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

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Airbus A380-800 versus North American B-25 Mitchell
72.72 m 238 ft 7 in length 16.15 m 53 ft 0 in
24.09 m 79 ft height 5 m 16 ft 4 in
79.75 m 261 ft 8 in wingspan 20.58 m 67 ft 6 in
4 engines 2 x Wright R-2600-92 Twin Cyclone
70000lbs thrust per engine 1,700 horsepower
280000lbs total thrust 3,400 horsepower
560,000 kg 1,234,600 lb MTOW 7,484 kg 16,500 lb
14,800 km 8,000 nm range 1,350 mi 1,175 nm
1,050 km/h 652 mph cruise speed 233 MPH 375 km/h
525-853 passengers 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.