Cessna O-2 Skymaster vs. Lockheed P-2 Neptune
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Cessna O-2 Skymaster |
versus |
Lockheed P-2 Neptune |
8.9 m |
29 ft 2 in |
length |
30.17 m |
99 ft 0 in |
2.87 m |
9 ft 5 in |
height |
10.15 m |
33 ft 4 in |
11.58 m |
38 ft |
wingspan |
33.53 m |
110 ft |
Two 210-hp Continental IO-360s |
engines |
2 x Wright R-3350 radial engines |
210 hp |
thrust per engine |
Approximately 3,700 hp |
420 hp |
total thrust |
Approximately 7,400 hp |
5,400 lb |
2,449 kg |
MTOW |
27,216 kg |
60,000 lb |
1,705 km |
921 nm |
range |
7,885 km |
4,259 nm |
144 mph |
232 km/h |
cruise speed |
300 mph |
483 km/h |
2 |
capacity |
based on configuration |
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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.