Improved maneuverability and controllability are prime goals in meeting a broad spectrum of tactical missile requirements. Configuration based on the Vought 'Propulsion Augmented Control/Lift Surface' (PACS) approach to aeropropulsive integration are candidates for satisfying these requirements. The PACS concept utilizes a jet issuing from a trailing edge nozzle to induce augmented control loadings over fin or wing planforms. The current work provides experimental validation of PACS feasibility for a representative missile fin geometry at typical supersonic/transonic conditions. (Author)


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    Title :

    Propulsion Augmented Control/Lift Surface Validation for Missile Maneuver Application


    Contributors:
    R. L. Mask (author) / J. G. Spangler (author) / C. H. Haight (author)

    Publication date :

    1982


    Size :

    158 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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