Sukhoi SSJ 100 95LR vs. lockheed C-130 hercules

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Sukhoi SSJ 100 95LR versus lockheed C-130 hercules
29.94 m 98 ft 2 in length 29.79 m 97 ft 9 in
10.28 m 33 ft 8 in height 11.66 m 38 ft 3 in
27.8 m 91 ft 2 in wingspan 40.41 m 132 ft 7 in
2 PowerJet SaM146 turbofans engines 4 x Allison T56-A-15 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 4,590 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 18,360 hp total
49,450 kg 109,000 lb MTOW 70,307 kg 155,000 lb
4,578 km 2,470 nm range 3,760 km 2,031 nm
515 mph 830 km/h cruise speed 540 km/h 335 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.