Sea Skua | |
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Sea Skua missile on a Westland Lynx of the German Navy
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Type | Air-to-surface missile |
Place of origin | United Kingdom |
Service history | |
In service | 1982 |
Used by | See operators |
Wars | Falklands War, Gulf War |
Production history | |
Designer | British Aircraft Corporation |
Designed | 1972 |
Manufacturer | British Aircraft Corporation (1972-1977) BAe Dynamics (1977-1999) MBDA (UK) Ltd (since 1999) |
Produced | 1975 |
Specifications | |
Weight | 145 kg |
Length | 2.5 m |
Diameter | 0.25 m |
Warhead | 30 kg SAP, 9 kg RDX |
Detonation
mechanism |
Impact Fuze, delayed detonation. |
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|
Engine | solid fuel booster / solid fuel sustainer |
Wingspan | 0.72 m |
Operational
range |
25 km |
Speed | Mach 0.8 + |
Guidance
system |
semi-active radar homing |
Steering
system |
control surfaces |
Launch
platform |
Westland Lynx, Combattante BR-42 FAC |
The Sea Skua is a British lightweight short-range air-to-surface missile (ASM) designed for use from helicopters against ships. It is primarily used by the Royal Navy on the Westland Lynx. Although the missile is intended for helicopter use, Kuwait employs it in a shore battery and on their Umm Al Maradem (Combattante BR-42) fast attack craft.
The British Aircraft Corporation (BAC) began development of the weapon in May 1972. The British Government authorised its production in October 1975. At the time, the missile was known as CL834. In November 1979 the first launches took place at the Aberporth Range in Cardigan Bay. Three missiles were launched from the ground and three by helicopters. Further tests were made and in July 1981, full-scale production was ordered of the new missile, now called "Sea Skua".
With the missile weighing only 320 pounds (150 kg) at launch, a Lynx helicopter can carry up to four (two on each wing pylon). The booster is a Royal Ordnance (now Roxel UK) "Redstart" steel body, while the sustainer is a Royal Ordnance "Matapan" light alloy body. The missile flies at high subsonic speed to a range of up to 15.5 miles (24.9 km). The official range is declared to be 15 km, but this is widely exceeded. The missile has two sensors: a semi-active radar homing system by Marconi Defence Systems, and a Thomson-TRT AHV-7 radar altimeter (which is also used by the Exocet missile), built under licence by British Aerospace Defence Systems.
It can be set to travel at one of four pre-selected heights, depending on the surface conditions. Near the target, the missile climbs to a height at which it can "acquire" the target. The launching helicopter illuminates the target with its radar (originally the specially developed Ferranti Seaspray in the case of the Lynx), and the missile's homing head homes in on the reflected energy. On impact it penetrates the hull of a ship before detonating the 62 pounds (28 kg) blast fragmentation warhead. A semi armour piercing (SAP) warhead is also available; this contains 9 kilograms (20 lb) of RDX, aluminium and wax. The fuze is an impact-delayed model.