FORCETALLY
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Measured figures
Operational; Operational range
Single source24 kilometres (15 mi)[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.
Configuration
| Specification | 2K12 Kub | FB-10 |
|---|---|---|
| Speed | Mach 2.8[source] | — |
| Type | Tracked medium-range surface-to-air missile system[source] | mobile short-range air defense missile system[source] |
| Place of origin | Soviet Union[source] | — |
| In service | 1967–present[source] | — |
| Used by | See list of 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] | — |
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | Shanghai Academy of Spaceflight Technology of China Aerospace Science and Technology Corporation (CASC)[source] |
| Designed | 1958–1967[source] | — |
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[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] | — |
| 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] | — |
| guidance | — | Radio command + imaging infrared (IIR) homing seeker[source]FB-10A / HQ-13 specification only, not FB-10 original spin-stabilized missile with a imaging infrared (IIR) homing seeker[source]FB-10 original missile only; not FB-10A |
| Engagement altitude | — | 15 to 5,000 meters (49 to 16,404 feet)[source]FB-10 original missile 7,500 m (24,600 ft)[source]FB-10A / HQ-13 missile only |
| Chassis | — | Dongfeng Mengshi chassis[source]HQ-13 / FB-10A platform |
| Armament | — | The missile launch vehicle variant carries eight HQ-13 (FB-10A) missiles, while the gun-missile vehicle (SWS3) variant carries a 35mm single-barrel autocannon with two HQ-13 (FB-10A) missiles[source] |
| Sensors and processing systems | — | command vehicle carries an active electronically scanned array (AESA) search radar with 50 km (31 mi) range, while the launch vehicles carries a targeting radar and an electro-optical tracking system[source]HQ-13 battery command and launch-vehicle sensors |
| Alternative designation | — | HQ-13[source] |
| Reported operators |
| — |