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At a glance
Measured figures
Length
Single source1.2 m (3 ft 11 in)[source]
UMTAS-GM-2
Single sourceConfiguration
| Specification | MILAN | UMTAS |
|---|---|---|
| Type | Anti-tank missile[source] | Air-to-surface , anti-tank guided missile[source] |
| Place of origin | France, West Germany[source] | Turkey[source] |
| In service | 1972–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 |
UMTAS/LUMTAS
Single sourceUMTAS/LUMTAS-GM-1
Single sourceUMTAS/LUMTAS -1.8 m (5 ft 11 in) UMTAS/LUMTAS-GM-1 -1.72 m (5 ft 8 in) UMTAS-GM-2 -2 m (6 ft 7 in)[source]
Mass
Single source16.4 kg[source]
UMTAS-GM-2 launcher
Single sourceUMTAS-GM-2 missile
Single sourceUMTAS/LUMTAS-GM-1 launcher
Single sourceUMTAS/LUMTAS-GM-1 missile
Single sourceUMTAS/LUMTAS launcher
Single sourceUMTAS/LUMTAS missile
Single sourceUMTAS/LUMTAS -37.5 kg (83 lb) missile 62 kg (137 lb) launcher UMTAS/LUMTAS-GM-1 -41.3 kg (91 lb) missile 25 kg (55 lb) launcher UMTAS-GM-2 -60 kg (130 lb) missile 40 kg (88 lb) launcher[source]
Maximum; Maximum speed
Single source200 m/s (660 ft/s)[source]
Operational; MILAN ER
Single sourceOperational; Operational range
Single source200–2,000 m (660–6,560 ft); 3,000 m (MILAN ER)[source]
Operational; UMTAS-GM-2 from aircraft
Single sourceOperational; UMTAS-GM-2 from vehicles
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designed | 1970s[source] | 2005-2017[source] |
|---|
| Manufacturer | MBDA Also produced under license by: Bharat Dynamics (India) BAe Dynamics (United Kingdom)[source] | Roketsan[source] |
|---|
| Unit cost | £7,500 (1984)[source] | — |
|---|
| Produced | 1971[source] | 2017-current[source] |
|---|
| No. built | 350,000 missiles, 10,000 launchers[source] | — |
|---|
| Variants | See variants[source] | UMTAS L-UMTAS[source] |
|---|
| Warhead | Single or tandem HEAT[source] | Tandem HEAT / blast-fragmentation / thermobaric[source] |
|---|
| Detonation mechanism | contact[source] | Impact Proximity[source] |
|---|
| Engine | solid-fuel rocket[source] | HTPB ‐based solid-fuel rocket motor[source] |
|---|
| Guidance system | SACLOS wire[source] | RF data link Imaging infrared (UMTAS) Semi-active laser (L-UMTAS)[source] |
|---|
| Steering system | Jet deflector[source] | — |
|---|
| Launch platform | Individual, vehicle[source] | AH-1W SuperCobra T129 ATAK SH-60B Seahawk TAI Hürkuş TAI Hürjet IOMAX Archangel Mil Mi-8[source] |
|---|
| References | — | Janes[source] |
|---|
| Reported operators |
| — |
|---|
Operational; UMTAS/LUMTAS
Single sourceOperational; UMTAS/LUMTAS-GM-1 from aircraft
Single sourceOperational; UMTAS/LUMTAS-GM-1 from vehicles
Single sourceUMTAS/LUMTAS -500–8,000 m (0.31–4.97 mi) UMTAS/LUMTAS-GM-1 -1,000–16,000 m (0.62–9.94 mi) from vehicles, 1,000–32,000 m (0.62–19.88 mi) from aircraft UMTAS-GM-2 -1,000–32,000 m (0.62–19.88 mi) from vehicles 1,000–50,000 m (0.62–31.07 mi) from aircraft[source]