Attribute | ![]() North American B-25 Mitchell × | ![]() Douglas DC-3 × |
---|---|---|
General | ||
Manufacturer | North American Aviation NAA | Douglas Aircraft Co. |
Model | North American B-25 Mitchell | Douglas DC-3 |
Country | United States | United States |
Manufactured from (year) | 1940 | 1935 |
Manufactured to (year) | 1945 | 1942 |
Type | Military Propellor Planes | Passenger Turbo Props |
Icao | B25 | DC3 |
Performance | ||
Engine | 2x Wright R-2600-92 Twin Cyclone | 2x Pratt & Whitney R-1830-S1C3G Twin Wasp |
Power, hp (hp) | 1,700 | 1,200 |
Max cruise speed (km/h) | 437 | 370 |
Approach speed (km/h) | 148 | - |
Travel range (km) | 2,167 | 3,500 |
Service ceiling (m) | 7,376 | 7,315 |
Rate of climb (m/sec) | 5.08 | 5.74 |
Weights | ||
Max take off weight (kg) | 15,876 | 13,605 |
Max payload (kg) | 3,060 | 2,725 |
Fuel tank capacity (l) | 3,687 | 3,112 |
Dimensions | ||
Seats | 5 | 32 |
Cabin height (m) | - | 1.5 |
Cabin width (m) | - | 1.7 |
Cabin length (m) | - | 9.1 |
Exterior length (m) | 16.13 | 19.6 |
Tail height (m) | 4.98 | 4.1 |
Fuselage diameter (m) | 1.4 | 2 |
Wing span (m) | 20.6 | 29 |
Wing tips | No Winglets | No Winglets |