Fouga CM.170 Magister vs. Antonov An-124 Ruslan

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Fouga CM.170 Magister versus Antonov An-124 Ruslan
10.06 m 33 ft 0 in length 69.10 m 226 ft 9 in
2.8 m 9 ft 2 in height 20.78 m 68 ft 2 in
12.15 m 39 ft 1 wingspan 73.3 m 240 ft 6 in
Two Turbomeca Marboré IIA turbojets engines 4 x Ivchenko Progress D-18T turbofan engines
3.9 kN thrust per engine Approximately 51,590 lbf
7.8 kN total thrust Approximately 206,360 lbf
3,200 kg 7,050 lb MTOW 405,000 kg 893,000 lb
924 km 499 nm range 3,700 km 1,998 nm
715 km/h 444 mph cruise speed 800 km/h 497 mph
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.