Sukhoi SSJ 100 95LR vs. Lockheed Martin F-35 Lightning II

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Sukhoi SSJ 100 95LR versus Lockheed Martin F-35 Lightning II
29.94 m 98 ft 2 in length 15.67 m 51 ft 4 in
10.28 m 33 ft 8 in height 4.33 m 14 ft 2 in
27.8 m 91 ft 2 in wingspan 10.7 m 35 ft 1 in
2 PowerJet SaM146 turbofans engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
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 40,000 lb
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 40,000 lb
49,450 kg 109,000 lb MTOW 31,800 kg 70,000 lb
4,578 km 2,470 nm range 1,380 mi 1,200 nm
515 mph 830 km/h cruise speed 520 kt 302 mph
98 (up to 108) passengers capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.