Douglas C-54 Skymaster vs. Lockheed Martin C-130J Super Hercules

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Douglas C-54 Skymaster versus Lockheed Martin C-130J Super Hercules
28.60 m 93 ft 10 in length 34.37 m 112 ft 9 in
8.38 m 27 ft 6 in height 11.86 m 38 ft 11 in
35.81 m 117 ft 6 in wingspan 40.41 m 132 ft 7 in
4 x Pratt & Whitney R-2000 Twin Wasp radial engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
1,200 to 1,450 horsepower (895 to 1,080 kW) thrust per engine Approximately 4,700 hp per engine
4,800 to 5,800 horsepower total thrust Approximately 18,800 hp total
29,484 kg 65,000 lb MTOW 76,610 kg 168,900 lb
6,500 km 3,510 nm range 4,600 km 2,485 nm
340 km/h 211 mph cruise speed 660 km/h 410 mph
Up to 50 passengers or 28,500 lb cargo capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.