

Preparing your view.



At a glance
Eryx (missile)larger figure on 1 of 4
Measured figures
Length
Single source0.905 m (2.97 ft)[source]
Length
Single sourceConfiguration
| Specification | Eryx (missile) | MILAN |
|---|---|---|
| Type | Anti-tank guided missile[source] | Anti-tank missile[source] |
| Place of origin | France[source] | France, West Germany[source] |
| In service | 1994–present[source] | 1972–present[source] |
| Used by | See Operators[source] | See operators[source] |
MILANlarger figure on 3 of 4
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]
Eryx · Calibre
Single source160 mm[source]Eryx
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Yemeni Civil War (2015-present) Saudi-led intervention in Yemen[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] |
|---|
| Designed | 1985–1992[source] | 1970s[source] |
|---|
| Manufacturer | MBDA France, MKEK (under license)[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
|---|
| Produced | From 1993[source] | 1971[source] |
|---|
| Warhead | 137 mm diameter 3.6 kg tandem HEAT (penetrating 900 mm RHA behind reactive armour , or 2.5 m through concrete )[source] | Single or tandem HEAT[source] |
|---|
| Guidance system | SACLOS wire[source] | SACLOS wire[source] |
|---|
| Launch platform | Man-portable Vehicle-launched[source] | Individual, vehicle[source] |
|---|
| Unit cost | — | £7,500 (1984)[source] |
|---|
| No. built | — | 350,000 missiles, 10,000 launchers[source] |
|---|
| Variants | — | See variants[source] |
|---|
| Detonation mechanism | — | contact[source] |
|---|
| Engine | — | solid-fuel rocket[source] |
|---|
| Steering system | — | Jet deflector[source] |
|---|
| Reported operators |
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