Airbus A330-200 vs. Lockheed Martin C-130J Super Hercules

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Airbus A330-200 versus Lockheed Martin C-130J Super Hercules
58.82 m 193 ft 0 in length 34.37 m 112 ft 9 in
17.39 m 57 ft 1 in height 11.86 m 38 ft 11 in
64 m 210 ft wingspan 40.41 m 132 ft 7 in
2 Turbofans engines 4 x Rolls-Royce AE 2100D3 turboprop engines
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine Approximately 4,700 hp per engine
Depends on the engine variant total thrust Approximately 18,800 hp total
251,000 kg 553,400 lb MTOW 76,610 kg 168,900 lb
15,094 km 8,150 nm range 4,600 km 2,485 nm
531 mph 855 km/h cruise speed 660 km/h 410 mph
220-260 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.