Mikoyan-Gurevich MiG-17 vs. Northrop T-38 Talon

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Mikoyan-Gurevich MiG-17 versus Northrop T-38 Talon
11.26 m 37 ft 0 in length 14.1 m 46 ft 4 in
3.8 m 12 ft 6 in height 3.9 m 12 ft 10 in
9.63 m 31 ft 7 in wingspan 7.7 m 25 ft 3 in
1 x Klimov VK-1F afterburning turbojet engines Two General Electric J85-GE-5A turbojet engines
7,452-pound thrust thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
7,452-pound thrust total thrust 4,100 pounds dry thrust; 5,800 with afterburners
6,076 kg 13,400 lb MTOW 12,093 lb 5,485 kg
1,444 km 780 nm range 1,759 km 950 nm
Mach 0.89 1,099 km/h cruise speed 745 kts 1,380 km/h
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.