Fouga CM.170 Magister vs. Lockheed U-2

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Fouga CM.170 Magister versus Lockheed U-2
10.06 m 33 ft 0 in length 19.2 m 63 ft 0 in
2.8 m 9 ft 2 in height 4.8 m 15 ft 9 in
12.15 m 39 ft 1 wingspan 32 m 105 ft
Two Turbomeca Marboré IIA turbojets engines 1 × General Electric F118-101
3.9 kN thrust per engine 17,000 lbf (76 kN)
7.8 kN total thrust 17,000 lbf (76 kN)
3,200 kg 7,050 lb MTOW 18,144 kg 40,000 lb
924 km 499 nm range 6,090 nm 11,278 km
715 km/h 444 mph cruise speed 475 mph 764 km/h
2 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.