Airbus A330-200 vs. Lockheed U-2
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Airbus A330-200 |
versus |
Lockheed U-2 |
58.82 m |
193 ft 0 in |
length |
19.2 m |
63 ft 0 in |
17.39 m |
57 ft 1 in |
height |
4.8 m |
15 ft 9 in |
64 m |
210 ft |
wingspan |
32 m |
105 ft |
2 Turbofans |
engines |
1 × General Electric F118-101 |
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf |
thrust per engine |
17,000 lbf (76 kN) |
Depends on the engine variant |
total thrust |
17,000 lbf (76 kN) |
251,000 kg |
553,400 lb |
MTOW |
18,144 kg |
40,000 lb |
15,094 km |
8,150 nm |
range |
6,090 nm |
11,278 km |
531 mph |
855 km/h |
cruise speed |
475 mph |
764 km/h |
220-260 |
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.