Airbus A321-200 vs. North American B-25 Mitchell
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Airbus A321-200 |
versus |
North American B-25 Mitchell |
44.51 m |
146 ft 0 in |
length |
16.15 m |
53 ft 0 in |
11.76 m |
38 ft 7 in |
height |
5 m |
16 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
20.58 m |
67 ft 6 in |
2 GE CFM56-5B3 |
engines |
2 x Wright R-2600-92 Twin Cyclone |
31,600 lbs |
thrust per engine |
1,700 horsepower |
63,200 lbs |
total thrust |
3,400 horsepower |
89,000 kg |
196,200 lb |
MTOW |
7,484 kg |
16,500 lb |
4,000 nmi |
7,408 km |
range |
1,350 mi |
1,175 nm |
871 km/h |
541 mph |
cruise speed |
233 MPH |
375 km/h |
185 to 220 |
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.