Airbus A350-1000 vs. Lockheed U-2
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Airbus A350-1000 |
versus |
Lockheed U-2 |
73.79 m |
242 ft 1 in |
length |
19.2 m |
63 ft 0 in |
17.08 m |
56 ft |
height |
4.8 m |
15 ft 9 in |
64.75 m |
212 ft 5 in |
wingspan |
32 m |
105 ft |
2 Trent XWB-97 turbofan engines |
engines |
1 × General Electric F118-101 |
97,000 lb |
thrust per engine |
17,000 lbf (76 kN) |
194,000 lb |
total thrust |
17,000 lbf (76 kN) |
319,000 kg |
703,300 lb |
MTOW |
18,144 kg |
40,000 lb |
16,100 km |
8,695 nm |
range |
6,090 nm |
11,278 km |
1,099 km/h |
683 mph |
cruise speed |
475 mph |
764 km/h |
350 to 410 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.