Sunday, November 23, 2008

deagel.com

Gazelle


IOC: 1973
Total Production: 1,255


Also Known As
Gazelle AH.1
SA 340
SA 341
SA 341B
SA 341C
SA 341D
SA 341E
SA 341F
SA 341G
SA 341H
SA 341L
SA 342
SA 342J
SA 342K
SA 342M


Origin
France
United Kingdom


Contractor/s
AgustaWestland
Eurocopter

Applications
Jeanne D'Arc



Guided Missiles:
HOT (6)

SAM & ABM Missiles:
Mistral (2)

Sensors & Communications:
Aware

Description: Gazelle is a single-engine, three-bladed helicopter developed by a joint venture between British and French rotary-wing aircraft companies aimed at replacing Alouette II. More than 1,200 helicopter of all models were produced for both civil and military customers all over the world until the mid 1990s when production ceased. Gazelle helicopter family is powered by a Turbomeca Astazou turboshaft rated at 858-shp. Eurocopter's Fenestron shrouded tail rotor was introduced on this aircraft. Militarized models perform training, reconnaissance, utility and anti-tank missions.

Military variants of Gazelle may be equipped with Mistral, HOT, AT-3 or SA-7 missile systems as well as gun pods of up to 20mm. The first Gazelle prototype was designated the SA 340. The first production model was SA 341. Gazelle powered by more powerful Astazou XIVH engines were designated SA 342. The French Army's ALAT deployed successfully Gazelles during the Gulf War in 1991 assuming primarily anti-tank missions. Currently, ALAT's anti-tank helicopters are being replaced by Tiger.

Specifications
Accommodation: Crew 2, Passengers 3

Guns: Main Gun Caliber 20 mm

Dimensions: Height 3.1 m, Length 11.9 m, Main Rotor Diameter 10.5 m, Width 2 m

Weights: Max Weight 2,000 kg (4,409 lb)

Performance: Ceiling 5,000 m (16,404 ft), Max Range 700 km (378 nm), Top Speed 86 mps (310 kph)

Power: Power 858 shp

Other: Main Rotor Blades 3, Number of Engines 1

Gazelle - Contracts, Orders & Sales

  see transactions report


 



Operators

see operators map

Angola
Burundi
Cameroon
Chad
China
Cyprus
Ecuador
Egypt
France
Gabon
Iraq
Kenya
Kuwait

As of Holdings
2005 16
Lebanon
Morocco
Qatar
Rwanda
Senegal
Serbia
Syria
United Kingdom

As of Holdings
2007 56
2006 65


Image Gallery


Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)


Last Updated: Saturday, November 22, 2008

Leave Feedback >>