Airbus A340-200 vs. Lockheed U-2

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Airbus A340-200 versus Lockheed U-2
59.4 m 194 ft 11 in length 19.2 m 63 ft 0 in
16.8 m 55 ft 1 in height 4.8 m 15 ft 9 in
60.3 m 197 ft 9 in wingspan 32 m 105 ft
4 x CFM International CFM56-5C4 engines 1 × General Electric F118-101
34,000 lbf thrust per engine 17,000 lbf (76 kN)
136,000 lbf total thrust 17,000 lbf (76 kN)
275,000 kg 606,300 lb MTOW 18,144 kg 40,000 lb
12,400 km 6,699 nm range 6,090 nm 11,278 km
880 km/h 547 mph cruise speed 475 mph 764 km/h
Typical seating 3-class 210-250 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.