North American B-25 Mitchell vs. Antonov An-124 Ruslan

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North American B-25 Mitchell versus Antonov An-124 Ruslan
16.15 m 53 ft 0 in length 69.10 m 226 ft 9 in
5 m 16 ft 4 in height 20.78 m 68 ft 2 in
20.58 m 67 ft 6 in wingspan 73.3 m 240 ft 6 in
2 x Wright R-2600-92 Twin Cyclone engines 4 x Ivchenko Progress D-18T turbofan engines
1,700 horsepower thrust per engine Approximately 51,590 lbf
3,400 horsepower total thrust Approximately 206,360 lbf
7,484 kg 16,500 lb MTOW 405,000 kg 893,000 lb
1,350 mi 1,175 nm range 3,700 km 1,998 nm
233 MPH 375 km/h cruise speed 800 km/h 497 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.