McDonnell-Douglas DC-9-30 vs. Lockheed Martin C-130J Super Hercules

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McDonnell-Douglas DC-9-30 versus Lockheed Martin C-130J Super Hercules
36.36 m 119 ft 3 in length 34.37 m 112 ft 9 in
8.5 m 27 ft 11 in height 11.86 m 38 ft 11 in
28.44 m 93 ft 4 in wingspan 40.41 m 132 ft 7 in
2x Pratt & Whitney JT8D engines 4 x Rolls-Royce AE 2100D3 turboprop engines
15,000 pound-force thrust per engine Approximately 4,700 hp per engine
30,000 pound-force (2 engines) total thrust Approximately 18,800 hp total
54,885 kg 121,000 lb MTOW 76,610 kg 168,900 lb
2,632 km 1,422 nm range 4,600 km 2,485 nm
898 km/h 558 mph cruise speed 660 km/h 410 mph
Up to 139 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.