Airbus A330-300 vs. Mitsubishi A6M Zero

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Airbus A330-300 versus Mitsubishi A6M Zero
63.66 m 208 ft 9 in length 9.06 m 29 ft 9 in
16.79 m 55 ft 1 in height 3.05 m 10 ft
60.3 m 197 ft 9 in wingspan 12 m 39 ft 4 in
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Depends on the engine type total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
242,000 kg 533,600 lb MTOW 2,800 kg 6,170 lb
11,750 km 6,346 nm range 1,010 nm 1,871 km
900 km/h 559 mph cruise speed 180 knots 105 mph
250-290 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.