Airbus A340-300X vs. Lockheed U-2
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Airbus A340-300X |
versus |
Lockheed U-2 |
63.60 m |
208 ft 6 in |
length |
19.2 m |
63 ft 0 in |
16.7 m |
54 ft 9 in |
height |
4.8 m |
15 ft 9 in |
60.3 m |
197 ft 9 in |
wingspan |
32 m |
105 ft |
4 Turbofan Engines |
engines |
1 × General Electric F118-101 |
151.2 kN |
thrust per engine |
17,000 lbf (76 kN) |
604.8 kN |
total thrust |
17,000 lbf (76 kN) |
275,000 kg |
606,300 lb |
MTOW |
18,144 kg |
40,000 lb |
13,699 km |
7,403 nm |
range |
6,090 nm |
11,278 km |
915 km/h |
569 mph |
cruise speed |
475 mph |
764 km/h |
295 |
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.