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