Airbus A321neo vs. Lockheed Martin C-130J Super Hercules

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Airbus A321neo 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 4 x Rolls-Royce AE 2100D3 turboprop engines
35,000 lb thrust per engine Approximately 4,700 hp per engine
70,000 lb total thrust Approximately 18,800 hp total
97,000 kg 213,800 lb MTOW 76,610 kg 168,900 lb
7,400 km 4,000 nm range 4,600 km 2,485 nm
828 km/h 514 mph cruise speed 660 km/h 410 mph
180 to 220 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.