Airbus A310-300 vs. Chengdu J-20

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Airbus A310-300 versus Chengdu J-20
46.66 m 153 ft 1 in length 20.4 m 66 ft 11 in
15.8 m 51 ft 10 in height 4.45 m 14 ft 7 in
43.9 m 144 ft wingspan 13.01 m 42 ft 8 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2x Saturn 117S or Xian WS-15
52,000 lb thrust per engine 30,000-32,000 lbs
104,000 lb total thrust 60,000-64,000 lbs
148,768 kg 328,000 lb MTOW 37,000 kg 81,600 lb
8,050 km 4,348 nm range 3,200 nm 5,926 km
482 knots 279 mph cruise speed 1,305 mph 2,100 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.