Chengdu J-20 vs. Mitsubishi A6M Zero

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Chengdu J-20 versus Mitsubishi A6M Zero
20.4 m 66 ft 11 in length 9.06 m 29 ft 9 in
4.45 m 14 ft 7 in height 3.05 m 10 ft
13.01 m 42 ft 8 in wingspan 12 m 39 ft 4 in
2x Saturn 117S or Xian WS-15 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
30,000-32,000 lbs thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
60,000-64,000 lbs total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
37,000 kg 81,600 lb MTOW 2,800 kg 6,170 lb
3,200 nm 5,926 km range 1,010 nm 1,871 km
1,305 mph 2,100 km/h cruise speed 180 knots 105 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.