FORCETALLY
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At a glance
2K12 Kublarger figure on 0 of 1
HQ-19larger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | 2K12 Kub | HQ-19 |
|---|---|---|
| Speed | Mach 2.8[source] | 10 kilometres per second (6.2 mi/s)[source] |
| Type | Tracked medium-range surface-to-air missile system[source] | Surface to air missile Anti-Ballistic Missile Anti-Satellite missile[source] |
| Place of origin | Soviet Union[source] | China[source] |
| In service | 1967–present[source] |
Wingspan
Single source1.245 m[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.
2018 - present[source] |
| Used by | See list of operators[source] | People's Liberation Army Air Force[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] | — |
|---|
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | — |
|---|
| Designed | 1958–1967[source] | — |
|---|
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[source] | — |
|---|
| Produced | 1968–1985[source] | 1990s-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] | 200 km[source] |
|---|
| Launch platform | 2P25 TEL[source] | TAS5380 TEL[source] |
|---|
| Developed from | — | HQ-9[source] |
|---|
| Reported operators |
| — |
|---|