Mitsubishi F-2
Photo ©: Katsunori Kimura (photos at airliners.net)
F-2
Fighter
The Mitsubishi F-2 is a single-engine single-seat multi-role fighter aircraft built by the Japanese manufacturer Mitsubishi Heavy Industries.
| Crew | 1 | |
| Propulsion | 1 Turbofan Engine | |
| Engine Model | General Electric F110-GE-129 | |
| Engine Power dry/with Afterburner | 75,5 / 131,7 kN | 16973 / 29607 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 | 36,5 ft |
| Wing Area | 34,8 m² | 375 ft² |
| Length | 15,52 m | 50,9 ft |
| Height | 4,96 m | 16,3 ft |
| First Flight | 07.10.1995 | |
| Production Status | in production | |
| Developed from | Lockheed F-16 | |
| Data for (Version) | Mitsubishi F-2A | |
| Variants | F-2A, F-2B | |
Remarks
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.
| Extras | |
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