Airbus A380-800 vs. Lockheed U-2

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Airbus A380-800 versus Lockheed U-2
72.72 m 238 ft 7 in length 19.2 m 63 ft 0 in
24.09 m 79 ft height 4.8 m 15 ft 9 in
79.75 m 261 ft 8 in wingspan 32 m 105 ft
4 engines 1 × General Electric F118-101
70000lbs thrust per engine 17,000 lbf (76 kN)
280000lbs total thrust 17,000 lbf (76 kN)
560,000 kg 1,234,600 lb MTOW 18,144 kg 40,000 lb
14,800 km 8,000 nm range 6,090 nm 11,278 km
1,050 km/h 652 mph cruise speed 475 mph 764 km/h
525-853 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.