Credit
Rama · CC BY-SA 2.0 fr · Resized · CC BY-SA 2.0 fr · Source ↗ · Modified
FORCETALLY
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At a glance
MILANlarger figure on 1 of 1
Measured figures
Length
Single source1.2 m (3 ft 11 in)[source]
Missile
Single sourceConfiguration
| Specification | MILAN | RK-3 Corsar |
|---|---|---|
| Type | Anti-tank missile[source] | ATGM[source] |
| Place of origin | France, West Germany[source] | Ukraine[source] |
| In service | 1972–present[source] | 2017-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 |
RK-3 Corsarlarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Missile: 1.16 metres (3.8 ft)[source]
Mass
Single source16.4 kg[source]
Launcher w/ thermal imager
Single sourceMissile in container
Single sourceMount
Single sourceTotal system
Single sourceTotal system: 35.8 kilograms (79 lb) Launcher w/ thermal imager: 12 kg (26 lb) Mount: 8.3 kg (18 lb) Missile in container: 15.5 kg (34 lb)[source]
Maximum; Maximum speed
Single source200 m/s (660 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
War in Donbas Russian invasion of Ukraine[source] |
| Designed | 1970s[source] | since 2005[source] |
|---|
| Manufacturer | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] | Luch[source] |
|---|
| Unit cost | £7,500 (1984)[source] | USD 20 000 (July 2013)[source] |
|---|
| Produced | 1971[source] | — |
|---|
| No. built | 350,000 missiles, 10,000 launchers[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | Single or tandem HEAT[source] | RK-3K: Tandem-charge HEAT RK-3OF: HE-fragmentation[source] |
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| Detonation mechanism | contact[source] | contact[source] |
|---|
| Engine | solid-fuel rocket[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | SACLOS wire[source] | laser beam riding[source] |
|---|
| Steering system | Jet deflector[source] | — |
|---|
| Launch platform | Individual, vehicle[source] | — |
|---|
| Designer | — | "Luch" State Kyiv Design Bureau[source] |
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| Reported operators |
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