The results of development of an advanced composite door landing-gear assembly are summarized. The development program consisted of design, analysis, fabrication, and structural testing of a door sector assembly designed to the operating loads expected for the Phase B Space Shuttle orbiter.


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    Titel :

    Graphite-epoxy door development for application to Space Shuttle.


    Beteiligte:
    Kam, C. Y. (Autor:in) / Kong, S. J. (Autor:in) / Freeman, V. L. (Autor:in)

    Kongress:

    National Symposium and Exhibition on New horizons in materials and processing ; 1973 ; Los Angeles, CA


    Erscheinungsdatum :

    01.01.1973


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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