The graphite fiber reinforced glass matrix composite system is described. Although this composite is not yet a mature material, it possesses low density, attractive mechanical properties at elevated temperatures, and good environmental stability. Properties are reported for a borosilicate glass matrix unidirectionally reinforced with 60 volume percent HMS graphite fiber. The flexural strength and fatigue characteristics at room and elevated temperature, resistance to thermal cycling and continuous high temperature oxidation, and thermal expansion characteristics of the composite are reported. The properties of this new composite are compared to those of advanced resin and metal matrix composites showing that graphite fiber reinforced glass matrix composites are attractive for aerospace applications. (Kursetz)


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    Titel :

    Graphite fiber reinforced glass matrix composites for aerospace applications


    Weitere Titelangaben:

    Kohlenfaserverstaerkte Verbundwerkstoffe mit Glasmatrix in ihrer Anwendung in der Raumfahrttechnik


    Beteiligte:
    Prewo, K.M. (Autor:in) / Bacon, J.F. (Autor:in) / Dicus, D.L. (Autor:in)


    Erscheinungsdatum :

    1979


    Format / Umfang :

    11 Seiten, 8 Bilder, 3 Tabellen, 7 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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