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Dassault Rafale Multi-Role Fighter |
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DESCRIPTION:
Instead of proceeding with the Eurofighter project, France decided to develop its own advanced next-generation fighter, the ACX, later to become the Rafale. The design incoporates canards and a fly-by-wire control system for exceptional maneuverability as well as radar-absorbant paint and more rounded surfaces to improve stealth. The Rafale C is a single seat attack fighter for the Air Force while the Rafale M is a navalized version designed to operate from French aircraft carriers. Current plans call for 94 one-seat and 140 two-seat aircraft to be built for the Air Force and 86 for the Navy. The Rafale is intended to replace the Air Force's Mirage III, Mirage 5, Mirage F.1, Jaguar, and Mirage IVP as well as the Navy's F-8 Crusader and Super Etendard.
Data below for Rafale C |
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| HISTORY: | |
| First Flight |
(Rafale A) 4 July 1986 (Rafale C) 19 May 1991 (Rafale M) 12 December 1991 |
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Service Entry
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2002 (?)
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CREW:
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(Rafale C, Rafale M) one: pilot (Rafale B) two: pilot, systems officer |
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ESTIMATED COST:
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unknown
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| AIRFOIL SECTIONS: | |
| Wing Root | unknown |
| Wing Tip |
unknown
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| DIMENSIONS: | |
| Length | 50.21 ft (15.30 m) |
| Wingspan | 35.77 ft (10.90 m) |
| Height | 17.54 ft (5.34 m) |
| Wing Area |
494 ft2 (46.00 m2) including canards? |
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Canard Area
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unknown
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| WEIGHTS: | |
| Empty | 19,975 lb (9,060 kg) |
| Normal Takeoff | 33,200 lb (15,060 kg) |
| Max Takeoff | 47,400 lb (21,500 kg) |
| Fuel Capacity |
internal: 1,405 gal (5,325 L) external: 1,745 gal (6,600 L) |
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Max Payload
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17,635 lb (8,000 kg)
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| PROPULSION: | |
| Powerplant | two SNECMA M88-3 afterburning turbofans |
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Thrust
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39,116 lb (174.0 kN) with afterburner
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| PERFORMANCE: | |
| Max Level Speed |
at altitude: 1,320 mph (2,125 km/h) at 36,090 ft (11,000 m), Mach 2.0 at sea level: 864 mph (1,390 km/h), Mach 1.135 |
| Initial Climb Rate | unknown |
| Service Ceiling | 65,000 ft (19,810 m) |
| Range |
typical: 1,000 nm (1,850 km) [interceptor mission] 1,180 nm (2,185 km) [low-level attack mission] ferry: 2,000 nm (3,705 km) |
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g-Limits
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+9.0 / -3.6
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| ARMAMENT: | |
| Gun | one 30-mm DEFA 791B cannon |
| Stations | twelve external hardpoints and two wingtip rails |
| Air-to-Air Missile | MICA |
| Air-to-Surface Missile | ASMP nuclear weapon, AS.39 Exocet, AS.30 |
| Bomb | 227/1000 kg LGB bombs |
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Other
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rocket pods, ECM pods
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| KNOWN VARIANTS: | |
| Rafale A | Aerodynamic prototype slightly larger and heavier than final production models, used GE F404 engines while the M-88 was under development |
| Rafale B | Two-seat attack fighter/trainer, originally intended as a trainer only, but now envisioned as the primary production model |
| Rafale C | One-seat attack fighter |
| Rafale D | Slightly smaller and lighter version of the Rafale C employing greater stealth features |
| Rafale M |
Carrier-borne single-seat fighter, slightly heavier than Rafale C due to addition of arrestor hook and
strengthened landing gear
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| KNOWN COMBAT RECORD: |
none
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| KNOWN OPERATORS: |
French Air Force French Navy |
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3-VIEW SCHEMATIC:
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SOURCES:
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