FORCETALLY
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Measured figures
Configuration
| Specification | 2K12 Kub | Aselsan Gökdeniz |
|---|---|---|
| Speed | Mach 2.8[source] | — |
| Type | Tracked medium-range surface-to-air missile system[source] | Gun-based CIWS[source] |
| Place of origin | Soviet Union[source] | Turkey[source] |
| In service | 1967–present[source] | — |
| Used by | See list of operators |
Wingspan
Single source1.245 m[source]
Warhead weight
Single source59 kg[source]
2 x
Single sourceRate of fire
Single source1100 rpm (2 x 550 rpm)[source]
ATOM 35mm
Single sourceHEI-T
Single sourceATOM 35mm: 1,020 m/s (3,300 ft/s) HEI-T: 1,175 m/s (3,850 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| 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] | — |
|---|
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | Aselsan[source] |
|---|
| Designed | 1958–1967[source] | — |
|---|
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[source] | Aselsan[source] |
|---|
| Produced | 1968–1985[source] | 2019-Present[source] |
|---|
| No. built | 500 launchers, 10,000 missiles[source] | — |
|---|
| Variants | 2K12 Kub, 2K12E Kvadrat (export version), 2K12M3, 2K12M4[source] | — |
|---|
| Main armament | 3 3M9M4(or variants) guided missiles[source] | — |
|---|
| Engine | Integral rocket motor/ ramjet booster and sustainer motor[source] | — |
|---|
| Guidance system | Command guidance with terminal semi-active radar homing (SARH)[source] | — |
|---|
| Warhead | Frag-HE[source] | — |
|---|
| Detonation mechanism | Contact and proximity[source] | — |
|---|
| 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] | — |
|---|
| Shell | — | 35×228mm ATOM, 35×228mm HEI-T[source] |
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| Shell weight | — | ATOM 35mm: 1.750 kg (3 lb 14 oz) HEI-T: 1.565 kg (3 lb 7 oz)[source] |
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| Barrels | — |
|---|
| Action | — | Gas-operated[source] |
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| Traverse | — | 360°[source] |
|---|
| Feed system | — | Automatic linkless[source] |
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| Alternative designation | — | GOKDENIZ[source] |
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| Reported operators |
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