Airbus A321neo vs. Lockheed Martin F-35 Lightning II

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Airbus A321neo versus Lockheed Martin F-35 Lightning II
44.51 m 146 ft 0 in length 15.67 m 51 ft 4 in
11.76 m 38 ft 7 in height 4.33 m 14 ft 2 in
35.8 m 117 ft 5 in wingspan 10.7 m 35 ft 1 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
35,000 lb thrust per engine 40,000 lb
70,000 lb total thrust 40,000 lb
97,000 kg 213,800 lb MTOW 31,800 kg 70,000 lb
7,400 km 4,000 nm range 1,380 mi 1,200 nm
828 km/h 514 mph cruise speed 520 kt 302 mph
180 to 220 passengers capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.