Northrop T-38 Talon vs. Polikarpov I-16

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Northrop T-38 Talon versus Polikarpov I-16
14.1 m 46 ft 4 in length 6.13 m 20 ft 1 in
3.9 m 12 ft 10 in height 3.25 m 10 ft 8 in
7.7 m 25 ft 3 in wingspan 9 m 29 ft 6 in
Two General Electric J85-GE-5A turbojet engines engines 1x Shvetsov M-25 radial engine
2,050 pounds dry thrust; 2,900 with afterburners thrust per engine 1000 hp
4,100 pounds dry thrust; 5,800 with afterburners total thrust 1000 hp
12,093 lb 5,485 kg MTOW 2,060 kg 4,540 lb
1,759 km 950 nm range 248 mi 216 nm
745 kts 1,380 km/h cruise speed 180 mph 290 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.