Airbus A380-800 vs. Lockheed U-2
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Airbus A380-800 |
versus |
Lockheed U-2 |
72.72 m |
238 ft 7 in |
length |
19.2 m |
63 ft 0 in |
24.09 m |
79 ft |
height |
4.8 m |
15 ft 9 in |
79.75 m |
261 ft 8 in |
wingspan |
32 m |
105 ft |
4 |
engines |
1 × General Electric F118-101 |
70000lbs |
thrust per engine |
17,000 lbf (76 kN) |
280000lbs |
total thrust |
17,000 lbf (76 kN) |
560,000 kg |
1,234,600 lb |
MTOW |
18,144 kg |
40,000 lb |
14,800 km |
8,000 nm |
range |
6,090 nm |
11,278 km |
1,050 km/h |
652 mph |
cruise speed |
475 mph |
764 km/h |
525-853 passengers |
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.