FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
9K115-1 Metis-Mlarger figure on 1 of 2
Measured figures
Length
Single source980 mm[source]
Length
Single sourceConfiguration
| Specification | 9K115-1 Metis-M | MILAN |
|---|---|---|
| Type | Anti-tank guided missile[source] | Anti-tank missile[source] |
| Place of origin | Russia[source] | France, West Germany[source] |
| In service | 1992–present[source] | 1972–present[source] |
| Used by | See Operators[source] | See operators[source] |
MILANlarger figure on 1 of 2
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]
Operational; Metis-M
Single sourceOperational; Metis-M1
Single source1500 m (Metis-M) 80 m - 2000 m (Metis-M1)[source]
Operational; MILAN ER
Single sourceOperational; Operational range
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | 2006 Lebanon War Syrian Civil War War in Iraq (2013-2017)[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] |
|---|
| Manufacturer | KBP Instrument Design Bureau[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
|---|
| Unit cost | $15,500 per missile (2019, export cost)[source] | £7,500 (1984)[source] |
|---|
| Produced | 1992–present[source] | 1971[source] |
|---|
| Warhead | HEAT tandem warhead, Armor penetration behind ERA : 800 mm (Metis-M) 900-980 mm (Metis-M1) thermobaric anti-personnel/anti-material warhead is also available[source] | Single or tandem HEAT[source] |
|---|
| Engine | Solid-fuel rocket[source] | solid-fuel rocket[source] |
|---|
| Guidance system | SACLOS wire-guided missile[source] | SACLOS wire[source] |
|---|
| Designed | — | 1970s[source] |
|---|
| No. built | — | 350,000 missiles, 10,000 launchers[source] |
|---|
| Variants | — | See variants[source] |
|---|
| Detonation mechanism | — | contact[source] |
|---|
| Steering system | — | Jet deflector[source] |
|---|
| Launch platform | — | Individual, vehicle[source] |
|---|
| Reported operators |
|
|
|---|
200–2,000 m (660–6,560 ft); 3,000 m (MILAN ER)[source]