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

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Airbus A300-600 versus Lockheed Martin C-130J Super Hercules
54.10 m 177 ft 6 in length 34.37 m 112 ft 9 in
16.5 m 54 ft 2 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 turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
56,000lb to 61,500lb thrust per engine Approximately 4,700 hp per engine
112,000–123,000 lb total thrust Approximately 18,800 hp total
171,700 kg 378,600 lb MTOW 76,610 kg 168,900 lb
7,500 km 4,052 nm range 4,600 km 2,485 nm
897 km/h 557 mph cruise speed 660 km/h 410 mph
210-250 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.