Lockheed Martin C-130J Super Hercules vs. Mil Mi-26

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Lockheed Martin C-130J Super Hercules versus Mil Mi-26
34.37 m 112 ft 9 in length 40.03 m 131.3 ft
11.86 m 38 ft 11 in height 8.15 m 26.7 ft
40.41 m 132 ft 7 in wingspan
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 4,700 hp per engine thrust per engine 8,380 kW
Approximately 18,800 hp total total thrust 16,760 kW
76,610 kg 168,900 lb MTOW 56,000 kg 123,459 lb
4,600 km 2,485 nm range 800 km 432 nm
660 km/h 410 mph cruise speed 255 km/h 158 mph
based on configuration capacity Up to 90 passengers
rotor diameter 32.00 m 105 ft 0 in
rate of climb 8 m/s 1,574 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.