Antonov An-225 Mriya vs. Airbus H225 Super Puma

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Antonov An-225 Mriya versus Airbus H225 Super Puma
84.0 m 275 ft 7 in length 14.06 m 46 ft 2 in
18.1 m 59 ft 5 in height 4.38 m 14 ft 4 in
88.4 m 290 ft 2 in wingspan
6 x Ivchenko Progress D-18T turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 23,400 kgf per engine thrust per engine 2,778 hp
Approximately 140,400 kgf total total thrust 5,556 hp
640,000 kg 1,411,200 lb MTOW 11,000 kg 24,251 lb
15,400 km 8,315 nm range 857 km 463 nm
800 km/h 497 mph cruise speed 242 km/h 150 mph
based on configuration 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.