Airbus A320-200 vs. Lockheed Martin C-130J Super Hercules

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Airbus A320-200 versus Lockheed Martin C-130J Super Hercules
38.7 m 127 ft 0 in length 34.37 m 112 ft 9 in
17.4 m 57 ft 1 in height 11.86 m 38 ft 11 in
35.8 m 117 ft 5 in wingspan 40.41 m 132 ft 7 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Between 21,000 - 33,000 lbf thrust per engine Approximately 4,700 hp per engine
Between 42,000 - 66,000 lbf total thrust Approximately 18,800 hp total
77,000 kg 169,800 lb MTOW 76,610 kg 168,900 lb
5,700 km 3,078 nm range 4,600 km 2,485 nm
530 mph 853 km/h cruise speed 660 km/h 410 mph
Typically between 140-180 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.