Airbus A340-300X vs. Lockheed U-2

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Airbus A340-300X versus Lockheed U-2
63.60 m 208 ft 6 in length 19.2 m 63 ft 0 in
16.7 m 54 ft 9 in height 4.8 m 15 ft 9 in
60.3 m 197 ft 9 in wingspan 32 m 105 ft
4 Turbofan Engines engines 1 × General Electric F118-101
151.2 kN thrust per engine 17,000 lbf (76 kN)
604.8 kN total thrust 17,000 lbf (76 kN)
275,000 kg 606,300 lb MTOW 18,144 kg 40,000 lb
13,699 km 7,403 nm range 6,090 nm 11,278 km
915 km/h 569 mph cruise speed 475 mph 764 km/h
295 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.