Airbus A350-1000 vs. Lockheed U-2

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Airbus A350-1000 versus Lockheed U-2
73.79 m 242 ft 1 in length 19.2 m 63 ft 0 in
17.08 m 56 ft height 4.8 m 15 ft 9 in
64.75 m 212 ft 5 in wingspan 32 m 105 ft
2 Trent XWB-97 turbofan engines engines 1 × General Electric F118-101
97,000 lb thrust per engine 17,000 lbf (76 kN)
194,000 lb total thrust 17,000 lbf (76 kN)
319,000 kg 703,300 lb MTOW 18,144 kg 40,000 lb
16,100 km 8,695 nm range 6,090 nm 11,278 km
1,099 km/h 683 mph cruise speed 475 mph 764 km/h
350 to 410 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.