Lightweight, reusable cryogenic containers reduce costs of operation of advanced hypersonic airplanes and space launch vehicles. Specimens demonstrated in temperature range of negative 420 to positive 400 degrees F (negative 251 to positive 204 degrees C). Prototype reusable cryogenic foam insulation developed. Consists of two discrete layers of closed-cell polymethacrylimide foam of density 6.9 lb/ft to the 3rd power (111 kg/m to the 3rd power) bonded together with epoxy adhesive. Additionally reinforced with 0.003-in. (0.08-mm)-thick layer of fiberglass cloth. Wrapped with precut and preformed vapor-barrier cover. Such containers useful on Earth in laboratories, factories, and transportation systems.


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    Titel :

    Advanced Reusable Foam Cryogenic Insulation


    Beteiligte:
    Taylor, Allan H. (Autor:in) / Mcauliffe, P. S. (Autor:in) / Sparks, L. L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.04.1990



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Reusable cryogenic foam insulation for advanced aerospace vehicles

    Mcauliffe, Patrick S. / Taylor, Allan H. / Sparks, Larry L. et al. | NTRS | 1991


    Reusable cryogenic foam insulation for advanced aerospace vehicles

    MCAULIFFE, PATRICK / TAYLOR, ALLAN / SPARKS, LARRY et al. | AIAA | 1991


    Reusable High-Temperature/Cryogenic Foam-Insulation System

    Davis, Randall C. / Taylor, Allan H. / Jackson, L. Robert et al. | NTRS | 1987


    Development of a reusable, flight-weight cryogenic foam insulation system

    Mcauliffe, P. S. / Davis, R. C. / Taylor, A. H. | NTRS | 1986


    Development of a reusable, flight-weight cryogenic foam insulation system

    MCAULIFFE, P. / DAVIS, R. / TAYLOR, A. | AIAA | 1986