France - naval aviation and armaments
Modification | Purpose | Deliveries | Number of commissioned | Discarding | Differences from the previous modification |
SE-313B | utility | 1955 - 1956 | 32 | 1997 | Turbomeca Artouste I engine (355 hp) |
SA-318C | utility | 1964 - 1965 | 32 | 1997 | Turbomeca Astazou IIA engine (530 hp) |
Modification | SE-313B |
SA-318C |
Rotor diameter, m |
10.20 | 10.20 |
Length, m |
9.70 | 9.75 |
Height, m |
2.75 | 2.75 |
Rotating area, m2 |
81.72 | 81.72 |
Empty mass, kg |
895 | 890 |
Full flying-off mass, kg |
1600 | 1650 |
Engine | 1 Turbomeca Artouste I | 1 Turbomeca Astazou IIA |
Power, h. p. | 365 | 535 |
Maximal speed, km/h | 185 | 205 |
Cruise speed, km/h | 165 | 180 |
Flying range, km | 565 | 720 |
Vertical speed, m/s | 4.2 | 6.6 |
Maximal altitude, m | 2150 | 3300 |
Complement | 1- 2 | 1 |
Armament | 3 passengers | 4 passengers |
SE-313B Alouette II
SA-318C Alouette II
© Ivan Gogin, 2009