Airbus A320neo vs. Lockheed U-2

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Airbus A320neo versus Lockheed U-2
37.57 m 123 ft 3 in length 19.2 m 63 ft 0 in
11.76 m 38 ft 7 in height 4.8 m 15 ft 9 in
35.8 m 117 ft 5 in wingspan 32 m 105 ft
2 x PW 1100G or 2 x CFM LEAP-1A engines 1 × General Electric F118-101
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 17,000 lbf (76 kN)
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 17,000 lbf (76 kN)
79,000 kg 174,200 lb MTOW 18,144 kg 40,000 lb
6,300 km 3,403 nm range 6,090 nm 11,278 km
M0.82 101,3 km/h cruise speed 475 mph 764 km/h
150-180 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.