Canadair CT-114 Tutor vs. Mitsubishi A6M Zero

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Canadair CT-114 Tutor versus Mitsubishi A6M Zero
9.75 m 32 ft 0 in length 9.06 m 29 ft 9 in
2.84 m 9 ft 4 in height 3.05 m 10 ft
11.07 m 36 ft 4 in wingspan 12 m 39 ft 4 in
1 Orenda J85-CAN-40 turbojet engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
2,950 lbs thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
2,950 lbs total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
3,331 kg 7,350 lb MTOW 2,800 kg 6,170 lb
1,520 km 821 nm range 1,010 nm 1,871 km
310 knots 180 mph cruise speed 180 knots 105 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.