Thermo-structural performance of the Space Shuttle orbiter Columbia's leading-edge structural subsystem for the first five (5) flights is compared with the design goals. Lessons learned from thse initial flights of the first reusable manned spacecraft are discussed in order to assess design maturity, deficiencies, and modifications required to rectify the design deficiencies. Flight data and post-flight inspections support the conclusion that the leading-edge structural subsystem hardware performance was outstanding for the initial five (5) flights.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Space shuttle orbiter leading-edge flight performance compared to design goals


    Contributors:


    Publication date :

    1983-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




    Space Shuttle Orbiter Leading Edge Thermal Performance

    Collicott, Howard E. / Bauer, Paul E. | 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


    Space Shuttle Orbiter Leading Edge Structural Subsystem development

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


    Space Shuttle Orbiter Leading Edge Structural Subsystem development

    Curry, D. M. / Latchem, J. W. / Whisenhunt, G. B. | NTRS | 1983