Chengdu J-20 vs. Canadair CL-415

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Chengdu J-20 versus Canadair CL-415
20.4 m 66 ft 11 in length 19.82 m 65 ft 0 in
4.45 m 14 ft 7 in height 8.66 m 28 ft 5 in
13.01 m 42 ft 8 in wingspan 28.6 m 93 ft 1
2x Saturn 117S or Xian WS-15 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
30,000-32,000 lbs thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
60,000-64,000 lbs total thrust 4,300 to 4,760 shaft horsepower
37,000 kg 81,600 lb MTOW 19,733 kg 43,525 lb
3,200 nm 5,926 km range 1,600 km 864 nm
1,305 mph 2,100 km/h cruise speed 290 km/h 180 mph
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.