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At a glance
APILASlarger figure on 1 of 2
MILANlarger figure on 1 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source1,300 mm (51.2 in)[source]
Length
Single sourceConfiguration
| Specification | APILAS | MILAN |
|---|---|---|
| Type | Anti-tank weapon[source] | Anti-tank missile[source] |
| Place of origin | France[source] | France, West Germany[source] |
| In service | 1985-present[source] | 1972–present[source] |
| Used by | See Operators[source] | See operators[source] |
1.2 m (3 ft 11 in)[source]
Maximum; Maximum speed
Single source200 m/s (660 ft/s)[source]
Barrel length
Single source180 mm (7.1 in)[source]
Muzzle velocity
Single source293 m/s (961 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | South African Border War Gulf War Syrian Civil War[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 | GIAT Industries[source] | — |
|---|
| Manufacturer | GIAT Industries[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
|---|
| Unit cost | €2,000[source] | £7,500 (1984)[source] |
|---|
| Produced | 1985-2006[source] | 1971[source] |
|---|
| No. built | 120,000[source] | 350,000 missiles, 10,000 launchers[source] |
|---|
| Role | portable one-shot 112 mm recoilless anti-tank rocket launcher[source] | — |
|---|
| Designed | — | 1970s[source] |
|---|
| Variants | — | See variants[source] |
|---|
| Warhead | — | Single or tandem HEAT[source] |
|---|
| Detonation mechanism | — | contact[source] |
|---|
| Engine | — | solid-fuel rocket[source] |
|---|
| Guidance system | — | SACLOS wire[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]