Airbus A340-500 vs. Lockheed U-2

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Airbus A340-500 versus Lockheed U-2
67.93 m 222 ft 10 in length 19.2 m 63 ft 0 in
17.53 m 57 ft 6 in height 4.8 m 15 ft 9 in
63.45 m 208 ft 2 in wingspan 32 m 105 ft
4 Rolls-Royce Trent 500 engines 1 × General Electric F118-101
54,000 lbf (240 kN) thrust per engine 17,000 lbf (76 kN)
216,000 lbf (960 kN) total thrust 17,000 lbf (76 kN)
380,000 kg 837,800 lb MTOW 18,144 kg 40,000 lb
16,670 km 9,000 nm range 6,090 nm 11,278 km
475 knots 880 km/h cruise speed 475 mph 764 km/h
Typical seating 3-class 270-310 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.