Airbus A350-900ULR vs. Lockheed U-2

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Airbus A350-900ULR 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)
280,000 kg 617,300 lb MTOW 18,144 kg 40,000 lb
17,964 km 9,700 nm range 6,090 nm 11,278 km
552 mph 888 km/h cruise speed 475 mph 764 km/h
300-350 passengers in three classes 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.