de Havilland Canada DHC-2 Beaver vs. Mitsubishi A6M Zero

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de Havilland Canada DHC-2 Beaver versus Mitsubishi A6M Zero
13.56 m 44 ft 6 in length 9.06 m 29 ft 9 in
5 m 16 ft 5 in height 3.05 m 10 ft
16.56 m 54 ft 4 in wingspan 12 m 39 ft 4 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
Approximately 3,100 hp (2,312 kW) each thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Approximately 6,200 hp (4,624 kW) total total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
24,200 lb 10,977 kg MTOW 2,800 kg 6,170 lb
2,535 km 1,369 nm range 1,010 nm 1,871 km
228 mph 367 km/h cruise speed 180 knots 105 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.