Airbus A350-800 vs. Lockheed U-2

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Airbus A350-800 versus Lockheed U-2
60.54 m 198 ft 7 in length 19.2 m 63 ft 0 in
17.05 m 55 ft 11 in height 4.8 m 15 ft 9 in
64.7 m 212 ft 5 in wingspan 32 m 105 ft
2 Turbofans (wing mounted) engines 1 × General Electric F118-101
75,760 lb thrust per engine 17,000 lbf (76 kN)
151,520 lb total thrust 17,000 lbf (76 kN)
283,000 kg 623,900 lb MTOW 18,144 kg 40,000 lb
11,708 km 6,319 nm range 6,090 nm 11,278 km
552 mph 888 km/h cruise speed 475 mph 764 km/h
Typically carries 300 to 350 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.