Attribute | North American B-25 Mitchell × | Martin 2-0-2 × |
---|---|---|
General | ||
Manufacturer | North American Aviation NAA | Glenn L. Martin Company |
Model | North American B-25 Mitchell | Martin 2-0-2 |
Country | United States | United States |
Manufactured from (year) | 1940 | 1946 |
Manufactured to (year) | 1945 | 1948 |
Type | Military Propellor Planes | Passenger Turbo Props |
Icao | B25 | - |
Performance | ||
Engine | 2x Wright R-2600-92 Twin Cyclone | 2x Pratt & Whitney R-2800 CA-18 Double Wasp |
Power, hp (hp) | 1,700 | 2,400 |
Max cruise speed (km/h) | 437 | 500 |
Approach speed (km/h) | 148 | 122 |
Travel range (km) | 2,167 | 1,022 |
Service ceiling (m) | 7,376 | 10,058 |
Rate of climb (m/sec) | 5.08 | 11.18 |
Take off distance (m) | - | 477 |
Landing distance (m) | - | 520 |
Weights | ||
Max take off weight (kg) | 15,876 | 18,098 |
1↑Max payload (kg) | 3,060 | 4,200 |
Fuel tank capacity (l) | 3,687 | 6,587 |
Dimensions | ||
Seats | 5 | 4 |
Exterior length (m) | 16.13 | 21.74 |
Tail height (m) | 4.98 | 8.66 |
Fuselage diameter (m) | 1.4 | 2.8 |
Wing span (m) | 20.6 | 28.42 |
Wing tips | No Winglets | No Winglets |