Lockheed Martin C-130J Super Hercules vs. Airbus H225 Super Puma

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Lockheed Martin C-130J Super Hercules versus Airbus H225 Super Puma
34.37 m 112 ft 9 in length 14.06 m 46 ft 2 in
11.86 m 38 ft 11 in height 4.38 m 14 ft 4 in
40.41 m 132 ft 7 in wingspan
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 4,700 hp per engine thrust per engine 2,778 hp
Approximately 18,800 hp total total thrust 5,556 hp
76,610 kg 168,900 lb MTOW 11,000 kg 24,251 lb
4,600 km 2,485 nm range 857 km 463 nm
660 km/h 410 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.