Airbus A340-200 vs. Lockheed Martin C-130J Super Hercules
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Airbus A340-200 |
versus |
Lockheed Martin C-130J Super Hercules |
59.4 m |
194 ft 11 in |
length |
34.37 m |
112 ft 9 in |
16.8 m |
55 ft 1 in |
height |
11.86 m |
38 ft 11 in |
60.3 m |
197 ft 9 in |
wingspan |
40.41 m |
132 ft 7 in |
4 x CFM International CFM56-5C4 |
engines |
4 x Rolls-Royce AE 2100D3 turboprop engines |
34,000 lbf |
thrust per engine |
Approximately 4,700 hp per engine |
136,000 lbf |
total thrust |
Approximately 18,800 hp total |
275,000 kg |
606,300 lb |
MTOW |
76,610 kg |
168,900 lb |
12,400 km |
6,699 nm |
range |
4,600 km |
2,485 nm |
880 km/h |
547 mph |
cruise speed |
660 km/h |
410 mph |
Typical seating 3-class 210-250 |
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.