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At a glance
9M113 Konkurslarger figure on 4 of 5
Measured figures
Length
Single sourcewithout gas generator
Single sourceConfiguration
| Specification | 9M113 Konkurs | MILAN |
|---|---|---|
| Type | Anti-tank missile[source] | Anti-tank missile[source] |
| Place of origin | Soviet Union[source] | France, West Germany[source] |
| In service | 1974–present[source] | 1972–present[source] |
| Used by | See operators[source] | See operators[source] |
MILANlarger figure on 1 of 5
Counts only measures both sources give with the same scope. A larger figure is not a better system.
1,150 mm (45 in) 875 mm (34.4 in) without gas generator[source]
Length
Single source1.2 m (3 ft 11 in)[source]
Operational; Operational range
Single sourceOperational; to
Single source70 m (230 ft) to 4 km (2.5 mi)[source]
Operational; Operational range
Single sourceOperational; MILAN ER
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Syrian Civil War War in Iraq (2013-2017) War in Donbas Yemeni Civil War (2014-present) Saudi-led intervention in Yemen 2020 Nagorno-Karabakh conflict Russo-Ukrainian 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] |
|---|
| Designed | 1970[source] | 1970s[source] |
|---|
| Manufacturer | Tula Machinery Design Bureau (Tula KBP) – Tulsky Oruzheiny Zavod Bharat Dynamics Limited[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
|---|
| Variants | 9M113M[source] | See variants[source] |
|---|
| Warhead | 2.7 kg (6.0 lb) 9N131 HEAT[source] | Single or tandem HEAT[source] |
|---|
| Detonation mechanism | Contact[source] | contact[source] |
|---|
| Engine | Solid-fuel rocket[source] | solid-fuel rocket[source] |
|---|
| Guidance system | Wire-guided SACLOS[source] | SACLOS wire[source] |
|---|
| Steering system | Two control surfaces[source] | Jet deflector[source] |
|---|
| Launch platform | Individual, vehicle[source] | Individual, vehicle[source] |
|---|
| Unit cost | — | £7,500 (1984)[source] |
|---|
| Produced | — | 1971[source] |
|---|
| No. built | — | 350,000 missiles, 10,000 launchers[source] |
|---|
| Reported operators |
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|---|
200–2,000 m (660–6,560 ft); 3,000 m (MILAN ER)[source]