Attribute | ![]() Mitsubishi F-1 × | ![]() Mitsubishi T-2 × |
---|---|---|
General | ||
Manufacturer | Mitsubishi Heavy Industries | Mitsubishi Heavy Industries |
Model | Mitsubishi F-1 | Mitsubishi T-2 |
Country | Japan | Japan |
Manufactured from (year) | 1975 | 1971 |
Manufactured to (year) | 1987 | 1988 |
Type | Fighter Jets | Military Trainers |
Icao | F1 | T2 |
Performance | ||
Engine | 2x Ishikawa-Harima TF40-801A | 2x Ishikawa-Harima TF40-801A |
Power, lbf (lbf) | 8,000 | 7,140 |
Avionics | J/AWG-12 radar, J/ASQ-1 FCS, Lear-Siegler AHRS, J/APR-3 RHAWS | Mitsubishi Electric J/AWG-11, French Thomson-CSF HUD, Lear-Siegler 501OBL AHRS |
Max cruise speed (km/h) | 1,704 | 1,704 |
Approach speed (km/h) | 282 | - |
Travel range (km) | 2,871 | 2,871 |
Service ceiling (m) | 15,240 | 15,240 |
Rate of climb (m/sec) | 177.8 | 177.8 |
Weights | ||
Max take off weight (kg) | 13,674 | 12,800 |
Max payload (kg) | 2,720 | 2,700 |
Fuel tank capacity (l) | 3,710 | 3,823 |
Dimensions | ||
Seats | 1 | 2 |
Exterior length (m) | 17.86 | 17.85 |
Tail height (m) | 4.48 | 4.39 |
Fuselage diameter (m) | 1 | 1.1 |
Wing span (m) | 7.88 | 7.88 |
Wing tips | No Winglets | No Winglets |