Cessna O-2 Skymaster vs. Consolidated B-24 Liberator
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Cessna O-2 Skymaster |
versus |
Consolidated B-24 Liberator |
8.9 m |
29 ft 2 in |
length |
20.42 m |
67 ft 0 in |
2.87 m |
9 ft 5 in |
height |
5.49 m |
18 ft |
11.58 m |
38 ft |
wingspan |
33.53 m |
110 ft |
Two 210-hp Continental IO-360s |
engines |
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines |
210 hp |
thrust per engine |
1,200 hp, 1,200 hp each |
420 hp |
total thrust |
4,800 hp (calculated from 4 engines each with 1,200 hp) |
5,400 lb |
2,449 kg |
MTOW |
26,580 kg |
58,600 lb |
1,705 km |
921 nm |
range |
2,850 mi |
2,481 nm |
144 mph |
232 km/h |
cruise speed |
175 mph |
282 km/h |
2 |
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.