Airbus A350-900 vs. Lockheed U-2

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Airbus A350-900 versus Lockheed U-2
66.80 m 219 ft 2 in length 19.2 m 63 ft 0 in
17.05 m 55 ft 11 in height 4.8 m 15 ft 9 in
64.75 m 212 ft 5 in wingspan 32 m 105 ft
2 Rolls-Royce Trent XWB engines 1 × General Electric F118-101
84,000 lbs thrust per engine 17,000 lbf (76 kN)
168,000 lbs total thrust 17,000 lbf (76 kN)
283,000 kg 623,900 lb MTOW 18,144 kg 40,000 lb
15,372 km 8,300 nm range 6,090 nm 11,278 km
888 km/h 552 mph cruise speed 475 mph 764 km/h
300-350 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.