|
|
|||||||
|
HKP
2 - Sud
Aviation SE.3130 Alouette II (1958-1988) |
|||||||
|
|
Page 1 (3) |
|
|||||
|
|
|||||||
![]() |
|||||||
|
Almost
1.600 Alouette II helicopters were manufactured in France by Sud
Aviation (later Aérospatiale and then Eurocopter..) during two decades.
The first one flew in 1955. Production under license continued later in
India. The Alouette II was the first helicopter design that used a gas
turbine instead of a conventional heavier piston engine. All the three military service branches in Sweden acquired the Alouette II, totally 29 helicopters. Ten of these were licence built in Sweden by SAAB in their helicopter plant at Norrköping. The Swedish designation was HKP 2. The helicopter had a crew of two and could normally carry three passengers. It had a loading capacity of 760 kg (including pilot and fuel). The engine was a Turboméca Artouste IIC, delivering 390 hp. It was given the Swedish designation TM 1.
The
HKP 2 had a fuselage of welded steel tubing. The cockpit was surrounded
by a large bubble canopy, giving the pilot sight in nearly every
direction. The landing gear could be fitted with floats or two small
wheels. Photos:Top: HKP 2 # 02034 at the destroyer HMS Småland, now floating museum at Göteborgs Maritima Centrum. Below: HKP 2 (Air Force # 02406, former Army # 02202) at Flygvapenmuseum. Bottom (b/w photo): Army # 02206 at Malmen. Length
9,7 m. Rotor dia. 10,2 m. MTOW 1.650 kg. Cruising speed 180 km/h. |
|||||||
![]() |
|||||||
|
|
|||||||
|
|
|||||||
|
|
|
||||||
|
© Lars Henriksson |
|
Updated 2008-01-02 |
|||||