Lockheed Martin C-130J Super Hercules vs. Canadair CL-415
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Lockheed Martin C-130J Super Hercules |
versus |
Canadair CL-415 |
34.37 m |
112 ft 9 in |
length |
19.82 m |
65 ft 0 in |
11.86 m |
38 ft 11 in |
height |
8.66 m |
28 ft 5 in |
40.41 m |
132 ft 7 in |
wingspan |
28.6 m |
93 ft 1 |
4 x Rolls-Royce AE 2100D3 turboprop engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
Approximately 4,700 hp per engine |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
Approximately 18,800 hp total |
total thrust |
4,300 to 4,760 shaft horsepower |
76,610 kg |
168,900 lb |
MTOW |
19,733 kg |
43,525 lb |
4,600 km |
2,485 nm |
range |
1,600 km |
864 nm |
660 km/h |
410 mph |
cruise speed |
290 km/h |
180 mph |
based on configuration |
capacity |
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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.