Airbus A330-300 vs. Consolidated B-24 Liberator
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here.
| Airbus A330-300 |
versus |
Consolidated B-24 Liberator |
| 63.66 m |
208 ft 9 in |
length |
20.42 m |
67 ft 0 in |
| 16.79 m |
55 ft 1 in |
height |
5.49 m |
18 ft |
| 60.3 m |
197 ft 9 in |
wingspan |
33.53 m |
110 ft |
| General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
| 311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
1,200 hp, 1,200 hp each |
| Depends on the engine type |
total thrust |
4,800 hp (calculated from 4 engines each with 1,200 hp) |
| 242,000 kg |
533,600 lb |
MTOW |
26,580 kg |
58,600 lb |
| 11,750 km |
6,346 nm |
range |
2,850 mi |
2,481 nm |
| 900 km/h |
559 mph |
cruise speed |
175 mph |
282 km/h |
| 250-290 |
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.
