Antonov An-124 Ruslan vs. Lockheed C-69 Constellation

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Antonov An-124 Ruslan versus Lockheed C-69 Constellation
69.10 m 226 ft 9 in length 29.72 m 97 ft 6 in
20.78 m 68 ft 2 in height 6.02 m 19 ft 9 in
73.3 m 240 ft 6 in wingspan 37.49 m 123 ft
4 x Ivchenko Progress D-18T turbofan engines engines 4 x Wright R-3350 Duplex-Cyclone radial engines
Approximately 51,590 lbf thrust per engine 2,200 to 3,700 horsepower (1,640 to 2,760 kW)
Approximately 206,360 lbf total thrust 8,800 to 14,800 horsepower
405,000 kg 893,000 lb MTOW 44,453 kg 98,000 lb
3,700 km 1,998 nm range 5,200 km 2,808 nm
800 km/h 497 mph cruise speed 507 km/h 315 mph
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.