Fouga CM.170 Magister vs. Mitsubishi A6M Zero

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Fouga CM.170 Magister versus Mitsubishi A6M Zero
10.06 m 33 ft 0 in length 9.06 m 29 ft 9 in
2.8 m 9 ft 2 in height 3.05 m 10 ft
12.15 m 39 ft 1 wingspan 12 m 39 ft 4 in
Two Turbomeca Marboré IIA turbojets engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
3.9 kN thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
7.8 kN total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
3,200 kg 7,050 lb MTOW 2,800 kg 6,170 lb
924 km 499 nm range 1,010 nm 1,871 km
715 km/h 444 mph cruise speed 180 knots 105 mph
2 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.