Lockheed U-2 vs. Airbus A380-800F

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Lockheed U-2 versus Airbus A380-800F
19.2 m 63 ft 0 in length 72.73 m 238 ft 7 in
4.8 m 15 ft 9 in height 24.09 m 79 ft
32 m 105 ft wingspan 79.75 m 261 ft 8 in
1 × General Electric F118-101 engines 4 x Engine Alliance GP7200 turbofan engines
17,000 lbf (76 kN) thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
17,000 lbf (76 kN) total thrust 280,000 to 320,000 pounds
18,144 kg 40,000 lb MTOW 590,000 kg 1,300,733 lb
6,090 nm 11,278 km range 14,800 km 7,992 nm
475 mph 764 km/h cruise speed 903 km/h 561 mph
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.