Tupolev TU-155 vs. Mitsubishi A6M Zero

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Tupolev TU-155 versus Mitsubishi A6M Zero
47.63 m 156 ft 3 in length 9.06 m 29 ft 9 in
16.4 m 53 ft 10 in height 3.05 m 10 ft
64.9 m 212 ft 11 in wingspan 12 m 39 ft 4 in
4 × Kuznetsov NK-321 turbofans engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
304.5 kN (68,500 lbf) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
1,218 kN (274,000 lbf) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
640,000 kg 1,411,000 lb MTOW 2,800 kg 6,170 lb
7,000 km 3,780 nm range 1,010 nm 1,871 km
850 km/h 528 mph cruise speed 180 knots 105 mph
350 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.