Lockheed U-2 vs. Antonov An-124 Ruslan

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Lockheed U-2 versus Antonov An-124 Ruslan
19.2 m 63 ft 0 in length 69.10 m 226 ft 9 in
4.8 m 15 ft 9 in height 20.78 m 68 ft 2 in
32 m 105 ft wingspan 73.3 m 240 ft 6 in
1 × General Electric F118-101 engines 4 x Ivchenko Progress D-18T turbofan engines
17,000 lbf (76 kN) thrust per engine Approximately 51,590 lbf
17,000 lbf (76 kN) total thrust Approximately 206,360 lbf
18,144 kg 40,000 lb MTOW 405,000 kg 893,000 lb
6,090 nm 11,278 km range 3,700 km 1,998 nm
475 mph 764 km/h cruise speed 800 km/h 497 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.