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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.