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At a glance
Measured figures
Length
Single source5,800 mm[source]
Sea Wolf · Length
Single sourceConfiguration
| Specification | 2K12 Kub | Sea Wolf (missile) |
|---|---|---|
| Type | Tracked medium-range surface-to-air missile system[source] | Surface-to-air[source]Sea Wolf |
| Place of origin | Soviet Union[source] | United Kingdom[source]Sea Wolf |
| In service | 1967–present[source] | Since 1979[source]Sea Wolf |
| Used by | See list of operators |
1.9 m (6 ft 2.8 in )[source]Sea Wolf
Warhead weight
Single source59 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
See operators[source]Sea Wolf |
| Wars | List Yom Kippur War Angolan Civil War Chadian Civil War Western Sahara War Iran–Iraq War 1982 Lebanon War Gulf War Yugoslav wars Kosovo War Syrian Civil War Russo-Ukrainian War Russian invasion of Ukraine Yemeni Civil War (2014–present) 2020 Nagorno-Karabakh war[source] | Falklands War , Gulf War[source]Sea Wolf |
|---|
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | British Aircraft Corporation[source]Sea Wolf |
|---|
| Designed | 1958–1967[source] | 1967[source]Sea Wolf |
|---|
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[source] | British Aircraft Corporation (1967–1977) BAe Dynamics (1977–1999) MBDA UK (since 1999)[source]Sea Wolf |
|---|
| Produced | 1968–1985[source] | 1979[source]Sea Wolf |
|---|
| No. built | 500 launchers, 10,000 missiles[source] | — |
|---|
| Variants | 2K12 Kub, 2K12E Kvadrat (export version), 2K12M3, 2K12M4[source] | Electronics; GWS-25, GWS-26, GWS-27 Vertical Launch[source]Sea Wolf |
|---|
| Main armament | 3 3M9M4(or variants) guided missiles[source] | — |
|---|
| Engine | Integral rocket motor/ ramjet booster and sustainer motor[source] | Blackcap solid fuel sustainer[source]Sea Wolf |
|---|
| Guidance system | Command guidance with terminal semi-active radar homing (SARH)[source] | Automatic Command to Line-Of-Sight (ACLOS)[source]Sea Wolf |
|---|
| Warhead | Frag-HE[source] | 14 kg (30.9 lb) HE blast-fragmentation[source]Sea Wolf |
|---|
| Detonation mechanism | Contact and proximity[source] | Direct contact / proximity fuze activated[source]Sea Wolf |
|---|
| Propellant | integral rocket motor/ramjet booster and sustainer motor[source] | — |
|---|
| Flight altitude | Max. 14,000 metres (46,000 ft) Min. 100 metres (330 ft)[source] | — |
|---|
| Launch platform | 2P25 TEL[source] | Ship[source]Sea Wolf |
|---|
| Flight ceiling | — | 3,000 m (9,842.5 ft)[source]Sea Wolf |
|---|
| Steering system | — | Control surfaces[source]Sea Wolf |
|---|
| Former operator · United Kingdom | — | United Kingdom[source] |
|---|
| Former operator · Chile | — | Chile[source] |
|---|
| Former operator · Indonesia | — | Indonesia[source] |
|---|
| Reported operators |
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