McDonnell-Douglas DC-10-30 vs. Sukhoi SSJ 100 95LR
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McDonnell-Douglas DC-10-30 |
versus |
Sukhoi SSJ 100 95LR |
55.35 m |
181 ft 8 in |
length |
29.94 m |
98 ft 2 in |
17.8 m |
58 ft 5 in |
height |
10.28 m |
33 ft 8 in |
50.39 m |
165 ft 4 in |
wingspan |
27.8 m |
91 ft 2 in |
3x GE CF6-50C Turbofan |
engines |
2 PowerJet SaM146 turbofans |
54,000 lbf |
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 |
162,000 lbf |
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 |
251,744 kg |
555,000 lb |
MTOW |
49,450 kg |
109,000 lb |
9,630 km |
5,200 nm |
range |
4,578 km |
2,470 nm |
507 knots |
939 km/h |
cruise speed |
515 mph |
830 km/h |
Up to 380 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.