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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Graphite-epoxy door development for application to Space Shuttle.


    Contributors:
    Kam, C. Y. (author) / Kong, S. J. (author) / Freeman, V. L. (author)

    Conference:

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


    Publication date :

    1973-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English






    Space Shuttle development update

    Brand, V. | NTRS | 1984


    Space shuttle SRM development

    Adams, I. C. / Call, F. W. | NTRS | 1979


    Space shuttle nozzle development

    Canfield, A.R. / Anderson, E.E. / Nichols, G.E. | Tema Archive | 1978