Airbus A310-300 vs. Antonov An-124 Ruslan
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Airbus A310-300 |
versus |
Antonov An-124 Ruslan |
46.66 m |
153 ft 1 in |
length |
69.10 m |
226 ft 9 in |
15.8 m |
51 ft 10 in |
height |
20.78 m |
68 ft 2 in |
43.9 m |
144 ft |
wingspan |
73.3 m |
240 ft 6 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
4 x Ivchenko Progress D-18T turbofan engines |
52,000 lb |
thrust per engine |
Approximately 51,590 lbf |
104,000 lb |
total thrust |
Approximately 206,360 lbf |
148,768 kg |
328,000 lb |
MTOW |
405,000 kg |
893,000 lb |
8,050 km |
4,348 nm |
range |
3,700 km |
1,998 nm |
482 knots |
279 mph |
cruise speed |
800 km/h |
497 mph |
190-230 passengers |
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.