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

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Airbus A380-800 versus Lockheed Martin C-130J Super Hercules
72.72 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 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
70000lbs thrust per engine Approximately 4,700 hp per engine
280000lbs total thrust Approximately 18,800 hp total
560,000 kg 1,234,600 lb MTOW 76,610 kg 168,900 lb
14,800 km 8,000 nm range 4,600 km 2,485 nm
1,050 km/h 652 mph cruise speed 660 km/h 410 mph
525-853 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.