Attribute | North American B-25 Mitchell × | Vickers VC.1 Viking × |
---|---|---|
General | ||
Manufacturer | North American Aviation NAA | Vickers-Armstrongs |
Model | North American B-25 Mitchell | Vickers VC.1 Viking |
Country | United States | United Kingdom |
Manufactured from (year) | 1940 | 1945 |
1↑Manufactured to (year) | 1945 | 1954 |
Type | Military Propellor Planes | Passenger Turbo Props |
Icao | B25 | VC1 |
Performance | ||
Engine | 2x Wright R-2600-92 Twin Cyclone | 2x Bristol Hercules 634 |
Power, hp (hp) | 1,700 | 1,690 |
Max cruise speed (km/h) | 437 | 424 |
Approach speed (km/h) | 148 | - |
Travel range (km) | 2,167 | 2,778 |
Service ceiling (m) | 7,376 | 7,620 |
Rate of climb (m/sec) | 5.08 | 7.62 |
Take off distance (m) | - | 780 |
Landing distance (m) | - | 1,200 |
Weights | ||
Max take off weight (kg) | 15,876 | 15,422 |
Max payload (kg) | 3,060 | 2,500 |
Fuel tank capacity (l) | 3,687 | 3,369 |
Dimensions | ||
Seats | 5 | 26 |
Exterior length (m) | 16.13 | 19.86 |
Tail height (m) | 4.98 | 5.97 |
Fuselage diameter (m) | 1.4 | 2.6 |
Wing span (m) | 20.6 | 27.2 |
Wing tips | No Winglets | No Winglets |