Airbus A321LR vs. Lockheed Martin C-130J Super Hercules

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Airbus A321LR 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
Over 33,000 lbs (147 kN) thrust per engine Approximately 4,700 hp per engine
66,000 lbs (294 kN) 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
832 km/h 517 mph cruise speed 660 km/h 410 mph
180-220 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.