Bombardier CRJ1000 vs. Consolidated B-24 Liberator
... or view the full comparison list
here.
| Bombardier CRJ1000 |
versus |
Consolidated B-24 Liberator |
| 39.1 m |
128 ft 5 in |
length |
20.42 m |
67 ft 0 in |
| 7.5 m |
24 ft 7 in |
height |
5.49 m |
18 ft |
| 26.2 m |
86 ft |
wingspan |
33.53 m |
110 ft |
| 2 GE CF34-8C5A1 turbofans |
engines |
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
| 13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve |
thrust per engine |
1,200 hp, 1,200 hp each |
| 27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve |
total thrust |
4,800 hp (calculated from 4 engines each with 1,200 hp) |
| 41,640 kg |
91,800 lb |
MTOW |
26,580 kg |
58,600 lb |
| 3,004 km |
1,623 nm |
range |
2,850 mi |
2,481 nm |
| 515 mph |
829 km/h |
cruise speed |
175 mph |
282 km/h |
| 100 (common) |
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.
