McDonnell-Douglas MD-11 vs. Mitsubishi A6M Zero
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| McDonnell-Douglas MD-11 |
versus |
Mitsubishi A6M Zero |
| 61.20 m |
200 ft 10 in |
length |
9.06 m |
29 ft 9 in |
| 17.6 m |
57 ft 9 in |
height |
3.05 m |
10 ft |
| 51.6 m |
169 ft 4 in |
wingspan |
12 m |
39 ft 4 in |
| 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
engines |
1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine |
| 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
thrust per engine |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
| 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
total thrust |
940 hp for take-off, 950 hp at 4,200 m (13,800 ft) |
| 285,990 kg |
630,400 lb |
MTOW |
2,800 kg |
6,170 lb |
| 13,231 km |
7,147 nm |
range |
1,010 nm |
1,871 km |
| 961 km/h |
597 mph |
cruise speed |
180 knots |
105 mph |
| Max 410 passengers |
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.
