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 |
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capacity |
based on configuration |
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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.