FORCETALLY
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At a glance
2K12 Kublarger figure on 0 of 4
S-200 missile system
Measured figures
Length
Single source5,800 mm[source]
second stage only
Single sourceConfiguration
| Specification | 2K12 Kub | S-200 missile system |
|---|---|---|
| Type | Tracked medium-range surface-to-air missile system[source] | Strategic SAM system[source] |
| Place of origin | Soviet Union[source] | Soviet Union[source] |
| In service | 1967–present[source] | 1967–present[source] |
| Used by | See list of operators[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
with boosters
Single source10,764 mm (35.315 ft) (with boosters) 10,452 mm (34.291 ft) (second stage only)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
See list of present and former operators[source] |
| 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] | First Libyan Civil War Syrian civil war Russo-Ukrainian war[source] |
|---|
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | KB-1 design bureau (system), GSKB Spetsmash (launcher)[source] |
|---|
| Designed | 1958–1967[source] | 1964[source] |
|---|
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[source] | Almaz-Antey[source] |
|---|
| Produced | 1968–1985[source] | — |
|---|
| No. built | 500 launchers, 10,000 missiles[source] | — |
|---|
| Variants | 2K12 Kub, 2K12E Kvadrat (export version), 2K12M3, 2K12M4[source] | S-200A, S-200V, S-200M, S-200VE, S-200D, S-200C[source] |
|---|
| Main armament | 3 3M9M4(or variants) guided missiles[source] | — |
|---|
| Engine | Integral rocket motor/ ramjet booster and sustainer motor[source] | Main: Dual-thrust liquid-fueled rocket engine Boosters: 4 solid-fueled strap-on rocket boosters[source] |
|---|
| Guidance system | Command guidance with terminal semi-active radar homing (SARH)[source] | Semi-active radar homing[source] |
|---|
| Warhead | Frag-HE[source] | Frag-HE[source] |
|---|
| Detonation mechanism | Contact and proximity[source] | Proximity and command fusing[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] | — |
|---|
| Flight ceiling | — | 40,800 metres (133,900 ft)[source] |
|---|
| Boost time | — | 3–5.1 seconds[source] |
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| Reported operators |
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