Airbus A330-200 vs. Mitsubishi A6M Zero

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Airbus A330-200 versus Mitsubishi A6M Zero
58.82 m 193 ft 0 in length 9.06 m 29 ft 9 in
17.39 m 57 ft 1 in height 3.05 m 10 ft
64 m 210 ft wingspan 12 m 39 ft 4 in
2 Turbofans engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Depends on the engine variant total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
251,000 kg 553,400 lb MTOW 2,800 kg 6,170 lb
15,094 km 8,150 nm range 1,010 nm 1,871 km
531 mph 855 km/h cruise speed 180 knots 105 mph
220-260 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.