The development of the Space Shuttle Orbiter Leading Edge Structural Subsystem (LESS) is traced from concept definition, through technical development, to final design, qualification testing and flight performance. A detailed description of the LESS is presented to support a discussion of the design, material development and thermal/structural integration. Extensive development/qualification tests and analytical studies were performed to verify the thermal/structural system performance and to certify the LESS for flight. Flight data and detailed post-flight inspection results are presented which support the conclusion that the LESS system performance has been outstanding.


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    Titel :

    Space Shuttle Orbiter Leading Edge Structural Subsystem development


    Beteiligte:
    Curry, D. M. (Autor:in) / Latchem, J. W. (Autor:in) / Whisenhunt, G. B. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1983 ; Reno, NV


    Erscheinungsdatum :

    1983-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Space Shuttle Orbiter Leading Edge Structural Subsystem development

    CURRY, D. / LATCHEM, J. / WHISENHUNT, G. | AIAA | 1983


    Space Shuttle Orbiter leading edge structural subsystem thermal performance

    Curry, D. M. / Cunningham, J. A. / Frahm, J. R. | NTRS | 1982


    Space Shuttle Orbiter leading edge structural subsystem thermal performance

    CURRY, D. / CUNNINGHAM, J. / FRAHM, J. | AIAA | 1982