Aérospatiale Alouette II
The
Alouette II is a light
helicopter originally manufactured by
Sud Aviation and later
Aérospatiale of
France. The Alouette II is the first helicopter to use a gas turbine instead of a conventional heavier piston engine.
It was mostly used for military purposes in observation, photography, air/sea rescue, liaison and training but it has also carried anti-tank missiles and homing torpedoes. As a civilian helicopter it was put to use as a casualty evacuation (with two external stretcher panniers), crop-spraying and flying crane (with a 500kg external sling load).
Although Sud-Est's previous helicopter design, the
SE.3120 Alouette, broke helicopter speed and distance records in July
1953, it was too complex an aircraft to market successfully. With the records falling, the French government started showing interest but with their financial backing the state gave an ultimatum that within 2 years a helicopter had to be in production otherwise all activities around rotary wings would cease! SNCASE came up with 7 turbo-engine helicopters designs: X.310A - X.310G. Earlier
Joseph Szydlowski, the founder of
Turboméca had successfully managed to develop the
Artouste, a 260 hp single shaft turbine engine derived from his
Orédon turbine. The X.310G design was chosen and together with the Artouste engine was fast tracked towards production as the
SE.3130 Alouette II.
The SE-3130, first flew on
March 12 1955 and within 3 months a pre-series Alouette II flown by
Jean Boulet set a new helicopter altitude record of 8,209 m on
June 6 then on
June 13 pushed the record even further to 10,984 m.
The Alouette II made the news on
July 3 1956 when it became the first helicopter to perform a mountain-rescue by evacuating a mountaineer who had suffered from cardiac arrest at over 4,000 m and again on
January 3 1957 the Alouette II was called upon to rescue the crew of a crashed
Sikorsky S-58 which was searching for missing mountaineers Jean Vincendon and François Henry on
Mont Blanc.
The Alouette II gained its domestic certificate of airworthiness on
May 2 1957.
Production started initially to fulfil orders from the French armed forces and civilian customers, but by the time production ended in
1975 with over 1500 Alouette II's had been built and in use in over 80 countries including 47 armed forces. It is also licence built in
Brazil,
Sweden,
India and in the
United States.
In
1963 the Alouette II became the first commercially operated turbine helicopter in the USA.
Indian
Hindustan Aeronautics Limited license-built SA.315B Lama called Cheetahs regulary deploy at 7500 meters (24,600 ft.) to forward observation outposts and air bases of the
Indian Air Force in the
Himalaya mountain ranges.
*
SE.3130 Alouette II - After
1967 called
SA.313B Alouette II*
SE.3131 Gouverneu - VIP version which led up to the
Alouette III*
SE.3140 Alouette II - Proposed version, it was going to be powered by a 298 kW (400hp) Turbomeca Turmo II engine. None were ever built.
*
HKP 2 Alouette II -
Swedish licence version of the SE.3130
*
SE.3150 Alouette Astazou - It has a 550 shp Turboméca Astazou IIA shaft turbine (derated to 360 shp) and strengthened transmission system of the
Alouette III*
SE.3180 Alouette II - After
1967 called
SA.318C Alouette II derived from the SE.3150
*
HAL Chetak -
Indian licence version of the SE.3180
*
SA-315B Lama - Derived from the SE.3150, it was designed for high altitude operations using a 650kW (870shp) Turboméca Astazou IIIB turboshaft, derated to 410kW (550shp). This derivative still holds the absolute altitude record for all types of helicopters since 1972: 12,442 m.
*
HAL Cheetah - Indian licence built version of the SA.315B Lama.
*
HAL Lancer - modified and updated version of Cheetah.
*
HB 315B Gaviao - Brazilian licence built version of the SA.315B Lama.
*
Angola,
Argentina,
Austria (16)
*
Belgium (39)
*
Benin,
Bolivia,
*
Brazil,
*
Cambodia (8)
*
Cameroon,
*
Central African Republic,
*
Chile,
*
Congo (3)
*
Côte d'Ivoire (2)
*
Djibouti,
*
Dominican Republic (2)
*
Ecuador,
*
El Salvador,
*
France (363)
*
Germany (267)
*
Guinea-Bissau,
*
India (over 250 built under license as the HAL Cheetah)
*
Indonesia (3)
*
Israel (4)
*
Laos (2)
*
Lebanon (3)
*
Mexico (2)
*
Morocco (7)
*
Netherlands (8)
*
Peru (6)
*
Portugal (7)
*
Senegal,
*
South Africa (7)
*
Sweden (25)
*
Switzerland (30)
*
Togo,
*
Tunisia (8)
*
Turkey,
*
United Kingdom (17)
|
Orthographically projected diagram of the Aérospatiale Alouette II. |
{{aircraft specifications
plane or copter?=copter | jet or prop?=prop
| crew=1 | capacity=4 passengers | length main=9.70 m | length alt=31 ft 10 in | span main=10.20 m | span alt=33 ft 6 in | height main=2.75 m | height alt=9 ft 0 in | area main=81.7 m² | area alt=879.4 ft² | empty weight main=895 kg | empty weight alt=1,975 lb | loaded weight main= | loaded weight alt= | max takeoff weight main=1,600 kg | engine (prop)=Turboméca Artouste IIC6 | type of prop=turboshaft | number of props=1 | power main=410 kW | max speed main=185 km/h | max speed alt=99.9 knots, 115 mph | range main=565 km | range alt=305 nm, 350 mi | ceiling main=2,250 m | ceiling alt=7,380 ft | climb rate main=4.2 m/s | climb rate alt=825 ft/min | loading main= | loading alt= | power/mass main= | power/mass alt={{aircontent|related=|similar aircraft=|sequence= * SE.310 - SE.311 - SE.312 - SE.313 - SE.314 - SE.315 - SE.316 - SA.318 - SA.319 - SA.320 - SA.321|lists= * List of civil aircraft * List of helicopters * List of utility aircraft
|