Airbus A320neo vs. Lockheed Martin F-35 Lightning II

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Airbus A320neo versus Lockheed Martin F-35 Lightning II
37.57 m 123 ft 3 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
2 x PW 1100G or 2 x CFM LEAP-1A engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 40,000 lb
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 40,000 lb
79,000 kg 174,200 lb MTOW 31,800 kg 70,000 lb
6,300 km 3,403 nm range 1,380 mi 1,200 nm
M0.82 101,3 km/h cruise speed 520 kt 302 mph
150-180 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.