McDonnell-Douglas DC-10-30 vs. Lockheed Martin C-130J Super Hercules

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McDonnell-Douglas DC-10-30 versus Lockheed Martin C-130J Super Hercules
55.35 m 181 ft 8 in length 34.37 m 112 ft 9 in
17.8 m 58 ft 5 in height 11.86 m 38 ft 11 in
50.39 m 165 ft 4 in wingspan 40.41 m 132 ft 7 in
3x GE CF6-50C Turbofan engines 4 x Rolls-Royce AE 2100D3 turboprop engines
54,000 lbf thrust per engine Approximately 4,700 hp per engine
162,000 lbf total thrust Approximately 18,800 hp total
251,744 kg 555,000 lb MTOW 76,610 kg 168,900 lb
9,630 km 5,200 nm range 4,600 km 2,485 nm
507 knots 939 km/h cruise speed 660 km/h 410 mph
Up to 380 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.