This report describes a thrust vector control system for rockets that use a solid protrusion inserted into the exit cone of the rocket nozzle. This protrusion is inserted linearly into one side of the rocket exit nozzle and creates a side force for use in control of the missile in flight.


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    Title :

    Solid Protrusion Jet Vector Control System


    Contributors:

    Publication date :

    1979


    Size :

    7 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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