Boeing F/A-18E/F Super Hornet vs. Mitsubishi A6M Zero

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Boeing F/A-18E/F Super Hornet versus Mitsubishi A6M Zero
18.5 m 60 ft 3 in length 9.06 m 29 ft 9 in
4.87 m 16 ft height 3.05 m 10 ft
13.68 m 44 ft 1 wingspan 12 m 39 ft 4 in
Two F414-GE-400 turbofan engines engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
Up to 17,000 lbs thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
Up to 34,000 lbs total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
29,937 kg 66,000 lb MTOW 2,800 kg 6,170 lb
2,346 km 1,268 nm range 1,010 nm 1,871 km
1032 knots 1,911 km/h cruise speed 180 knots 105 mph
Overall capability across all eleven hardpoints is 17,750lbs of external stores 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.