Douglas DC-8-61 vs. Mitsubishi A6M Zero

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Douglas DC-8-61 versus Mitsubishi A6M Zero
57.0 m 187 ft 0 in length 9.06 m 29 ft 9 in
13.1 m 43 ft height 3.05 m 10 ft
45.24 m 148 ft 5 in wingspan 12 m 39 ft 4 in
4x P&W JT3D-3B Turbofan engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
18,000 pound-force thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
72,000 pound-force total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
147,400 kg 325,000 lb MTOW 2,800 kg 6,170 lb
3,200 nm 5,926 km range 1,010 nm 1,871 km
483 knots 282 mph cruise speed 180 knots 105 mph
180 to 220 passengers in a mixed-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.