Background of development of experimental aircraft, designed by Avions Marcel Dassault; variable geometry experimental prototype is supersonic single engine two seater; it is powered with Pratt and Whitney/SNECMA, type TF-306, providing maximum thrust on ground of 9.15 tons and it weighs 10.05 tons (aircraft in its empty and unequipped conditions); owing to its aerodynamic features, aircraft can achieve very high performance in very wide range which is indicated; high lift capability is ensured by very important double flaps and by slotted slats; flight control.


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    Title :

    Dassault mirage G


    Additional title:

    Dassault mirage G


    Contributors:

    Published in:

    Publication date :

    1968


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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