Airbus A300-600 vs. lockheed C-130 hercules

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Airbus A300-600 versus lockheed C-130 hercules
54.10 m 177 ft 6 in length 29.79 m 97 ft 9 in
16.5 m 54 ft 2 in height 11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines
56,000lb to 61,500lb thrust per engine Approximately 4,590 hp per engine
112,000–123,000 lb total thrust Approximately 18,360 hp total
171,700 kg 378,600 lb MTOW 70,307 kg 155,000 lb
7,500 km 4,052 nm range 3,760 km 2,031 nm
897 km/h 557 mph cruise speed 540 km/h 335 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.