Airbus A350-1000 vs. Mitsubishi A6M Zero

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Airbus A350-1000 versus Mitsubishi A6M Zero
73.79 m 242 ft 1 in length 9.06 m 29 ft 9 in
17.08 m 56 ft height 3.05 m 10 ft
64.75 m 212 ft 5 in wingspan 12 m 39 ft 4 in
2 Trent XWB-97 turbofan engines engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
97,000 lb thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
194,000 lb total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
319,000 kg 703,300 lb MTOW 2,800 kg 6,170 lb
16,100 km 8,695 nm range 1,010 nm 1,871 km
1,099 km/h 683 mph cruise speed 180 knots 105 mph
350 to 410 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.