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 |
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capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.