Airbus A320-200 vs. Lockheed U-2

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Airbus A320-200 versus Lockheed U-2
38.7 m 127 ft 0 in length 19.2 m 63 ft 0 in
17.4 m 57 ft 1 in height 4.8 m 15 ft 9 in
35.8 m 117 ft 5 in wingspan 32 m 105 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 × General Electric F118-101
Between 21,000 - 33,000 lbf thrust per engine 17,000 lbf (76 kN)
Between 42,000 - 66,000 lbf total thrust 17,000 lbf (76 kN)
77,000 kg 169,800 lb MTOW 18,144 kg 40,000 lb
5,700 km 3,078 nm range 6,090 nm 11,278 km
530 mph 853 km/h cruise speed 475 mph 764 km/h
Typically between 140-180 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.