Consolidated B-24 Liberator vs. de Havilland Canada DHC-2 Beaver
... or view the full comparison list
here.
Consolidated B-24 Liberator |
versus |
de Havilland Canada DHC-2 Beaver |
20.42 m |
67 ft 0 in |
length |
13.56 m |
44 ft 6 in |
5.49 m |
18 ft |
height |
5 m |
16 ft 5 in |
33.53 m |
110 ft |
wingspan |
16.56 m |
54 ft 4 in |
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
engines |
2 x Armstrong Siddeley Double Mamba turboprop engines |
1,200 hp, 1,200 hp each |
thrust per engine |
Approximately 3,100 hp (2,312 kW) each |
4,800 hp (calculated from 4 engines each with 1,200 hp) |
total thrust |
Approximately 6,200 hp (4,624 kW) total |
26,580 kg |
58,600 lb |
MTOW |
24,200 lb |
10,977 kg |
2,850 mi |
2,481 nm |
range |
2,535 km |
1,369 nm |
175 mph |
282 km/h |
cruise speed |
228 mph |
367 km/h |
8,000 pounds |
capacity |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.