Sukhoi SSJ 100 95LR vs. Lockheed Martin C-130J Super Hercules
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Sukhoi SSJ 100 95LR |
versus |
Lockheed Martin C-130J Super Hercules |
29.94 m |
98 ft 2 in |
length |
34.37 m |
112 ft 9 in |
10.28 m |
33 ft 8 in |
height |
11.86 m |
38 ft 11 in |
27.8 m |
91 ft 2 in |
wingspan |
40.41 m |
132 ft 7 in |
2 PowerJet SaM146 turbofans |
engines |
4 x Rolls-Royce AE 2100D3 turboprop 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 |
Approximately 4,700 hp per engine |
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 |
Approximately 18,800 hp total |
49,450 kg |
109,000 lb |
MTOW |
76,610 kg |
168,900 lb |
4,578 km |
2,470 nm |
range |
4,600 km |
2,485 nm |
515 mph |
830 km/h |
cruise speed |
660 km/h |
410 mph |
98 (up to 108) passengers |
capacity |
based on configuration |
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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.