FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
LAHATlarger figure on 0 of 3
MILAN
Measured figures
Length
Single source975 mm (38.4 in )[source]
Length
Single sourceConfiguration
| Specification | LAHAT | MILAN |
|---|---|---|
| Type | ATGM[source] | Anti-tank missile[source] |
| Place of origin | Israel[source] | France, West Germany[source] |
| In service | 1991–present[source] | 1972–present[source] |
| Manufacturer | Israel Aerospace Industries[source] | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] |
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]
Operational; air launched
Single sourceOperational; ground launched
Single source6,000–8,000 m (6,600–8,700 yd ) ground launched 8,000–13,000 m (8,700–14,200 yd) air launched[source]
Operational; MILAN ER
Single sourceOperational; Operational range
Single sourceWarhead weight
Single source4.5 kg (9.9 lb )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Unit cost | $25,000 (1999)[source] | £7,500 (1984)[source] |
|---|
| Warhead | Tandem HEAT[source] | Single or tandem HEAT[source] |
|---|
| Guidance system | Semi-active laser homing[source] | SACLOS wire[source] |
|---|
| Launch platform | 105–120 mm smoothbore rotary-wing aircraft[source] | Individual, vehicle[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[source] |
|---|
| Designed | — | 1970s[source] |
|---|
| Produced | — | 1971[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 | — |
|
|---|
200–2,000 m (660–6,560 ft); 3,000 m (MILAN ER)[source]