Comparison of Lockheed Martin T50 Golden Eagle and Mitsubishi F-2 [S]ave
| Attribute |  Mitsubishi F-2 × |  Lockheed Martin T50 Golden Eagle × |
|---|---|---|
| General | ||
| Manufacturer | Mitsubishi Heavy Industries | Lockheed Martin Aeronautics |
| Model | Mitsubishi F-2 | Lockheed Martin T50 Golden Eagle |
| Country | Japan | United States |
| Manufactured from (year) | 1995 | 2005 |
| Manufactured to (year) | 2011 | - |
| Type | Fighter Jets | Military Trainers |
| Icao | F2 | K50 |
| Performance | ||
| Engine | 1x General Electric F110-IHI-129 | 2x 1 × General Electric F404-102 |
| Power, lbf (lbf) | 29,500 | 17,700 |
| Avionics | J/APG-2, AN/ARC-164, NEC V/UHF transceiver, Japan Aviation Electronics/Honeywell digital AFCS etc. | Lockheed Martin Advanced Avionics |
| Max cruise speed (km/h) | 2,124 | 1,833 |
| Approach speed (km/h) | - | 241 |
| Travel range (km) | 835 | 1,852 |
| Fuel economy (km/l) | - | 0.793 |
| Service ceiling (m) | 17,983 | 14,630 |
| Rate of climb (m/sec) | 243.84 | 198.12 |
| Take off distance (m) | 450 | 400 |
| Landing distance (m) | 650 | 520 |
| Weights | ||
| Max take off weight (kg) | 22,100 | 13,517 |
| Max landing weight (kg) | 18,300 | 10,300 |
| Max payload (kg) | 9,000 | 4,536 |
| Fuel tank capacity (l) | 4,637 | 3,331 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 15.5 | 12.98 |
| Tail height (m) | 5 | 4.78 |
| Fuselage diameter (m) | 1.3 | 1 |
| Wing span (m) | 11.1 | 9.17 |
| Wing tips | No Winglets | No Winglets |
Help · Contact us · Disclaimer · Contributors · Developers · Donate