The seal of the present invention is one which performs the dual function of providing a pressure seal and a thermal barrier in a variable space for the extreme pressure and heat conditions encountered, for example, in space flight. The seal features the ability to roll, compress, and expand to maintain a pressure-tight thermal seal for preventing entry of hot gases into spaces between adjacent members of the spacecraft.


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    Titel :

    Thermal Barrier Pressure Seal


    Beteiligte:
    J. Bellavia (Autor:in) / J. O. Kane (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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