| Attribute | Convair F-106 Delta Dart × | Lockheed Martin T50 Golden Eagle × |
|---|---|---|
| General | ||
| Manufacturer | Convair | Lockheed Martin Aeronautics |
| Model | Convair F-106 Delta Dart | Lockheed Martin T50 Golden Eagle |
| Country | United States | United States |
| Manufactured from (year) | 1956 | 2005 |
| Manufactured to (year) | 1968 | - |
| Type | Fighter Jets | Military Trainers |
| Icao | F106 | K50 |
| Performance | ||
| Engine | 1x Pratt & Whitney J75-P-17 | 2x 1 × General Electric F404-102 |
| Power, lbf (lbf) | 24,500 | 17,700 |
| Avionics | Hughes MA-1 Fire Control System & IBM Semi-Automatic Ground Environment | Lockheed Martin Advanced Avionics |
| Max cruise speed (km/h) | 2,454 | 1,833 |
| Approach speed (km/h) | 267 | 241 |
| Travel range (km) | 4,345 | 1,852 |
| Fuel economy (km/l) | - | 0.793 |
| Service ceiling (m) | 17,374 | 14,630 |
| Rate of climb (m/sec) | 152.4 | 198.12 |
| Take off distance (m) | 1,280 | 400 |
| Landing distance (m) | 1,341 | 520 |
| Weights | ||
| Max take off weight (kg) | 18,975 | 13,517 |
| Max landing weight (kg) | 16,021 | 10,300 |
| Max payload (kg) | 4,553 | 4,536 |
| Fuel tank capacity (l) | 5,731 | 3,331 |
| Dimensions | ||
| Seats | 1 | 2 |
| Exterior length (m) | 21.57 | 12.98 |
| Tail height (m) | 6.18 | 4.78 |
| Fuselage diameter (m) | 1.4 | 1 |
| Wing span (m) | 11.68 | 9.17 |
| Wing tips | No Winglets | No Winglets |