North American BT-9 vs. Mil Mi-26

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North American BT-9 versus Mil Mi-26
8.79 m 28 ft 10 in length 40.03 m 131.3 ft
2.82 m 9 ft 3 in height 8.15 m 26.7 ft
10.97 m 36 ft wingspan
1 x Wright R-975-3 radial engine engines 2 x Lotarev D-136 turboshaft engines
Approximately 440 hp thrust per engine 8,380 kW
Approximately 440 hp total thrust 16,760 kW
4,300 lb 1,950 kg MTOW 56,000 kg 123,459 lb
917 km 495 nm range 800 km 432 nm
150 mph 241 km/h cruise speed 255 km/h 158 mph
Pilot and one passenger 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.