de Havilland Canada DHC-2 Beaver vs. Fouga CM.170 Magister
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de Havilland Canada DHC-2 Beaver |
versus |
Fouga CM.170 Magister |
13.56 m |
44 ft 6 in |
length |
10.06 m |
33 ft 0 in |
5 m |
16 ft 5 in |
height |
2.8 m |
9 ft 2 in |
16.56 m |
54 ft 4 in |
wingspan |
12.15 m |
39 ft 1 |
2 x Armstrong Siddeley Double Mamba turboprop engines |
engines |
Two Turbomeca Marboré IIA turbojets |
Approximately 3,100 hp (2,312 kW) each |
thrust per engine |
3.9 kN |
Approximately 6,200 hp (4,624 kW) total |
total thrust |
7.8 kN |
24,200 lb |
10,977 kg |
MTOW |
3,200 kg |
7,050 lb |
2,535 km |
1,369 nm |
range |
924 km |
499 nm |
228 mph |
367 km/h |
cruise speed |
715 km/h |
444 mph |
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling |
capacity |
2 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.