A flightworthy active control landing gear system for a supersonic aircraft was designed to minimize aircraft loads during takeoff, impact, rollout, and taxi. The design consists of hydromechanical modifications to the existing gear and the development of a fail-safe electronic controller. analytical RESULTS INDICATE that for an aircraft sink rate of 0.914 m/sec (3 ft/sec) the system achieves a peak load reduction of 36% during landing impact.


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    Titel :

    Flightworthy active control landing gear for a supersonic aircraft


    Beteiligte:
    Ross, I. (Autor:in)

    Erscheinungsdatum :

    1980-06-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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