Sukhoi SSJ 100 95LR vs. Northrop T-38 Talon

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Sukhoi SSJ 100 95LR versus Northrop T-38 Talon
29.94 m 98 ft 2 in length 14.1 m 46 ft 4 in
10.28 m 33 ft 8 in height 3.9 m 12 ft 10 in
27.8 m 91 ft 2 in wingspan 7.7 m 25 ft 3 in
2 PowerJet SaM146 turbofans engines Two General Electric J85-GE-5A turbojet 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 2,050 pounds dry thrust; 2,900 with afterburners
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 4,100 pounds dry thrust; 5,800 with afterburners
49,450 kg 109,000 lb MTOW 12,093 lb 5,485 kg
4,578 km 2,470 nm range 1,759 km 950 nm
515 mph 830 km/h cruise speed 745 kts 1,380 km/h
98 (up to 108) passengers capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.