Lockheed U-2 vs. Antonov An-225 Mriya

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Lockheed U-2 versus Antonov An-225 Mriya
19.2 m 63 ft 0 in length 84.0 m 275 ft 7 in
4.8 m 15 ft 9 in height 18.1 m 59 ft 5 in
32 m 105 ft wingspan 88.4 m 290 ft 2 in
1 × General Electric F118-101 engines 6 x Ivchenko Progress D-18T turbofan engines
17,000 lbf (76 kN) thrust per engine Approximately 23,400 kgf per engine
17,000 lbf (76 kN) total thrust Approximately 140,400 kgf total
18,144 kg 40,000 lb MTOW 640,000 kg 1,411,200 lb
6,090 nm 11,278 km range 15,400 km 8,315 nm
475 mph 764 km/h cruise speed 800 km/h 497 mph
capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.