Airbus A330-300 vs. North American B-25 Mitchell
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Airbus A330-300 |
versus |
North American B-25 Mitchell |
63.66 m |
208 ft 9 in |
length |
16.15 m |
53 ft 0 in |
16.79 m |
55 ft 1 in |
height |
5 m |
16 ft 4 in |
60.3 m |
197 ft 9 in |
wingspan |
20.58 m |
67 ft 6 in |
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
2 x Wright R-2600-92 Twin Cyclone |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
1,700 horsepower |
Depends on the engine type |
total thrust |
3,400 horsepower |
242,000 kg |
533,600 lb |
MTOW |
7,484 kg |
16,500 lb |
11,750 km |
6,346 nm |
range |
1,350 mi |
1,175 nm |
900 km/h |
559 mph |
cruise speed |
233 MPH |
375 km/h |
250-290 |
capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.