are checked and the perimeter of the repair is sealed using a proprietary material, developed to fill cracks and small holes in the WLE.


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    Titel :

    Flexible Plug Repair for Shuttle Wing Leading Edge


    Beteiligte:
    Camarda, Charles J. (Autor:in) / Sikora, Joseph (Autor:in) / Smith, Russel (Autor:in) / Rivers, H. (Autor:in) / Scotti, Stephen J. (Autor:in) / Fuller, Alan M. (Autor:in) / Klacka, Robert (Autor:in) / Reinders, Martin (Autor:in) / Schwind, Francis (Autor:in) / Sullivan, Brian (Autor:in)


    Erscheinungsdatum :

    2012-02-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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