Credit
Mike1979 Russia · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
9M123 Khrizantemalarger figure on 2 of 4
9M133 Kornetlarger figure on 2 of 4
Measured figures
Length
Single source2,357 mm (7.733 ft)[source]
Length
Single sourceConfiguration
| Specification | 9M123 Khrizantema | 9M133 Kornet |
|---|---|---|
| Type | Anti-tank guided missile[source] | Anti-tank missile[source] |
| Place of origin | Russia[source] | Russia[source] |
| In service | 2005–present[source] | 1998–present[source] |
| Used by | Russia[source] | See Operators[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
1200 mm[source]
Mass
Single sourcewith launch tube
Single source46 kg (101 lb) (54 kg (119 lb) with launch tube)[source]
Mass
Single sourceweight with tripod/firing unit
Single sourceMaximum; Mach 1.2
Single source400 m/s (Mach 1.2)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Libyan civil war (2011)[source] | 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 | KBM ( Kolomna )[source] | KBP Instrument Design Bureau[source] |
|---|
| Designed | 1996 ( 1996 )[source] | 1988–1998[source] |
|---|
| Manufacturer | KBMN[source] | Degtyarev plant[source] |
|---|
| Produced | 2005-present[source] | 1994–present[source] |
|---|
| Variants | 9M123, 9M123-2, 9M123F, 9M123F-2[source] | See Variants[source] |
|---|
| Warhead | Tandem-charge HEAT (9M123), thermobaric (9M123F)[source] | 1,000+ (9K135), 1,200+ (E), 1,300+ (D) mm RHA penetration after ERA with Tandem HEAT , Thermobaric[source] |
|---|
| Detonation mechanism | Impact fuze[source] | Impact fuze[source] |
|---|
| Propellant | Solid-fuel rocket[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | ACLOS radar beam riding , SACLOS laser beam riding[source] | SACLOS laser beam riding[source] |
|---|
| Steering system | Two control surfaces[source] | Two control surfaces[source] |
|---|
| Accuracy | <5 m[source] | <5 m[source] |
|---|
| Launch platform | 9P157-2 tank destroyer (based on BMP-3 chassis), Mil Mi-28 , Ka-52 Alligator[source] | Individual, vehicles, Kornet-T , Kornet-D , Bumerang-BM , Kornet-D1 , Pokpung-Ho IV[source] |
|---|
| Unit cost | — | $26,000 per missile (2019, export cost)[source] |
|---|
| No. built | — | 35,000 (2009)[source] |
|---|
| Reported operators |
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|---|
with launch tube) /
Single source27 kg (29 kg with launch tube) / 63.7 kg (weight with tripod/firing unit)[source]