Airbus A321-200 vs. Lockheed U-2

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Airbus A321-200 versus Lockheed U-2
44.51 m 146 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 GE CFM56-5B3 engines 1 × General Electric F118-101
31,600 lbs thrust per engine 17,000 lbf (76 kN)
63,200 lbs total thrust 17,000 lbf (76 kN)
89,000 kg 196,200 lb MTOW 18,144 kg 40,000 lb
4,000 nmi 7,408 km range 6,090 nm 11,278 km
871 km/h 541 mph cruise speed 475 mph 764 km/h
185 to 220 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.