Gazelle

The Aérospatiale Gazelle is a five-seat helicopter, that was commonly used for light transport and reconnaissance duties in UK forces service. It is powered by a single turbine engine and was the first helicopter to feature a fenestron tail instead of a conventional tail rotor. It was designed by Sud Aviation, later Arospatiale, and manufactured in France and the UK through a joint production agreement with Westland Aircraft. The deal, signed in February 1967, allowed the production in Britain of 292 Gazelles and 48 Pumas ordered by the British armed forces; in return Aérospatiale was given a work share in the manufacturing programme for the 40 Lynx naval helicopters for the French Navy. Additionally, Westland would have a 65% work share in the manufacturing, and be a joint partner to Aérospatiale on further refinements and upgrades to the Gazelle. Westland would produce a total of 262 Gazelles of various models, mainly for various branches of the British armed forces. Gazelles for the civil market were also produced.

In 1973, 142 aircraft were on order by the UK, out of a then-intended fleet of 250. 660 Sqn, based in Salamanca Barracks, Germany, was the first British Army unit to be equipped with Gazelles, entering operational service on 6 July 1974. The Gazelles, replacements for the Sioux, were assigned the roles of reconnaissance, troop deployment, direction of artillery fire, casualty evacuation and anti-tank operations. In August 1974, 30 were based at CFS Tern Hill for RAF helicopter training.

The Royal Navy's Gazelles entered service in December 1974 with 705 Naval Air Squadron, Culdrose, to provide all-through flying training in preparation for the Lynx's service entry. A total of 23 Gazelles were ordered for Culdrose. Army-owned AH.1s also entered service with 3 Commando Brigade Air Squadron (3 CBAS) where they operated as utility and reconnaissance helicopters in support of the Royal Marines. The 12 Gazelles for 3 CBAS had entered service in 1975, by which time, there were 310 Gazelles on order for the British military.

The Gazelles that had replaced the Sioux in RAF Sek Kong towards the end of 1974 had been found unsuitable for Hong Kong and, by the end of 1975, had been returned to the UK. During its predominantly Cold War service period, the Army Gazelles flew over 660,000 hours and had over 1,000 modifications made to the aircraft. From the early 1980s, Army-operated Gazelles were fitted with the Gazelle Obvervation Aid, a gyro-stabilised sight to match their target finding capability with that of the Lynx.

The type was also frequently used to perform airborne patrols in Northern Ireland. On 17 February 1978, a British Army Gazelle crashed near Jonesborough, County Armagh, after coming under fire from the Provisional IRA during a ground skirmish.

During the Falklands War, the Gazelle played a valuable role operating from the flight decks of Royal Navy ships. Under a rapidly-performed crash programme specifically for the Falklands operation, Gazelles were fitted with 68mm SNEB rocket pods and various other optional equipment such as armour plating, flotation gear and folding blade mechanisms. Two Royal Marine Gazelles were shot down on the first day of the landings at San Carlos Water. In a high-profile incident of friendly fire on 6 June 1982, an Army Air Corps Gazelle was mistaken for a low-flying Argentine C-130 Hercules and was shot down by HMS Cardiff, a British Type 42 Destroyer.

The Gazelle also operated in a reconnaissance and liasion roles during the War in Afghanistan. In 2007, it was reported that, while many British helicopters had struggled with the conditions of the Afghan and Iraqi theatres, the Gazelle was the "best performing model" with roughly 80% being available for planned operations.

Various branches of the British military have operated Gazelles in other theatres, such as during the 1991 Gulf War against Iraq and in the 1999 intervention in Kosovo.

29 Flight Gazelle Helicopter on Training Exercise at BATUS in Canada (June 2011). Photo: ARMY IMAGE/MOD

[see page for license], via Wikimedia Commons

Specifications

Data from Airplane Magazine Vol 1 Issue 6

General characteristics

    • Crew: 2
    • Capacity: 3 Passengers
    • Length: 11.97 m (39 ft 0 in)
    • Main rotor diameter:10.5 m (34 ft 6 in)
    • Height: 3.15 m (10 ft 3 in)
    • Main rotor area: 86.5 m 2 (931 ft 2)
    • Empty weight: 908 kg (2,002 lb)
    • Gross weight: 1,800 kg (3,970 lb)
    • Powerplant: 1 x Turbomeca Astazou IIIA turboshaft, 440 kW (590 hp)

Performance

    • Maximum speed: 310 km/h (193 mph)
    • Cruising speed: 264 km/h (164 mph)
    • Range: 670 km (416 miles)
    • Service ceiling: 5,000 m (16,405 ft)
    • Rate of climb: 9 m/s (1,770 ft/min)

Sources

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*Wikipedia article ratings, in order of quality: Stub, Start, C, B, GA

Notes