Airbus A300-600 vs. Lockheed U-2

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Airbus A300-600 versus Lockheed U-2
54.10 m 177 ft 6 in length 19.2 m 63 ft 0 in
16.5 m 54 ft 2 in height 4.8 m 15 ft 9 in
44.84 m 147 ft 1 in wingspan 32 m 105 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 × General Electric F118-101
56,000lb to 61,500lb thrust per engine 17,000 lbf (76 kN)
112,000–123,000 lb total thrust 17,000 lbf (76 kN)
171,700 kg 378,600 lb MTOW 18,144 kg 40,000 lb
7,500 km 4,052 nm range 6,090 nm 11,278 km
897 km/h 557 mph cruise speed 475 mph 764 km/h
210-250 passengers 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.