Cessna O-2 Skymaster vs. Lockheed Martin C-130J Super Hercules
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Cessna O-2 Skymaster |
versus |
Lockheed Martin C-130J Super Hercules |
8.9 m |
29 ft 2 in |
length |
34.37 m |
112 ft 9 in |
2.87 m |
9 ft 5 in |
height |
11.86 m |
38 ft 11 in |
11.58 m |
38 ft |
wingspan |
40.41 m |
132 ft 7 in |
Two 210-hp Continental IO-360s |
engines |
4 x Rolls-Royce AE 2100D3 turboprop engines |
210 hp |
thrust per engine |
Approximately 4,700 hp per engine |
420 hp |
total thrust |
Approximately 18,800 hp total |
5,400 lb |
2,449 kg |
MTOW |
76,610 kg |
168,900 lb |
1,705 km |
921 nm |
range |
4,600 km |
2,485 nm |
144 mph |
232 km/h |
cruise speed |
660 km/h |
410 mph |
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.