Airbus A380-800F vs. Lockheed Martin C-130J Super Hercules
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Airbus A380-800F |
versus |
Lockheed Martin C-130J Super Hercules |
72.73 m |
238 ft 7 in |
length |
34.37 m |
112 ft 9 in |
24.09 m |
79 ft |
height |
11.86 m |
38 ft 11 in |
79.75 m |
261 ft 8 in |
wingspan |
40.41 m |
132 ft 7 in |
4 x Engine Alliance GP7200 turbofan engines |
engines |
4 x Rolls-Royce AE 2100D3 turboprop engines |
70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons) |
thrust per engine |
Approximately 4,700 hp per engine |
280,000 to 320,000 pounds |
total thrust |
Approximately 18,800 hp total |
590,000 kg |
1,300,733 lb |
MTOW |
76,610 kg |
168,900 lb |
14,800 km |
7,992 nm |
range |
4,600 km |
2,485 nm |
903 km/h |
561 mph |
cruise speed |
660 km/h |
410 mph |
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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.