Mikoyan-Gurevich MiG-21 vs. Northrop T-38 Talon

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Mikoyan-Gurevich MiG-21 versus Northrop T-38 Talon
15.76 m 51 ft 8 in length 14.1 m 46 ft 4 in
4.11 m 13 ft 6 in height 3.9 m 12 ft 10 in
7.16 m 23 ft 6 in wingspan 7.7 m 25 ft 3 in
1 x Tumansky R-25-300 afterburning turbojet engines Two General Electric J85-GE-5A turbojet engines
15,640 lb with reheat thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
15,640 lb total thrust 4,100 pounds dry thrust; 5,800 with afterburners
7,958 kg 17,500 lb MTOW 12,093 lb 5,485 kg
1,161 km 627 nm range 1,759 km 950 nm
1,386 mph 2,230 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.