Recent evolutions and improvements in three material families are presented: glass ceramic matrix composites for uses up to 1000 C; ceramic matrix composites for uses up to 1500 C; oxidation resistant carbon/carbon composites for uses beyond 1500 up to 2000 C. The strengths of these thermostructural composites are summarized. Their usefulness in applications (temperature/time) in the fields of missiles and ramjets, hypersonic transportation systems, space planes, etc. is shown.


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    Titel :

    Thermostructural Composites: Recent Evolutions and Improvements


    Beteiligte:
    J. F. Jamet (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    11 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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