lockheed C-130 hercules vs. Mil Mi-26

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lockheed C-130 hercules versus Mil Mi-26
29.79 m 97 ft 9 in length 40.03 m 131.3 ft
11.66 m 38 ft 3 in height 8.15 m 26.7 ft
40.41 m 132 ft 7 in wingspan
4 x Allison T56-A-15 turboprop engines engines 2 x Lotarev D-136 turboshaft engines
Approximately 4,590 hp per engine thrust per engine 8,380 kW
Approximately 18,360 hp total total thrust 16,760 kW
70,307 kg 155,000 lb MTOW 56,000 kg 123,459 lb
3,760 km 2,031 nm range 800 km 432 nm
540 km/h 335 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.