Mitsubishi A6M Zero vs. North American Rockwell OV-10 Bronco

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Mitsubishi A6M Zero versus North American Rockwell OV-10 Bronco
9.06 m 29 ft 9 in length 12.7 m 41 ft 7 in
3.05 m 10 ft height 4.62 m 15 ft 2 in
12 m 39 ft 4 in wingspan 12.19 m 40 ft
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine engines 2 x Garrett T76-G-420/421 turboprop engines
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) thrust per engine Approximately 715 hp each
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) total thrust Approximately 1,430 hp total
2,800 kg 6,170 lb MTOW 14,444 lb 6,553 kg
1,010 nm 1,871 km range 1,931 km 1,043 nm
180 knots 105 mph cruise speed 244 mph 393 km/h
capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.