Composite-material specimens made of graphite fibers and matrix composed of experimental copolymer of bismaleimide and bisfuran. Found to have mechanical and thermal properties comparable or superior to those of similar composite-material specimens. Candidates for use as lightweight structural components to replace metal components in high-temperature aircraft applications. Bismaleimides used widely for other purposes because of low cost and ease in fabrication. Mechanical properties equal or exceed those of composite made with commercial formulation.


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    Title :

    Composite Of Bisfuran/Bismaleimide With Graphite Fibers


    Contributors:

    Published in:

    Publication date :

    1995-12-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :





    Open-Hole Tension Fatigue Behavior of a Graphite/Bismaleimide at Elevated Temperatures

    Gates, T. S. / Johnston, W. M. / ASME; Aerospace Division | British Library Conference Proceedings | 1996


    Open-Hole Tension Fatigue Behavior of a Graphite/Bismaleimide at Elevated Temperatures

    Gates, T. S. / Johnston, W. M. | British Library Online Contents | 1996