Air Weapons

Utility (1973)

Aérospatiale

SA 341 Gazelle

SA 341 Gazelle

The Aérospatiale SA 341 Gazelle began as a result of the Aviation Légère's (ALAT) requirement for a light observation helicopter. It shared a number of similarities with the Alouette family but introduced a new enclosed fuselage, a German-built rotor, and most revolutionary, a patented Fenestron ducted fan anti-torque tail rotor which would soon become commonplace in many modern Aérospatiale (and later Eurocopter) designs . The Fenestron is unique in that the rotor is enclosed within the tail skin thus making it more safe for ground crew in addition to being much quieter than conventional tail rotors. Eventually it was realized that the Gazelle would make an excellent attakc platform and was therefore equipped with cannons, rockets, and anti-tank missiles in addition to advanced avionics to reduce pilot workload. The Gazelle has seen extensive action in the Falklands, the Gulf War, Kosovo, among countless other minor conflicts and has been adopted by some 30 nations which include license production in the United Kingdom (Westland), Yugoslavia (SOKO), and Egypt (Arab British Helicopter Company).

The Gazelle was initially developed as the SA 340 prototype which included the Alouette III's conventional rotor in place of the Fenestron type. It was first flown on 7 April 1967 entering service in the early 1970s as the SA 341. The British were a major user of the Gazelle and a number of variants were used exclusively by the Army, (SA 341B), Royal Navy (SA 341C) and the RAF (SA 341D), known in service as the Gazelle AH.1, HT.2, and HT.3 respectively. In French service, the Gazelle was eventually fitted with an uprated powerplant and designated SA 341F while in Yugoslavia, a SOKO-built version was known as the SA 341H and was the first to feature anti-tank and anti-helicopter armament (specifically, AT-3 and SA-7 missiles). Similar French developments led to the SA 342 with more powerful engines and numerous weapon configurations. Export military and civilian versions were known the SA 342J and SA 342L respectively while the more capable and advanced SA 342M was used by the French for the anti-tank and helicopter escort roles.

Preceded by:

SA 316 Alouette III (1961)

Succeeded by:

EC 665 Tigre (2003)

Datafile

DesignSA 341FSA 342M
NameGazelleGazelle
TypeUtilityClose Support
Year19731980
Crew22
Dimensions
Length39 ft 3½ in39 ft 3½ in
Height10 ft 5½ in10 ft 5½ in
Rotor Diameter
Rotor Disc Area
Wing Span34 ft 5 in34 ft 5 in
Wing Arean/an/a
Weight
Empty2,022 lbs2,150 lbs
Maximum3,968 lbs4,189 lbs
Wing Loading4.3 lb/ft²4.5 lb/ft²
Performance
Speed164 mph193 mph
Ceiling16,404 ft14,108 ft
Range416 mi469 mi
Powerplant
Engine1 x Astazou IIIA
Turbomeca
590 hp
1 x Astazou XIVM
Turbomeca
858 hp
Thrust/Weight0.580.80
Armament
Guns1 x 20-mm
1 x 20-mm
Payload1,477 lbs1,620 lbs
Hardpoints-2
AS Weapons-AS.12
HOT
Production
Builtn/a150
Total1,775