FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
2K12 Kublarger figure on 1 of 3
CA-95larger figure on 2 of 3
Measured figures
Length
Single source5,800 mm[source]
Length
Single sourceConfiguration
| Specification | 2K12 Kub | CA-95 |
|---|---|---|
| Type | Tracked medium-range surface-to-air missile system[source] | Vehicle-mounted SAM system[source] |
| Place of origin | Soviet Union[source] | Romania[source] |
| In service | 1967–present[source] | — |
| Used by | See list of operators[source] | Romanian Land Forces Armed Forces of Ukraine[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
5,75 m[source]
gasoline
Single sourcegasoline 140 hp (104 kW)[source]
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.
| 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] | Russian invasion of Ukraine[source] |
|---|
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | — |
|---|
| Designed | 1958–1967[source] | — |
|---|
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[source] | ROMARM[source] |
|---|
| Produced | 1968–1985[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] | 4X surface to air missiles +2 spares[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] | — |
|---|
| Armor | — | against 7.62mm rounds & shrapnel[source] |
|---|
| Secondary armament | — | 7.62mm PKT machine gun[source] |
|---|
| Power/weight | — | 20 hp/tonne[source] |
|---|
| Suspension | — | wheeled 4x4[source] |
|---|
| Reported operators |
| — |
|---|