Derived from SE.3200 Frelon
1962
Specifications
| Engine | 3 x Safran Turmo III C7 1274 shp |
|---|---|
| Capacity | 5 + 27 |
| Length (m) | 23 |
| Height (m) | 6.6 |
| Blades | 6 |
| Rotor diam. (m) | 18.9 |
| Disc area (m2) | 280 |
| Weight (kgs) | Empty: 6800 Max: 13000 |
| Speed (km/h) | Max: 270 |
| Range (km) | 1000 |
| Ceiling (m) | 3100 |
| Rate/Climb (m/min) | 402 |
Derivatives & Versions
| SA321F Super Frelon | 1966 | Commercial transport version for 37 passengers. |
| SA321G Super Frelon | 1966 | Anti-submarine version and the first version to enter production, following an initial order of 17 from the French Government in Oct 1965. |
| SA321K Super Frelon | 1966 | Israel military transport version |
| SA321L Super Frelon | 1968 | South Africa military transport version |
| SA321M Super Frelon | 1971 | Military transport version for Libya, with Turmo IIIE6 engines but without radar or floatation gear. |
| SA321J Super Frelon | 1975 | Commercial transport version for 27 passengers |
| SA321H Super Frelon | 1976 | Export version for Iraq, with Turbomeca Turmo IIIE engines, Omera search radar and Exocet capable. |
| → Z-8 | 1985 |