| Attribute | Mitsubishi T-2 × | North American FJ-4 Fury × |
|---|---|---|
| General | ||
| Manufacturer | Mitsubishi Heavy Industries | North American Aviation NAA |
| Model | Mitsubishi T-2 | North American FJ-4 Fury |
| Country | Japan | United States |
| Manufactured from (year) | 1971 | 1954 |
| Manufactured to (year) | 1988 | 1968 |
| Type | Military Trainers | Fighter Jets |
| Icao | T2 | FJ4 |
| Performance | ||
| Engine | 2x Ishikawa-Harima TF40-801A | 1x Wright J65-W-16A |
| Power, lbf (lbf) | 7,140 | 7,700 |
| Avionics | Mitsubishi Electric J/AWG-11, French Thomson-CSF HUD, Lear-Siegler 501OBL AHRS | - |
| Max cruise speed (km/h) | 1,704 | 1,093 |
| Travel range (km) | 2,871 | 3,250 |
| Service ceiling (m) | 15,240 | 14,265 |
| Rate of climb (m/sec) | 177.8 | 38.91 |
| Weights | ||
| Max take off weight (kg) | 12,800 | 10,750 |
| Max payload (kg) | 2,700 | 2,200 |
| Fuel tank capacity (l) | 3,823 | 3,180 |
| Dimensions | ||
| Seats | 2 | 1 |
| Exterior length (m) | 17.85 | 11.1 |
| Tail height (m) | 4.39 | 4.2 |
| Fuselage diameter (m) | 1.1 | 1.4 |
| Wing span (m) | 7.88 | 11.9 |
| Wing tips | No Winglets | No Winglets |