Douglas DC-8 vs. Lockheed Martin C-130J Super Hercules

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Douglas DC-8 versus Lockheed Martin C-130J Super Hercules
57.10 m 187 ft 4 in length 34.37 m 112 ft 9 in
16.84 m 55 ft 3 in height 11.86 m 38 ft 11 in
45.24 m 148 ft 5 in wingspan 40.41 m 132 ft 7 in
4 x Pratt & Whitney JT3D turbofan engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 17,000 lbf per engine thrust per engine Approximately 4,700 hp per engine
Approximately 68,000 lbf total total thrust Approximately 18,800 hp total
158,760 kg 350,000 lb MTOW 76,610 kg 168,900 lb
11,918 km 6,437 nm range 4,600 km 2,485 nm
900 km/h 559 mph cruise speed 660 km/h 410 mph
Up to 259 passengers 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.