McDonnell Douglas F-4 Phantom II vs. Mitsubishi A6M Zero

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McDonnell Douglas F-4 Phantom II versus Mitsubishi A6M Zero
19.2 m 63 ft 0 in length 9.06 m 29 ft 9 in
5.03 m 16 ft 6 in height 3.05 m 10 ft
11.72 m 38 ft 5 in wingspan 12 m 39 ft 4 in
Two General Electric J79s engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
17,900 lbs thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
35,800 lbs total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
27,965 kg 61,700 lb MTOW 2,800 kg 6,170 lb
3,031 km 1,636 nm range 1,010 nm 1,871 km
Mach 2.2 2,717 km/h cruise speed 180 knots 105 mph
Up to 16,000 lbs of externally carried ordnance 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.