Airbus A321-200 vs. lockheed C-130 hercules

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Airbus A321-200 versus lockheed C-130 hercules
44.51 m 146 ft 0 in length 29.79 m 97 ft 9 in
11.76 m 38 ft 7 in height 11.66 m 38 ft 3 in
35.8 m 117 ft 5 in wingspan 40.41 m 132 ft 7 in
2 GE CFM56-5B3 engines 4 x Allison T56-A-15 turboprop engines
31,600 lbs thrust per engine Approximately 4,590 hp per engine
63,200 lbs total thrust Approximately 18,360 hp total
89,000 kg 196,200 lb MTOW 70,307 kg 155,000 lb
4,000 nmi 7,408 km range 3,760 km 2,031 nm
871 km/h 541 mph cruise speed 540 km/h 335 mph
185 to 220 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.