Airbus A380-800F vs. Lockheed Martin C-130J Super Hercules

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Airbus A380-800F versus Lockheed Martin C-130J Super Hercules
72.73 m 238 ft 7 in length 34.37 m 112 ft 9 in
24.09 m 79 ft height 11.86 m 38 ft 11 in
79.75 m 261 ft 8 in wingspan 40.41 m 132 ft 7 in
4 x Engine Alliance GP7200 turbofan engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons) thrust per engine Approximately 4,700 hp per engine
280,000 to 320,000 pounds total thrust Approximately 18,800 hp total
590,000 kg 1,300,733 lb MTOW 76,610 kg 168,900 lb
14,800 km 7,992 nm range 4,600 km 2,485 nm
903 km/h 561 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.