The Columbia accident has focused attention on the critical need for on-orbit repair concepts for wing leading edges in the event that potentially catastrophic damage is incurred during Space Shuttle Orbiter flight. The leading edge of the space shuttle wings consists of a series of eleven panels on each side of the orbiter. These panels are fabricated from reinforced carbon-carbon (RCC) which is a light weight composite with attractive strength at very high temperatures. This paper reports one large area repair concept referred to as metallic overwrap.


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    Titel :

    Metallic Concepts for Repair of Reinforced Carbon-Carbon Space Shuttle Leading Edges


    Beteiligte:
    F. Ritzert (Autor:in) / J. Nesbitt (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch