Airbus A320-200 vs. Mitsubishi A6M Zero

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Airbus A320-200 versus Mitsubishi A6M Zero
38.7 m 127 ft 0 in length 9.06 m 29 ft 9 in
17.4 m 57 ft 1 in height 3.05 m 10 ft
35.8 m 117 ft 5 in wingspan 12 m 39 ft 4 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
Between 21,000 - 33,000 lbf thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Between 42,000 - 66,000 lbf total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
77,000 kg 169,800 lb MTOW 2,800 kg 6,170 lb
5,700 km 3,078 nm range 1,010 nm 1,871 km
530 mph 853 km/h cruise speed 180 knots 105 mph
Typically between 140-180 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.