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Specifications (Tiger HAP)
General characteristics
- Crew: 2 (pilot, weapon systems officer)
- Length: 14.08 m fuselage (46 ft 2 in)
- Rotor diameter: 13.00 m (42 ft 8 in)
- Height: 3.83 m (12 ft 7 in)
- Disc area: 133 m² (1,430 ft²)
- Empty weight: 3,060 kg (6,750 lb)
- Max takeoff weight: 6,000 kg (13,000 lb)
- Internal fuel capacity: 1,080 kg (2,380 lb)
- Powerplant: 2× Rolls-Royce/Turbomeca/MTU MTR390 turboshafts, 873 kW (1,170 shp) each
Performance
- Maximum speed: 290 km/h with mast, 315 km/h without mast (157 knots, 181 mph with mast, 170 knots or 196 mph without mast)
- Range: 800 km (430 nm, 500 mi) combat (with external tanks in the inboard stations: 1300km)
- Service ceiling: 4,000 m (13,000 ft)
- Rate of climb: 10.7 m/s (2,105 ft/min)
Armament
- Guns:
- 1× 30 mm (1.18 in) GIAT 30 cannon in chin turret
On its two inner hardpoints and two outer hardpoints the Eurocopter Tiger can carry a combination of the following weapons:
- on each of its two inner hardpoints:
- 2x 20 mm (0.787 in) machine cannons in a pod, or
- 22× 68 mm (2.68 in) SNEB unguided missiles in a pod
- on each of its two outer hardpoints:
- 2× Mistral air-to-air missiles, or
- 12× 68 mm (2.68 in) SNEB unguided missiles in a pod