Antonov An-225 Mriya vs. Lockheed C-69 Constellation

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Antonov An-225 Mriya versus Lockheed C-69 Constellation
84.0 m 275 ft 7 in length 29.72 m 97 ft 6 in
18.1 m 59 ft 5 in height 6.02 m 19 ft 9 in
88.4 m 290 ft 2 in wingspan 37.49 m 123 ft
6 x Ivchenko Progress D-18T turbofan engines engines 4 x Wright R-3350 Duplex-Cyclone radial engines
Approximately 23,400 kgf per engine thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
Approximately 140,400 kgf total total thrust 8,800 to 14,800 horsepower
640,000 kg 1,411,200 lb MTOW 44,453 kg 98,000 lb
15,400 km 8,315 nm range 5,200 km 2,808 nm
800 km/h 497 mph cruise speed 507 km/h 315 mph
based on configuration capacity Up to 109 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.