Mitsubishi A6M Zero vs. Canadair CL-415

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Mitsubishi A6M Zero versus Canadair CL-415
9.06 m 29 ft 9 in length 19.82 m 65 ft 0 in
3.05 m 10 ft height 8.66 m 28 ft 5 in
12 m 39 ft 4 in wingspan 28.6 m 93 ft 1
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) total thrust 4,300 to 4,760 shaft horsepower
2,800 kg 6,170 lb MTOW 19,733 kg 43,525 lb
1,010 nm 1,871 km range 1,600 km 864 nm
180 knots 105 mph cruise speed 290 km/h 180 mph
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.