Airbus A330-300 vs. Lockheed Martin C-130J Super Hercules

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Airbus A330-300 versus Lockheed Martin C-130J Super Hercules
63.66 m 208 ft 9 in length 34.37 m 112 ft 9 in
16.79 m 55 ft 1 in height 11.86 m 38 ft 11 in
60.3 m 197 ft 9 in wingspan 40.41 m 132 ft 7 in
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine Approximately 4,700 hp per engine
Depends on the engine type total thrust Approximately 18,800 hp total
242,000 kg 533,600 lb MTOW 76,610 kg 168,900 lb
11,750 km 6,346 nm range 4,600 km 2,485 nm
900 km/h 559 mph cruise speed 660 km/h 410 mph
250-290 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.