McDonnell-Douglas MD-11 vs. Consolidated B-24 Liberator
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| McDonnell-Douglas MD-11 |
versus |
Consolidated B-24 Liberator |
| 61.20 m |
200 ft 10 in |
length |
20.42 m |
67 ft 0 in |
| 17.6 m |
57 ft 9 in |
height |
5.49 m |
18 ft |
| 51.6 m |
169 ft 4 in |
wingspan |
33.53 m |
110 ft |
| 3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) |
engines |
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
| 273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) |
thrust per engine |
1,200 hp, 1,200 hp each |
| 819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) |
total thrust |
4,800 hp (calculated from 4 engines each with 1,200 hp) |
| 285,990 kg |
630,400 lb |
MTOW |
26,580 kg |
58,600 lb |
| 13,231 km |
7,147 nm |
range |
2,850 mi |
2,481 nm |
| 961 km/h |
597 mph |
cruise speed |
175 mph |
282 km/h |
| Max 410 passengers |
capacity |
8,000 pounds |
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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.
