Airbus A300-600F vs. Lockheed Martin C-130J Super Hercules

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Airbus A300-600F versus Lockheed Martin C-130J Super Hercules
54.08 m 177 ft 5 in length 34.37 m 112 ft 9 in
17.05 m 55 ft 11 in height 11.86 m 38 ft 11 in
44.84 m 147 ft 1 in wingspan 40.41 m 132 ft 7 in
2 x General Electric CF6-80C2A5 turbofan engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 59,000 lbf per engine thrust per engine Approximately 4,700 hp per engine
Approximately 118,000 lbf total total thrust Approximately 18,800 hp total
170,000 kg 374,786 lb MTOW 76,610 kg 168,900 lb
4,830 km 2,608 nm range 4,600 km 2,485 nm
860 km/h 534 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.