Airbus A310-300 vs. Lockheed U-2

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Airbus A310-300 versus Lockheed U-2
46.66 m 153 ft 1 in length 19.2 m 63 ft 0 in
15.8 m 51 ft 10 in height 4.8 m 15 ft 9 in
43.9 m 144 ft wingspan 32 m 105 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 × General Electric F118-101
52,000 lb thrust per engine 17,000 lbf (76 kN)
104,000 lb total thrust 17,000 lbf (76 kN)
148,768 kg 328,000 lb MTOW 18,144 kg 40,000 lb
8,050 km 4,348 nm range 6,090 nm 11,278 km
482 knots 279 mph cruise speed 475 mph 764 km/h
190-230 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.