| TECHNICAL
SPECIFICATIONS ( Rafale) |
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General characteristics
- Crew: 1 or 2
- Length: 15.27 m (50.1 ft)
- Wingspan: 10.80 m (35.4 ft)
- Height: 5.34 m (17.5 ft)
- Wing area: 45.7 m (492 ft)
- Empty weight: 9.1 t (Rafale C); 9.5 t (Rafale B); 9.8 t (Rafale M)
- Max takeoff weight: 24,500 kg (54,000 lb)
- Powerplant: 2 x SNECMA M88-2 turbofans
- Dry thrust: 48.7 kN (10,960 lbf) each
- Thrust with afterburner: 73.0 kN (16,400 lbf) each
Performance
- Maximum speed:
- High altitude: Mach 1.8 (2,150 km/h, 1,160 knots)
- Low altitude: 1,390 km/h, 750 knots
- Combat radius: 1,852+ km (1,000+ nmi) on penetration mission
- Service ceiling 16,800 m (55,000 ft)
- Rate of climb: 304.8+ m/s (1,000+ ft/s)
- Wing loading: 326 kg/m (83 1/3 lb/ft)
- Thrust/weight: 1.13
Armament
- Guns: 1 x 30 mm (1.18 in) GIAT 30/719B cannon with 125 rounds
- Missiles:
- Air-to-air:
- MICA IR/EM or
- Magic II and in the future
- MBDA Meteor
- Air-to-ground:
- MBDA Apache or
- SCALP EG or
- AASM or
- GBU-12 Paveway II or
- AM 39 Exocet or
- ASMP-A nuclear missile
Avionics
- Thales RBE2 radar
- Thales SPECTRA electronic warfare system.
- Thales/SAGEM OSF (Optronique Secteur Frontal) infrared search and track system.
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