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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.