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BAir defence
Kinetic anti ballistic missile ( Aegis Ballistic Missile Defense System )
At a glance
2K12 Kublarger figure on 0 of 3
RIM-161 Standard Missile 3larger figure on 3 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Operational; Operational range
Single source24 kilometres (15 mi)[source]
Operational; Block IA/B
Single sourceOperational; Block IIA range and flight ceiling 900 – 1,050 km (depending on the type of target)
Single sourceBlock IA/B: 900–1,200 km (560–750 mi) Block IIA: 1,200 km range and flight ceiling 900 – 1,050 km (depending on the type of target)[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 | RIM-161 Standard Missile 3 |
|---|---|---|
| Speed | Mach 2.8[source] | 3 km/s (Mach 8.8) Block IA/B 4.5 km/s (Mach 13.2) Block IIA[source] |
| Type | Tracked medium-range surface-to-air missile system[source] | Kinetic anti ballistic missile ( Aegis Ballistic Missile Defense System )[source] |
| Place of origin | Soviet Union[source] | United States, Japan (Block IIA)[source] |
| In service | 1967–present[source] | 2014–present (Block IB)[source] |
| Used by | See list of operators[source] | United States Navy Japan Maritime Self-Defense Force Republic of Korea Navy Aegis Ashore: Romania Poland[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] | April 2024 Iranian strikes on Israel 2026 Iran war[source] |
| Designer | NIIP / Vympel MMZ ( GM chassis )[source] | — |
| Designed | 1958–1967[source] | — |
| Manufacturer | Ulyanovsk Mechanical Plant (SURNs) ZiK (TELs)[source] | RTX , Aerojet , ( Mitsubishi Heavy Industries Block IIA)[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] | GPS / INS / semi-active radar homing /passive LWIR infrared homing seeker (KW)[source] |
| Warhead | Frag-HE[source] | Lightweight Exo-Atmospheric Projectile (LEAP) kinetic warhead[source] |
| Detonation mechanism | Contact and proximity[source] | — |
| Propellant | integral rocket motor/ramjet booster and sustainer motor[source] | Stage 1: Mk 72 booster , solid-fuel , Aerojet Stage 2: MK 104 Dual Thrust Rocket Motor (DTRM), solid-fuel, Aerojet Stage 3: MK 136 Third Stage Rocket Motor (TSRM), solid-fuel, ATK Stage 4: Throttleable Divert and Attitude Control System (TDACS), Aerojet[source] |
| Flight altitude | Max. 14,000 metres (46,000 ft) Min. 100 metres (330 ft)[source] | — |
| Launch platform | 2P25 TEL[source] | — |
| Unit cost | — | US$9–25 million (2011) US$ 18.4m (FY2018) US$ 11.83m (FY2021)[source] |
| Reported operators |
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