Mitsubishi T-2
Trainer
The Mitsubishi T-2 is a twin-engined two-seat jet trainer aircraft produced by the Japanese manufacturer Mitsubishi Heavy Industries, operated by the Japan Air Self Defense Force (1975-2006).
| 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 | 15.200 m | 49.869 ft |
| Range | 2.589 km | 1.398 NM
1.609 mi. |
| Empty Weight | 6.307 kg | 13.905 lbs |
| max. Takeoff Weight | 12.900 kg | 28.440 lbs |
| Wing Span | 7,88 m | 25 ft 10 in |
| Wing Area | 21,2 m² | 228 ft² |
| Length | 17,86 m | 58 ft 7 in |
| Height | 4,39 m | 14 ft 5 in |
| First Flight | 20.07.1971 |
| Production Status | out of production |
| Total Production | 90 |
| ICAO Code | MT2 |
| Data for (Version) | Mitsubishi T-2 |
| Variants | T-2A, T-2B |
