Airbus A340-600 vs. Lockheed U-2
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here.
| Airbus A340-600 |
versus |
Lockheed U-2 |
| 75.36 m |
247 ft 3 in |
length |
19.2 m |
63 ft 0 in |
| 17.93 m |
58 ft 10 in |
height |
4.8 m |
15 ft 9 in |
| 63.45 m |
208 ft 2 in |
wingspan |
32 m |
105 ft |
| 4 x Rolls-Royce Trent 556 |
engines |
1 × General Electric F118-101 |
| 56,000 lbs |
thrust per engine |
17,000 lbf (76 kN) |
| 224,000 lbs |
total thrust |
17,000 lbf (76 kN) |
| 380,000 kg |
837,800 lb |
MTOW |
18,144 kg |
40,000 lb |
| 14,450 km |
7,804 nm |
range |
6,090 nm |
11,278 km |
| 890 km/h |
553 mph |
cruise speed |
475 mph |
764 km/h |
| 320-370 |
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.
