Chengdu J-20 vs. Lockheed U-2

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Chengdu J-20 versus Lockheed U-2
20.4 m 66 ft 11 in length 19.2 m 63 ft 0 in
4.45 m 14 ft 7 in height 4.8 m 15 ft 9 in
13.01 m 42 ft 8 in wingspan 32 m 105 ft
2x Saturn 117S or Xian WS-15 engines 1 × General Electric F118-101
30,000-32,000 lbs thrust per engine 17,000 lbf (76 kN)
60,000-64,000 lbs total thrust 17,000 lbf (76 kN)
37,000 kg 81,600 lb MTOW 18,144 kg 40,000 lb
3,200 nm 5,926 km range 6,090 nm 11,278 km
1,305 mph 2,100 km/h cruise speed 475 mph 764 km/h
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.