Airbus A319 vs. Lockheed U-2

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Airbus A319 versus Lockheed U-2
33.84 m 111 ft 0 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 (International Aero Engines V2524-A5) engines 1 × General Electric F118-101
27,000 lb thrust per engine 17,000 lbf (76 kN)
54,000 lb total thrust 17,000 lbf (76 kN)
75,500 kg 166,400 lb MTOW 18,144 kg 40,000 lb
3,700 nmi 6,852 km range 6,090 nm 11,278 km
829 km/h 515 mph cruise speed 475 mph 764 km/h
124 to 156 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.