Airbus A330-300 vs. Lockheed U-2

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Airbus A330-300 versus Lockheed U-2
63.66 m 208 ft 9 in length 19.2 m 63 ft 0 in
16.79 m 55 ft 1 in height 4.8 m 15 ft 9 in
60.3 m 197 ft 9 in wingspan 32 m 105 ft
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 1 × General Electric F118-101
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 17,000 lbf (76 kN)
Depends on the engine type total thrust 17,000 lbf (76 kN)
242,000 kg 533,600 lb MTOW 18,144 kg 40,000 lb
11,750 km 6,346 nm range 6,090 nm 11,278 km
900 km/h 559 mph cruise speed 475 mph 764 km/h
250-290 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.