The patent application describes a low drag gyro stabilized radome for an aircraft. The radome is pivoted for roll and pitch by a universal joint between the radome and a pylon rigidly attached to the aircraft thereby enabling the radome, under gyro control, to remain horizontal to the ground during varying flight attitudes. An enclosed antenna is driven independently of the radome for tilt and sweep motion.


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    Title :

    Gyro Stabilized Radome


    Contributors:

    Publication date :

    1975


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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