Lockheed L-1011 TriStar 500 vs. Mitsubishi A6M Zero

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Lockheed L-1011 TriStar 500 versus Mitsubishi A6M Zero
50.05 m 164 ft 3 in length 9.06 m 29 ft 9 in
16.87 m 55 ft 4 in height 3.05 m 10 ft
50.09 m 164 ft 4 in wingspan 12 m 39 ft 4 in
3 Rolls-Royce RB211 engines engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
42,000 lbf thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
126,000 lbf (3 engines x 42,000 lbf per engine) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
231,330 kg 510,000 lb MTOW 2,800 kg 6,170 lb
11,260 km 6,100 nm range 1,010 nm 1,871 km
525 knots 972 km/h cruise speed 180 knots 105 mph
Max. 315 passengers (typical 253) 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.