Fouga CM.170 Magister vs. McDonnell Douglas F-4 Phantom II

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Fouga CM.170 Magister versus McDonnell Douglas F-4 Phantom II
10.06 m 33 ft 0 in length 19.2 m 63 ft 0 in
2.8 m 9 ft 2 in height 5.03 m 16 ft 6 in
12.15 m 39 ft 1 wingspan 11.72 m 38 ft 5 in
Two Turbomeca Marboré IIA turbojets engines Two General Electric J79s
3.9 kN thrust per engine 17,900 lbs
7.8 kN total thrust 35,800 lbs
3,200 kg 7,050 lb MTOW 27,965 kg 61,700 lb
924 km 499 nm range 3,031 km 1,636 nm
715 km/h 444 mph cruise speed Mach 2.2 2,717 km/h
2 capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.