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At a glance
9M123 Khrizantemalarger figure on 5 of 5
MILAN
Measured figures
Length
Single source2,357 mm (7.733 ft)[source]
Length
Single sourceConfiguration
| Specification | 9M123 Khrizantema | MILAN |
|---|---|---|
| Type | Anti-tank guided missile[source] | Anti-tank missile[source] |
| Place of origin | Russia[source] | France, West Germany[source] |
| In service | 2005–present[source] | 1972–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.
1.2 m (3 ft 11 in)[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] | South African Border War Chadian-Libyan conflict Toyota War Western Sahara War Lebanese Civil War Iran–Iraq War Falklands War Gulf War 2003 invasion of Iraq Iraq War Opération Licorne Libyan Civil War Northern Mali Conflict Operation Sangaris War in Iraq (2013–2017) Syrian Civil War Russian invasion of Ukraine[source] |
|---|
| Designer | KBM ( Kolomna )[source] | — |
|---|
| Designed | 1996 ( 1996 )[source] | 1970s[source] |
|---|
| Manufacturer | KBMN[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
|---|
| Produced | 2005-present[source] | 1971[source] |
|---|
| Variants | 9M123, 9M123-2, 9M123F, 9M123F-2[source] | See variants[source] |
|---|
| Warhead | Tandem-charge HEAT (9M123), thermobaric (9M123F)[source] | Single or tandem HEAT[source] |
|---|
| Detonation mechanism | Impact fuze[source] | contact[source] |
|---|
| Propellant | Solid-fuel rocket[source] | — |
|---|
| Guidance system | ACLOS radar beam riding , SACLOS laser beam riding[source] | SACLOS wire[source] |
|---|
| Steering system | Two control surfaces[source] | Jet deflector[source] |
|---|
| Accuracy | <5 m[source] | — |
|---|
| Launch platform | 9P157-2 tank destroyer (based on BMP-3 chassis), Mil Mi-28 , Ka-52 Alligator[source] | Individual, vehicle[source] |
|---|
| Unit cost | — | £7,500 (1984)[source] |
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| No. built | — | 350,000 missiles, 10,000 launchers[source] |
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| Engine | — | solid-fuel rocket[source] |
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| Reported operators |
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