A fairing assembly for an aerial vehicle having a tank that forms a body of the vehicle and a wing coupled to the tank is provided. The fining assembly includes a substructure configured to couple with a tank skin of the tank, a thermal protection system coupled to the substructure, and a seal assembly coupled to the substructure, the seal assembly being configured to overlap at least a portion of an edge of the wing.


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    Titel :

    Fairing assembly and method therefor


    Beteiligte:
    BEST MICHAEL J (Autor:in) / EMBLER JONATHAN D (Autor:in) / KRUSE JOHN S (Autor:in) / PINNEY THOMAS R (Autor:in) / SMALLWOOD DREW L (Autor:in)

    Erscheinungsdatum :

    2020-09-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS



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