Northrop T-38 Talon vs. Sukhoi Su-57

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Northrop T-38 Talon versus Sukhoi Su-57
14.1 m 46 ft 4 in length 20.1 m 65 ft 11 in
3.9 m 12 ft 10 in height 3.8 m 12 ft 6 in
7.7 m 25 ft 3 in wingspan 14.1 m 46 ft 3 in
Two General Electric J85-GE-5A turbojet engines engines 2 (Izdeliye 117 or AL-41F1 augmented turbofans)
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 107.9 kN dry and 166.8 kN after burning
4,100 pounds dry thrust; 5,800 with afterburners total thrust 215.8 kN dry and 333.6 kN after burning
12,093 lb 5,485 kg MTOW 35,000 kg 77,200 lb
1,759 km 950 nm range 3,500 km 1,890 nm
745 kts 1,380 km/h cruise speed Mach 2 2470 km/h
Two (student and instructor) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.