Mitsubishi F-2
Fighter
The Mitsubishi F-2 is a single-engine single-seat multi-role fighter aircraft produced by the Japanese manufacturer Mitsubishi Heavy Industries.
The Mitsubishi F-2 is a development of the General Dynamics / Lockheed
F-16 Fighting Falcon and was developed together with Lockheed Martin. The F-2A is the single-seat version and F-2B is the two-seat version.
Propulsion | 1 Turbofan Engine |
Engine Model | General Electric F110-GE-129 |
Engine Power dry/with Afterburner | 75,6 / 129,0 kN | 17000 / 29000 lbf |
Speed | 2124 km/h | 1147 kts 1320 mph |
Mmo (max. Mach) | Mach 2.0 |
Service Ceiling | 17.900 m | 58.727 ft |
Rate of climb | 15300 m/min | 50197 ft/min |
Range | 833 km | 450 NM 518 mi. |
Empty Weight | 9.525 kg | 21.000 lbs |
max. Takeoff Weight | 22.100 kg | 48.720 lbs |
Wing Span | 11,13 m | 36 ft 6 in |
Wing Area | 34,8 m² | 375 ft² |
Length | 15,52 m | 50 ft 11 in |
Height | 4,96 m | 16 ft 3 in |
First Flight | 07.10.1995 |
Production Status | in production |
Developed from | Lockheed F-16 |
ICAO Code | F2 |
Data for (Version) | Mitsubishi F-2A |
Variants | F-2A, F-2B |