Lockheed P-2 Neptune vs. Mitsubishi A6M Zero

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Lockheed P-2 Neptune versus Mitsubishi A6M Zero
30.17 m 99 ft 0 in length 9.06 m 29 ft 9 in
10.15 m 33 ft 4 in height 3.05 m 10 ft
33.53 m 110 ft wingspan 12 m 39 ft 4 in
2 x Wright R-3350 radial engines engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
Approximately 3,700 hp thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Approximately 7,400 hp total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
27,216 kg 60,000 lb MTOW 2,800 kg 6,170 lb
7,885 km 4,259 nm range 1,010 nm 1,871 km
300 mph 483 km/h cruise speed 180 knots 105 mph
based on configuration 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.