Lockheed Martin F-35 Lightning II vs. Mitsubishi A6M Zero

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Lockheed Martin F-35 Lightning II versus Mitsubishi A6M Zero
15.67 m 51 ft 4 in length 9.06 m 29 ft 9 in
4.33 m 14 ft 2 in height 3.05 m 10 ft
10.7 m 35 ft 1 in wingspan 12 m 39 ft 4 in
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
40,000 lb thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
40,000 lb total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
31,800 kg 70,000 lb MTOW 2,800 kg 6,170 lb
1,380 mi 1,200 nm range 1,010 nm 1,871 km
520 kt 302 mph cruise speed 180 knots 105 mph
18,000 pounds of total ordinance 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.