A preliminary design study was conducted to evaluate the suitability of the NASA 515 airplane as a flight demonstration vehicle, and to develop plans, schedules, and budget costs for fly-by-wire/active controls technology flight validation in the NASA 515 airplane. The preliminary design and planning were accomplished for two phases of flight validation.


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    Title :

    Requirements and feasibility study of flight demonstration of Active Controls Technology (ACT) on the NASA 515 airplane


    Contributors:

    Publication date :

    1975-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English