Grumman OV-1 Mohawk vs. Mitsubishi A6M Zero

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Grumman OV-1 Mohawk versus Mitsubishi A6M Zero
12.52 m 41 ft 1 in length 9.06 m 29 ft 9 in
3.89 m 12 ft 9 in height 3.05 m 10 ft
14.63 m 48 ft wingspan 12 m 39 ft 4 in
2 x Lycoming T53 turboprop engines engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
Approximately 1,100 hp each thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Approximately 2,200 hp total total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
14,950 lb 6,781 kg MTOW 2,800 kg 6,170 lb
1,690 km 913 nm range 1,010 nm 1,871 km
230 mph 370 km/h cruise speed 180 knots 105 mph
Pilot and observer 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.