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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    Titel :

    Dassault mirage G


    Weitere Titelangaben:

    Dassault mirage G


    Beteiligte:
    Deplante, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Dassault Mirage IV

    Pelletier, Iain | Online Contents | 1996


    The Dassault Mirage G

    Deplante, Henri | Emerald Group Publishing | 1968




    Überschall-Jagdflugzeug Dassault Mirage 2000-5

    Kordik, E.J. | Tema Archiv | 1998