Airbus A310-300 vs. Lockheed Martin C-130J Super Hercules

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Airbus A310-300 versus Lockheed Martin C-130J Super Hercules
46.66 m 153 ft 1 in length 34.37 m 112 ft 9 in
15.8 m 51 ft 10 in height 11.86 m 38 ft 11 in
43.9 m 144 ft wingspan 40.41 m 132 ft 7 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 4 x Rolls-Royce AE 2100D3 turboprop engines
52,000 lb thrust per engine Approximately 4,700 hp per engine
104,000 lb total thrust Approximately 18,800 hp total
148,768 kg 328,000 lb MTOW 76,610 kg 168,900 lb
8,050 km 4,348 nm range 4,600 km 2,485 nm
482 knots 279 mph cruise speed 660 km/h 410 mph
190-230 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.