Airbus A310-300 vs. Sukhoi SSJ 100 95LR
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Airbus A310-300 |
versus |
Sukhoi SSJ 100 95LR |
46.66 m |
153 ft 1 in |
length |
29.94 m |
98 ft 2 in |
15.8 m |
51 ft 10 in |
height |
10.28 m |
33 ft 8 in |
43.9 m |
144 ft |
wingspan |
27.8 m |
91 ft 2 in |
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan |
engines |
2 PowerJet SaM146 turbofans |
52,000 lb |
thrust per engine |
15,400 (68.5 KN) to 16,100 (71.6 KN) at NTO, 17,500 (77.9 KN) to 17,800 (79.2 KN) with APR |
104,000 lb |
total thrust |
30,800 (137 KN) to 32,200 (143.2 KN) at NTO, 35,000 (155.8 KN) to 35,600 (158.4 KN) with APR |
148,768 kg |
328,000 lb |
MTOW |
49,450 kg |
109,000 lb |
8,050 km |
4,348 nm |
range |
4,578 km |
2,470 nm |
482 knots |
279 mph |
cruise speed |
515 mph |
830 km/h |
190-230 passengers |
capacity |
98 (up to 108) passengers |
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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.