Comparison of North American B-25 Mitchell and Vickers Valetta [S]ave
| Attribute |  North American B-25 Mitchell × |  Vickers Valetta × |
|---|---|---|
| General | ||
| Manufacturer | North American Aviation NAA | Vickers-Armstrongs |
| Model | North American B-25 Mitchell | Vickers Valetta |
| Country | United States | United Kingdom |
| Manufactured from (year) | 1940 | 1947 |
| Manufactured to (year) | 1945 | 1952 |
| Type | Military Propellor Planes | Military Transport Planes |
| Icao | B25 | - |
| Performance | ||
| Engine | 2x Wright R-2600-92 Twin Cyclone | 2x Bristol Hercules 230 |
| Power, hp (hp) | 1,700 | 2,000 |
| Max cruise speed (km/h) | 437 | 415 |
| Approach speed (km/h) | 148 | - |
| Travel range (km) | 2,167 | 2,352 |
| Service ceiling (m) | 7,376 | 6,553 |
| Rate of climb (m/sec) | 5.08 | 6.48 |
| Take off distance (m) | - | 1,140 |
| Landing distance (m) | - | 1,300 |
| Weights | ||
| Max take off weight (kg) | 15,876 | 16,556 |
| Max payload (kg) | 3,060 | 2,860 |
| Fuel tank capacity (l) | 3,687 | 3,290 |
| Dimensions | ||
| Seats | 5 | 38 |
| Exterior length (m) | 16.13 | 19.18 |
| Tail height (m) | 4.98 | 5.97 |
| 1↑Fuselage diameter (m) | 1.4 | 2.7 |
| Wing span (m) | 20.6 | 27.2 |
| Wing tips | No Winglets | No Winglets |
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