Antonov An-124 Ruslan vs. Airbus H225 Super Puma

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Antonov An-124 Ruslan versus Airbus H225 Super Puma
69.10 m 226 ft 9 in length 14.06 m 46 ft 2 in
20.78 m 68 ft 2 in height 4.38 m 14 ft 4 in
73.3 m 240 ft 6 in wingspan
4 x Ivchenko Progress D-18T turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 51,590 lbf thrust per engine 2,778 hp
Approximately 206,360 lbf total thrust 5,556 hp
405,000 kg 893,000 lb MTOW 11,000 kg 24,251 lb
3,700 km 1,998 nm range 857 km 463 nm
800 km/h 497 mph cruise speed 242 km/h 150 mph
capacity 24-28
rotor diameter 16.2 m 53 ft 2 in
rate of climb 10.7 m/s 2,106 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.