Dassault Rafale
1986
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Dassault Rafale

The Rafale ('Squall') was originally conceived in the early 1980s by Dassault as the ACX (Advanced Combat Experimental) to demonstrate technologies applicable to a French air force Jaguar replacement (ACT= Avions Combat Tactique) and a French navy Crusader and Super Etendard replacement (ACM= Avion de Combat Marine). The Rafale A technology demonstrator, powered by two General Electric F404 turbofans, was rolled out of the Saint-Cloud factory on 14 December 1985, and went supersonic on its first flight on 4 July 1986. In April 1987, the prototype demonstrated a series of approaches to the aircraft-carrier Clemenceau to establish the feasibility of carrier operations. In April 1989 the aircraft was laid-up for the substitution of a SNECMA M88-2 augmented turbofan in the port engine bay and flew in this configuration on 27 February 1990. The M88 is the selected engine for production versions of the Rafale.

3-View 
Dassault RafaleA three-view drawing (1638 x 924)


Specification 
 MODELRafale C
 ENGINE2 x SNECMA M88-2 turbofans, 7500kg
 WEIGHTS
    Take-off weight19500 kg42990 lb
    Empty weight9060 kg19974 lb
 DIMENSIONS
    Wingspan10.9 m35 ft 9 in
    Length15.3 m50 ft 2 in
    Height5.34 m17 ft 6 in
 PERFORMANCE
    Max. speed2070 km/h1286 mph
 ARMAMENT1 x 30mm cannon, bombs and missiles on 14 hardpoints

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