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At a glance
MILANlarger figure on 2 of 5
Measured figures
Length
Single source1.2 m (3 ft 11 in)[source]
Length
Single sourceConfiguration
| Specification | MILAN | SS.11 |
|---|---|---|
| Type | Anti-tank missile[source] | MCLOS wire-guided anti-tank missile[source] |
| Place of origin | France, West Germany[source] | France[source] |
| In service | 1972–present[source] | — |
| Used by | See operators[source] | — |
| Wars | 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 |
SS.11larger figure on 3 of 5
Counts only measures both sources give with the same scope. A larger figure is not a better system.
1,190 mm (3 ft 11 in)[source]
Warhead weight
Single source6.8 kg (15 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designed | 1970s[source] | 1953[source] |
|---|
| Manufacturer | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] | Nord Aviation[source] |
|---|
| Unit cost | £7,500 (1984)[source] | — |
|---|
| Produced | 1971[source] | 1956 – mid 1980s[source] |
|---|
| No. built | 350,000 missiles, 10,000 launchers[source] | 180,000[source] |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | Single or tandem HEAT[source] | Type 140AC anti-armour[source] |
|---|
| Detonation mechanism | contact[source] | — |
|---|
| Engine | solid-fuel rocket[source] | — |
|---|
| Guidance system | SACLOS wire[source] | Manual command to line of sight[source] |
|---|
| Steering system | Jet deflector[source] | — |
|---|
| Launch platform | Individual, vehicle[source] | — |
|---|
| Designer | — | Nord Aviation[source] |
|---|
| Reported operators |
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