Airbus A320-200 vs. lockheed C-130 hercules

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Airbus A320-200 versus lockheed C-130 hercules
38.7 m 127 ft 0 in length 29.79 m 97 ft 9 in
17.4 m 57 ft 1 in height 11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines
Between 21,000 - 33,000 lbf thrust per engine Approximately 4,590 hp per engine
Between 42,000 - 66,000 lbf total thrust Approximately 18,360 hp total
77,000 kg 169,800 lb MTOW 70,307 kg 155,000 lb
5,700 km 3,078 nm range 3,760 km 2,031 nm
530 mph 853 km/h cruise speed 540 km/h 335 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.