The Boeing SST design incorporates a variable-geometry wing. Some of the wing-pivot-joint and actuation-system configurations considered during the development of the SST variable-geometry design are discussed herein. In addition, the selected SST design is described, and detailed maintainability and maintenance requirements are reviewed.


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    Title :

    Maintainability Considerations in Variable Geometry Aircraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1967



    Publication date :

    1967-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Maintainability considerations in variable geometry aircraft

    Onewein, L.J. | Engineering Index Backfile | 1967


    Aerodynamic Design Considerations of Variable Geometry Aircraft

    Herring, R. N. / Landgraf, S. K. | SAE Technical Papers | 1967


    Aerodynamic design considerations of variable geometry aircraft

    Landgraf, S.K. / Herring, R.N. | Engineering Index Backfile | 1967



    Aircraft design for maintainability

    MAJOROS, ANTHONY | AIAA | 1989