Boeing 777-200 vs. Mitsubishi A6M Zero
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| Boeing 777-200 |
versus |
Mitsubishi A6M Zero |
| 63.7 m |
209 ft 1 in |
length |
9.06 m |
29 ft 9 in |
| 18.6 m |
61 ft |
height |
3.05 m |
10 ft |
| 64.8 m |
212 ft 7 in |
wingspan |
12 m |
39 ft 4 in |
| General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 |
engines |
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine |
| Up to 94,000 pounds |
thrust per engine |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
| Up to 188,000 pounds |
total thrust |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
| 299,370 kg |
660,000 lb |
MTOW |
2,800 kg |
6,170 lb |
| 5,240 nm |
9,711 km |
range |
1,010 nm |
1,871 km |
| 560 mph |
901 km/h |
cruise speed |
180 knots |
105 mph |
| 305 |
capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
