North American B-25 Mitchell vs. Airbus A380-800F

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North American B-25 Mitchell versus Airbus A380-800F
16.15 m 53 ft 0 in length 72.73 m 238 ft 7 in
5 m 16 ft 4 in height 24.09 m 79 ft
20.58 m 67 ft 6 in wingspan 79.75 m 261 ft 8 in
2 x Wright R-2600-92 Twin Cyclone engines 4 x Engine Alliance GP7200 turbofan engines
1,700 horsepower thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
3,400 horsepower total thrust 280,000 to 320,000 pounds
7,484 kg 16,500 lb MTOW 590,000 kg 1,300,733 lb
1,350 mi 1,175 nm range 14,800 km 7,992 nm
233 MPH 375 km/h cruise speed 903 km/h 561 mph
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.