North American B-25 Mitchell vs. Mil Mi-26

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North American B-25 Mitchell versus Mil Mi-26
16.15 m 53 ft 0 in length 40.03 m 131.3 ft
5 m 16 ft 4 in height 8.15 m 26.7 ft
20.58 m 67 ft 6 in wingspan
2 x Wright R-2600-92 Twin Cyclone engines 2 x Lotarev D-136 turboshaft engines
1,700 horsepower thrust per engine 8,380 kW
3,400 horsepower total thrust 16,760 kW
7,484 kg 16,500 lb MTOW 56,000 kg 123,459 lb
1,350 mi 1,175 nm range 800 km 432 nm
233 MPH 375 km/h cruise speed 255 km/h 158 mph
capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.