Rafale

Formation of five Rafales making a flypast in 2006

Diagram showing the employment of different construction material

Specifications
Crew: 1–2
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 m² (492 ft²)
Empty weight:

Loaded weight: 14,016 kg (30,900 lb)
Max. takeoff weight: 24,500 kg (C/D), 22,200 kg (M) (54,000 lb)
Powerplant: 2 × Snecma M88-2 turbofans
Dry thrust: 50.04 kN (11,250 lbf) each
Thrust with afterburner: 75.62 kN (17,000 lbf) each
Fuel capacity: 4,700 kg (10,360 lb) internal

Performance

Maximum speed:
High altitude: Mach 1.8 (1,912 km/h, 1,032 knots)
Low altitude: Mach 1.1 (1,390 km/h, 750 knots)
Range: 3,700+ km (2,000+ nmi)
Combat radius: 1,852+ km (1,000+ nmi)on penetration mission
Service ceiling: 15,235 m (50,000 ft)
Rate of climb: 304.8+ m/s (60,000+ ft/min)
Wing loading: 306 kg/m² (62.8 lb/ft²)
Thrust/weight: 0.988 (100% fuel, 2 EM A2A missile, 2 IR A2A missile) version M

Armament

Guns: 1× 30 mm (1.18 in) GIAT 30/719B autocannon with 125 rounds
Hardpoints: 14 for Air Force versions (Rafale B/C), 13 for Navy version (Rafale M) with a capacity of 9,500 kg (21,000 lb) external fuel and ordnance and provisions to carry combinations of:

Missiles:

MBDA MICA IR or EM or Magic II and
MBDA Meteor air-to-air missiles in the future

Air-to-ground:

Air-to-surface:

AM 39-Exocet Deterrence:

ASMP-A nuclear missile Other: