Fouga CM.170 Magister vs. Airbus H225 Super Puma
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Fouga CM.170 Magister |
versus |
Airbus H225 Super Puma |
10.06 m |
33 ft 0 in |
length |
14.06 m |
46 ft 2 in |
2.8 m |
9 ft 2 in |
height |
4.38 m |
14 ft 4 in |
12.15 m |
39 ft 1 |
wingspan |
|
|
Two Turbomeca Marboré IIA turbojets |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
3.9 kN |
thrust per engine |
2,778 hp |
7.8 kN |
total thrust |
5,556 hp |
3,200 kg |
7,050 lb |
MTOW |
11,000 kg |
24,251 lb |
924 km |
499 nm |
range |
857 km |
463 nm |
715 km/h |
444 mph |
cruise speed |
242 km/h |
150 mph |
2 |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.