Airbus A320-200 vs. Lockheed Martin F-35 Lightning II

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Airbus A320-200 versus Lockheed Martin F-35 Lightning II
38.7 m 127 ft 0 in length 15.67 m 51 ft 4 in
17.4 m 57 ft 1 in height 4.33 m 14 ft 2 in
35.8 m 117 ft 5 in wingspan 10.7 m 35 ft 1 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
Between 21,000 - 33,000 lbf thrust per engine 40,000 lb
Between 42,000 - 66,000 lbf total thrust 40,000 lb
77,000 kg 169,800 lb MTOW 31,800 kg 70,000 lb
5,700 km 3,078 nm range 1,380 mi 1,200 nm
530 mph 853 km/h cruise speed 520 kt 302 mph
Typically between 140-180 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.