Antonov An-225 Mriya vs. Mil Mi-26

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Antonov An-225 Mriya versus Mil Mi-26
84.0 m 275 ft 7 in length 40.03 m 131.3 ft
18.1 m 59 ft 5 in height 8.15 m 26.7 ft
88.4 m 290 ft 2 in wingspan
6 x Ivchenko Progress D-18T turbofan engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 23,400 kgf per engine thrust per engine 8,380 kW
Approximately 140,400 kgf total total thrust 16,760 kW
640,000 kg 1,411,200 lb MTOW 56,000 kg 123,459 lb
15,400 km 8,315 nm range 800 km 432 nm
800 km/h 497 mph cruise speed 255 km/h 158 mph
based on configuration 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.