de Havilland Venom vs. Lockheed Martin C-130J Super Hercules

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de Havilland Venom versus Lockheed Martin C-130J Super Hercules
6.71 m 22 ft 0 in length 34.37 m 112 ft 9 in
1.88 m 6 ft 2 in height 11.86 m 38 ft 11 in
12.7 m 41 ft 8 in wingspan 40.41 m 132 ft 7 in
1 (de Havilland Ghost 105) engines 4 x Rolls-Royce AE 2100D3 turboprop engines
23.6 kN thrust per engine Approximately 4,700 hp per engine
23.6 kN total thrust Approximately 18,800 hp total
6,945 kg 15,300 lb MTOW 76,610 kg 168,900 lb
1,730 km 935 nm range 4,600 km 2,485 nm
1030 km/h 640 mph cruise speed 660 km/h 410 mph
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.