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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.
 | A three-view drawing (1638 x 924) |
| MODEL | Rafale C |
| ENGINE | 2 x SNECMA M88-2 turbofans, 7500kg |
| WEIGHTS |
| Take-off weight | 19500 kg | 42990 lb |
| Empty weight | 9060 kg | 19974 lb |
| DIMENSIONS |
| Wingspan | 10.9 m | 35 ft 9 in |
| Length | 15.3 m | 50 ft 2 in |
| Height | 5.34 m | 17 ft 6 in |
| PERFORMANCE |
| Max. speed | 2070 km/h | 1286 mph |
| ARMAMENT | 1 x 30mm cannon, bombs and missiles on 14 hardpoints |
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