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The
Alouette II is manufactured by Aérospatiale of France. The Alouette
II was the first production 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).
Production started initially in 1955 with orders from the French armed
forces and civilian customers, but by the time production ended in
1975 with over 1500 Alouette IIs 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.
SA-318 ALOUETTE
II Specifications |
Type |
Light Utility
Helicopter |
Manufacturer |
Aerospatiale |
Accommodation |
Two crew and up to three
passengers |
Armament |
None |
Performance |
Max
speed 130mph (210kmh) |
Main Rotor Diameter |
36ft (11m) |
Length |
33ft 8in (10.3m) |
Height |
10ft (3.3m) |
Weight |
weight empty 2,251lb (1,021kg) |
Powerplant |
One Turboméca Artouste IIIB turboshaft
producing 570shp (425kW) |
Variants |
SA-313 |
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