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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    Titel :

    Thrust Vectoring Apparatus for Maneuvering Missile in Flight


    Beteiligte:
    M. V. Krumins (Autor:in) / L. H. Schindel (Autor:in)

    Erscheinungsdatum :

    1984


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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