Airbus A321XLR vs. Mitsubishi A6M Zero

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Airbus A321XLR versus Mitsubishi A6M Zero
44.51 m 146 ft 0 in length 9.06 m 29 ft 9 in
11.76 m 38 ft 7 in height 3.05 m 10 ft
35.8 m 117 ft 5 in wingspan 12 m 39 ft 4 in
CFM LEAP-1A and P&W PW1100G engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
33,000 lbs (147 kN) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
66,000 lbs (294 kN) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
101,000 kg 222,700 lb MTOW 2,800 kg 6,170 lb
4,700 nmi 8,704 km range 1,010 nm 1,871 km
963km/h 598mph cruise speed 180 knots 105 mph
180-220 seats (typical 2-class seating) 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.