Airbus A300-600 vs. Mitsubishi A6M Zero

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Airbus A300-600 versus Mitsubishi A6M Zero
54.10 m 177 ft 6 in length 9.06 m 29 ft 9 in
16.5 m 54 ft 2 in height 3.05 m 10 ft
44.84 m 147 ft 1 in wingspan 12 m 39 ft 4 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
56,000lb to 61,500lb thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
112,000–123,000 lb total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
171,700 kg 378,600 lb MTOW 2,800 kg 6,170 lb
7,500 km 4,052 nm range 1,010 nm 1,871 km
897 km/h 557 mph cruise speed 180 knots 105 mph
210-250 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.