Airbus A330-200 vs. lockheed C-130 hercules

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Airbus A330-200 versus lockheed C-130 hercules
58.82 m 193 ft 0 in length 29.79 m 97 ft 9 in
17.39 m 57 ft 1 in height 11.66 m 38 ft 3 in
64 m 210 ft wingspan 40.41 m 132 ft 7 in
2 Turbofans engines 4 x Allison T56-A-15 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 4,590 hp per engine
Depends on the engine variant total thrust Approximately 18,360 hp total
251,000 kg 553,400 lb MTOW 70,307 kg 155,000 lb
15,094 km 8,150 nm range 3,760 km 2,031 nm
531 mph 855 km/h cruise speed 540 km/h 335 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.