Douglas DC-8-61 vs. Lockheed Martin C-130J Super Hercules
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Douglas DC-8-61 |
versus |
Lockheed Martin C-130J Super Hercules |
57.0 m |
187 ft 0 in |
length |
34.37 m |
112 ft 9 in |
13.1 m |
43 ft |
height |
11.86 m |
38 ft 11 in |
45.24 m |
148 ft 5 in |
wingspan |
40.41 m |
132 ft 7 in |
4x P&W JT3D-3B Turbofan |
engines |
4 x Rolls-Royce AE 2100D3 turboprop engines |
18,000 pound-force |
thrust per engine |
Approximately 4,700 hp per engine |
72,000 pound-force |
total thrust |
Approximately 18,800 hp total |
147,400 kg |
325,000 lb |
MTOW |
76,610 kg |
168,900 lb |
3,200 nm |
5,926 km |
range |
4,600 km |
2,485 nm |
483 knots |
282 mph |
cruise speed |
660 km/h |
410 mph |
180 to 220 passengers in a mixed-class seating |
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.