Airbus A300-600 vs. Sukhoi SSJ 100 95LR
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Airbus A300-600 |
versus |
Sukhoi SSJ 100 95LR |
54.10 m |
177 ft 6 in |
length |
29.94 m |
98 ft 2 in |
16.5 m |
54 ft 2 in |
height |
10.28 m |
33 ft 8 in |
44.84 m |
147 ft 1 in |
wingspan |
27.8 m |
91 ft 2 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 PowerJet SaM146 turbofans |
56,000lb to 61,500lb |
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 |
112,000–123,000 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 |
171,700 kg |
378,600 lb |
MTOW |
49,450 kg |
109,000 lb |
7,500 km |
4,052 nm |
range |
4,578 km |
2,470 nm |
897 km/h |
557 mph |
cruise speed |
515 mph |
830 km/h |
210-250 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.