Airbus A350-900ULR vs. Lockheed U-2
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Airbus A350-900ULR |
versus |
Lockheed U-2 |
66.80 m |
219 ft 2 in |
length |
19.2 m |
63 ft 0 in |
17.05 m |
55 ft 11 in |
height |
4.8 m |
15 ft 9 in |
64.75 m |
212 ft 5 in |
wingspan |
32 m |
105 ft |
2 Rolls-Royce Trent XWB |
engines |
1 × General Electric F118-101 |
84,000 lbs |
thrust per engine |
17,000 lbf (76 kN) |
168,000 lbs |
total thrust |
17,000 lbf (76 kN) |
280,000 kg |
617,300 lb |
MTOW |
18,144 kg |
40,000 lb |
17,964 km |
9,700 nm |
range |
6,090 nm |
11,278 km |
552 mph |
888 km/h |
cruise speed |
475 mph |
764 km/h |
300-350 passengers in three classes |
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.