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.
Dassault mirage G
Dassault mirage G
Aircraft Engineering ; 40 , n 4
1968
2 pages
Article (Journal)
English
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