Amercom – Aérospatiale SA313 Alouette II , French Army , France 1972
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-sběratelský model vrtulníku Aérospatiale SA313 Alouette II 1/72 -provedení: kovový model s plastovými částmi
Aérospatiale Alouette II
The Aérospatiale Alouette II (French pronunciation: [alwɛt], Lark; company designations SA 313 and SA 318) is a French light helicopter originally manufactured by Sud Aviation and later Aérospatiale. It holds the distinction of being the first production helicopter to be powered by a gas turbine engine instead of the conventional heavier piston powerplant.
| Role | Light helicopter |
|---|---|
| National origin | France |
| Manufacturer | Sud Aviation Aérospatiale |
| First flight | 12 March 1955 |
| Introduction | 2 May 1957 |
| Status | In service |
| Primary users | French Army French Air Force German Army Swiss Air Force |
| Produced | 1956–1975 |
| Number built | 1,300+ |
| Variants | Aérospatiale SA 315B Lama |
| Developed into | Aérospatiale Alouette III |
General characteristics
- Crew: One
- Capacity: Four passengers
- Length: 9.66 m (31 ft 9 in)
- Rotor diameter: 10.20 m (33 ft 6 in)
- Height: 2.75 m (9 ft 0 in)
- Disc area: 81.7 m² (881.4 ft²)
- Empty weight: 895 kg (1,973 lb)
- Max. takeoff weight: 1,600 kg (3,527 lb)
- Powerplant: One × Turbomeca Artouste IIC6 turboshaft, 395 kW (530 hp) derated to 269 kW (460 hp) each
Performance
- Maximum speed: 185 km/h (100 knots, 115 mph) at sea level
- Cruise speed: 170 km/h (92 knots, 106 mph)
- Range: 565 km (305 nmi, 350 mi)
- Endurance: 4.1 hours
- Service ceiling: 2,300 m (7,545 ft)
- Rate of climb: 4.2 m/s (820 ft/min)
