Airbus A321-200 vs. Mitsubishi A6M Zero

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Airbus A321-200 versus Mitsubishi A6M Zero
44.51 m 146 ft 0 in length 9.06 m 29 ft 9 in
11.76 m 38 ft 7 in height 3.05 m 10 ft
35.8 m 117 ft 5 in wingspan 12 m 39 ft 4 in
2 GE CFM56-5B3 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
31,600 lbs thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
63,200 lbs total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
89,000 kg 196,200 lb MTOW 2,800 kg 6,170 lb
4,000 nmi 7,408 km range 1,010 nm 1,871 km
871 km/h 541 mph cruise speed 180 knots 105 mph
185 to 220 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.