| Attribute | Mitsubishi T-2 × | Vought F7U Cutlass × |
|---|---|---|
| General | ||
| Manufacturer | Mitsubishi Heavy Industries | Vought |
| Model | Mitsubishi T-2 | Vought F7U Cutlass |
| Country | Japan | United States |
| Manufactured from (year) | 1971 | 1948 |
| Manufactured to (year) | 1988 | 1955 |
| Type | Military Trainers | Fighter Jets |
| Icao | T2 | F7U |
| Performance | ||
| Engine | 2x Ishikawa-Harima TF40-801A | 2x Westinghouse J46-WE-8B |
| Power, lbf (lbf) | 7,140 | 6,000 |
| Avionics | Mitsubishi Electric J/AWG-11, French Thomson-CSF HUD, Lear-Siegler 501OBL AHRS | - |
| Max cruise speed (km/h) | 1,704 | 1,122 |
| Approach speed (km/h) | - | 172 |
| Travel range (km) | 2,871 | 1,482 |
| Service ceiling (m) | 15,240 | 12,375 |
| Rate of climb (m/sec) | 177.8 | 73.25 |
| Take off distance (m) | - | 486 |
| Landing distance (m) | - | 486 |
| Weights | ||
| Max take off weight (kg) | 12,800 | 12,174 |
| Max payload (kg) | 2,700 | 3,000 |
| Fuel tank capacity (l) | 3,823 | 3,676 |
| Dimensions | ||
| Seats | 2 | 1 |
| Exterior length (m) | 17.85 | 12.58 |
| Tail height (m) | 4.39 | - |
| Fuselage diameter (m) | 1.1 | 1 |
| Wing span (m) | 7.88 | 12.1 |
| Wing tips | No Winglets | No Winglets |