Airbus A321-200 vs. Lockheed Martin C-130J Super Hercules

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Airbus A321-200 versus Lockheed Martin C-130J Super Hercules
44.51 m 146 ft 0 in length 34.37 m 112 ft 9 in
11.76 m 38 ft 7 in height 11.86 m 38 ft 11 in
35.8 m 117 ft 5 in wingspan 40.41 m 132 ft 7 in
2 GE CFM56-5B3 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
31,600 lbs thrust per engine Approximately 4,700 hp per engine
63,200 lbs total thrust Approximately 18,800 hp total
89,000 kg 196,200 lb MTOW 76,610 kg 168,900 lb
4,000 nmi 7,408 km range 4,600 km 2,485 nm
871 km/h 541 mph cruise speed 660 km/h 410 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.