Airbus A310-300 vs. lockheed C-130 hercules
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Airbus A310-300 |
versus |
lockheed C-130 hercules |
46.66 m |
153 ft 1 in |
length |
29.79 m |
97 ft 9 in |
15.8 m |
51 ft 10 in |
height |
11.66 m |
38 ft 3 in |
43.9 m |
144 ft |
wingspan |
40.41 m |
132 ft 7 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
4 x Allison T56-A-15 turboprop engines |
52,000 lb |
thrust per engine |
Approximately 4,590 hp per engine |
104,000 lb |
total thrust |
Approximately 18,360 hp total |
148,768 kg |
328,000 lb |
MTOW |
70,307 kg |
155,000 lb |
8,050 km |
4,348 nm |
range |
3,760 km |
2,031 nm |
482 knots |
279 mph |
cruise speed |
540 km/h |
335 mph |
190-230 passengers |
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.