Thrust vectoring apparatus for a missile is described for imparting bank and pitch to the missile for maneuvering it in flight. The missile is provided with a generally rectangular jet exhaust opening in which is pivotally mounted a pair of two-dimensional plugs which define a plug nozzle for the opening. The plugs, disposed on opposite sides of a vertical longitudinal plane of the missile, are adapted to be selectively and independently pivoted in response to a control mechanism acting in response to guidance command signals for banking and pitching the missile for maneuvering it in flight.


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    Title :

    Thrust Vectoring Apparatus for Maneuvering Missile in Flight


    Contributors:

    Publication date :

    1984


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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