Sukhoi SSJ 100 95LR vs. Airbus H225 Super Puma
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Sukhoi SSJ 100 95LR |
versus |
Airbus H225 Super Puma |
29.94 m |
98 ft 2 in |
length |
14.06 m |
46 ft 2 in |
10.28 m |
33 ft 8 in |
height |
4.38 m |
14 ft 4 in |
27.8 m |
91 ft 2 in |
wingspan |
|
|
2 PowerJet SaM146 turbofans |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
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 |
thrust per engine |
2,778 hp |
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 |
total thrust |
5,556 hp |
49,450 kg |
109,000 lb |
MTOW |
11,000 kg |
24,251 lb |
4,578 km |
2,470 nm |
range |
857 km |
463 nm |
515 mph |
830 km/h |
cruise speed |
242 km/h |
150 mph |
98 (up to 108) passengers |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.