Dassault Mirage 2000 - Specifications (Mirage 2000C)

Specifications (Mirage 2000C)

Data from Complete Encyclopedia of World Aircraft, International Directory of Military Aircraft

General characteristics

Crew: 1
Length: 14.36 m (47 ft 1 in)
Wingspan: 9.13 m (29 ft)
Height: 5.20 m (17 ft)
Wing area: 41 m² (441.3 ft²)
Empty weight: 7,500 kg (16,350 lb)
Loaded weight: 13,800 kg (30,420 lb)
Max. takeoff weight: 17,000 kg (37,500 lb)
Powerplant: 1 × SNECMA M53-P2 afterburning turbofan
- Dry thrust: 64.3 kN (14,500 lbf)
- Thrust with afterburner: 95.1 kN (21,400 lbf)

Performance

Maximum speed: Mach 2.2 (2,530+ km/h, 1,500+ mph) at high altitude/ 1,110 km/h (690 mph) at low altitude
Range: 1,550 km (837 nmi, 963 mi) with drop tanks
Ferry range: 3,335 km (1,800 nmi, 2,073 mi) with auxiliary fuel
Service ceiling: 17,060 m (59,000 ft)
Rate of climb: 285 m/s (56,000 ft/min)
Wing loading: 337 kg/m² (69 lb/ft²)
Thrust/weight: 0.91

Armament

Guns: 2× 30 mm (1.18 in) DEFA 554 revolver cannon, 125 rounds per gun
Hardpoints: 9 total (4× under-wing, 5× under-fuselage) with a capacity of 6,300 kg (13,900 lb) external fuel and ordnance
Rockets: Matra 68 mm unguided rocket pods, 18 rockets per pod
Missiles:
- Air-to-air missiles:
  - 6× MBDA MICA IR/RF
  - 2× Matra R550 Magic-II and 2× Matra Super 530D
- Air-to-surface missiles:
  - 2× AM.39 Exocet
  - 2× AS-30L laser guided missile
  - 1× ASMP tactical nuclear cruise missile
Bombs: 9× Mk.82