Airbus A310-300 vs. Mitsubishi A6M Zero

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Airbus A310-300 versus Mitsubishi A6M Zero
46.66 m 153 ft 1 in length 9.06 m 29 ft 9 in
15.8 m 51 ft 10 in height 3.05 m 10 ft
43.9 m 144 ft wingspan 12 m 39 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
52,000 lb thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
104,000 lb total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
148,768 kg 328,000 lb MTOW 2,800 kg 6,170 lb
8,050 km 4,348 nm range 1,010 nm 1,871 km
482 knots 279 mph cruise speed 180 knots 105 mph
190-230 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.