Lockheed Martin C-130J Super Hercules vs. de Havilland Canada DHC-3 Otter
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| Lockheed Martin C-130J Super Hercules |
versus |
de Havilland Canada DHC-3 Otter |
| 34.37 m |
112 ft 9 in |
length |
10.52 m |
34 ft 6 in |
| 11.86 m |
38 ft 11 in |
height |
3.84 m |
12 ft 7 in |
| 40.41 m |
132 ft 7 in |
wingspan |
17.68 m |
58 ft |
| 4 x Rolls-Royce AE 2100D3 turboprop engines |
engines |
1 x Pratt & Whitney R-1340 radial engine |
| Approximately 4,700 hp per engine |
thrust per engine |
400 to 600 horsepower (298 to 447 kW) |
| Approximately 18,800 hp total |
total thrust |
400 to 600 horsepower (298 to 447 kW) |
| 76,610 kg |
168,900 lb |
MTOW |
5,670 kg |
12,500 lb |
| 4,600 km |
2,485 nm |
range |
1,296 km |
700 nm |
| 660 km/h |
410 mph |
cruise speed |
215 km/h |
134 mph |
| based on configuration |
capacity |
10-11 passengers |
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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.
