Antonov An-124 Ruslan vs. Mil Mi-26

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Antonov An-124 Ruslan versus Mil Mi-26
69.10 m 226 ft 9 in length 40.03 m 131.3 ft
20.78 m 68 ft 2 in height 8.15 m 26.7 ft
73.3 m 240 ft 6 in wingspan
4 x Ivchenko Progress D-18T turbofan engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 51,590 lbf thrust per engine 8,380 kW
Approximately 206,360 lbf total thrust 16,760 kW
405,000 kg 893,000 lb MTOW 56,000 kg 123,459 lb
3,700 km 1,998 nm range 800 km 432 nm
800 km/h 497 mph 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.