Loading the evidence…
Preparing your view.
Preparing your view.

BAnti-tank weapons
Air-to-surface missile Air-to-air missile Surface-to-surface missile Anti-tank guided missile
At a glance
9M133 Kornetlarger figure on 0 of 3
PARS 3 LRlarger 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
Maximum; Maximum speed
Single source1,044 kilometres per hour (290 m/s)[source]
HEAT
Single source4.6 kg (10 lb) HEAT[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | 9M133 Kornet | PARS 3 LR |
|---|---|---|
| Type | Anti-tank missile[source] | Air-to-surface missile Air-to-air missile Surface-to-surface missile Anti-tank guided missile[source] |
| Place of origin | Russia[source] | Germany[source] |
| In service | 1998–present[source] | — |
| Used by | See Operators[source] | — |
| Wars | Iraq War 2006 Lebanon War Israeli–Palestinian conflict 2021 Israel–Palestine crisis Gaza war Libyan Crisis (2011–present) Syrian Civil War War in Iraq (2013–2017) Russo-Ukrainian War Russo-Ukrainian war (2022–present) Yemeni Civil War Saudi Arabian-led intervention in Yemen Sinai insurgency 2020 Nagorno-Karabakh conflict[source] | — |
| Designer | KBP Instrument Design Bureau[source] | — |
| Designed | 1988–1998[source] | 1988–2011[source] |
| Manufacturer | Degtyarev plant[source] | Parsys GmbH, MBDA Deutschland GmbH , Diehl BGT Defence ,[source] |
| Unit cost | $26,000 per missile (2019, export cost)[source] | €600,000[source] |
| Produced | 1994–present[source] | 2012–present[source] |
| No. built | 35,000 (2009)[source] | — |
| Variants | See Variants[source] | see text[source] |
| Warhead | 1,000+ (9K135), 1,200+ (E), 1,300+ (D) mm RHA penetration after ERA with Tandem HEAT , Thermobaric[source] | 9 kg (19.84 lb) tandem HEAT 1,000+ mm RHA penetration after ERA from TDW[source] |
| Detonation mechanism | Impact fuze[source] | impact[source] |
| Propellant | Solid-fuel rocket[source] | — |
| Guidance system | SACLOS laser beam riding[source] | Target acquisition: passive IR and television CCD sensors in a mast mounted on launching helicopter Missile guidance: passive IR CCD sensors in the missile[source] |
| Steering system | Two control surfaces[source] | — |
| Accuracy | <5 m[source] | — |
| Launch platform | Individual, vehicles, Kornet-T , Kornet-D , Bumerang-BM , Kornet-D1 , Pokpung-Ho IV[source] | Helicopter[source] |
| Engine | — | solid fuel rocket[source] |
| Reported operators |
| — |