Mitsubishi F-1
Fighter / Fighter Bomber
The Mitsubishi F-1 is a twin-engined single-seat jet fighter and fighter bomber aircraft produced by the Japanese manufacturer Mitsubishi Heavy Industries, operated by the Japan Air Self Defense Force.
The Mitsubishi F-1 is a development of the
Mitsubishi T-2 jet trainer aircraft.
| Propulsion | 2 Turbofan Engines |
| Engine Model | Ishikawajima Harima TF-40-IHI-801A |
Engine Power (each)
dry/with Afterburner | 21,0 / 31,6 kN | 4721 / 7100 lbf |
| Speed | 1700 km/h | 918 kts
1056 mph |
| Service Ceiling | 15.250 m | 50.033 ft |
| Range | 1.130 km | 610 NM
702 mi. |
| Empty Weight | 6.358 kg | 14.017 lbs |
| max. Takeoff Weight | 13.674 kg | 30.146 lbs |
| Wing Span | 7,88 m | 25 ft 10 in |
| Wing Area | 21,2 m² | 228 ft² |
| Length | 17,66 m | 57 ft 11 in |
| Height | 4,39 m | 14 ft 5 in |
| First Flight | 03.06.1975 |
| Production Status | out of production |
| Total Production | 77 |
| Developed from | Mitsubishi T-2 |
| ICAO Code | F1 |
| Data for (Version) | Mitsubishi F-1 |
