Lockheed C-5 Galaxy vs. Airbus H225 Super Puma

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Lockheed C-5 Galaxy versus Airbus H225 Super Puma
75.31 m 247 ft 2 in length 14.06 m 46 ft 2 in
19.84 m 65 ft 1 in height 4.38 m 14 ft 4 in
67.89 m 222 ft 9 in wingspan
4 x General Electric TF39 turbofan engines engines 2 x Turbomeca Makila 2A turboshaft engines
41,000 pounds of thrust (182 kilonewtons) thrust per engine 2,778 hp
164,000 pounds total thrust 5,556 hp
381,018 kg 840,000 lb MTOW 11,000 kg 24,251 lb
8,000 km 4,320 nm range 857 km 463 nm
908 km/h 564 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.