Fouga CM.170 Magister vs. Northrop T-38 Talon

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Fouga CM.170 Magister versus Northrop T-38 Talon
10.06 m 33 ft 0 in length 14.1 m 46 ft 4 in
2.8 m 9 ft 2 in height 3.9 m 12 ft 10 in
12.15 m 39 ft 1 wingspan 7.7 m 25 ft 3 in
Two Turbomeca Marboré IIA turbojets engines Two General Electric J85-GE-5A turbojet engines
3.9 kN thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
7.8 kN total thrust 4,100 pounds dry thrust; 5,800 with afterburners
3,200 kg 7,050 lb MTOW 12,093 lb 5,485 kg
924 km 499 nm range 1,759 km 950 nm
715 km/h 444 mph cruise speed 745 kts 1,380 km/h
2 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.