FORCETALLY
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At a glance
Measured figures
Length
Single source102 cm (40 in)[source]
UMTAS-GM-2
Single sourceConfiguration
| Specification | AT4 | UMTAS |
|---|---|---|
| Type | Disposable anti-tank launcher[source] | Air-to-surface , anti-tank guided missile[source] |
| Place of origin | Sweden United States[source] | Turkey[source] |
| In service | 1987–present[source] | — |
| Used by | See Operators[source] | — |
| Wars | See Wars[source] | — |
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]
UMTAS-GM-2
Single sourceUMTAS/LUMTAS
Single sourceUMTAS/LUMTAS-GM-1
Single sourceUMTAS/LUMTAS -160 mm (6.3 in) UMTAS/LUMTAS-GM-1 -160 mm (6.3 in) UMTAS-GM-2 -180 mm (7.1 in)[source]
UMTAS-GM-2 launcher
Single sourceUMTAS-GM-2 missile
Single sourceCS
Single sourceMuzzle velocity
Single source290 m/s (950 ft/s; 1,000 km/h), 220 m/s (720 ft/s; 790 km/h) (CS)[source]
high-explosive anti-tank (HEAT) round
Single source440 g high-explosive anti-tank (HEAT) round[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Förenade Fabriksverken[source] | — |
|---|
| Manufacturer | Saab Bofors Dynamics (Swedish version) Alliant Techsystems (U.S. version)[source] | Roketsan[source] |
|---|
| Unit cost | US$1,480 (In 1999) US$2,857 (2025)[source] | — |
|---|
| No. built | 600,000+[source] | — |
|---|
| Variants | See Variants[source] | UMTAS L-UMTAS[source] |
|---|
| Sights | Iron sights , optional AN/PVS-4 night vision unit[source] | — |
|---|
| Filling | Octol[source] | — |
|---|
| Role | man-portable, disposable, shoulder-fired recoilless anti-tank weapon[source] | — |
|---|
| Designed | — | 2005-2017[source] |
|---|
| Produced | — | 2017-current[source] |
|---|
| Warhead | — | Tandem HEAT / blast-fragmentation / thermobaric[source] |
|---|
| Detonation mechanism | — | Impact Proximity[source] |
|---|
| Engine | — | HTPB ‐based solid-fuel rocket motor[source] |
|---|
| Guidance system | — | RF data link Imaging infrared (UMTAS) Semi-active laser (L-UMTAS)[source] |
|---|
| Launch platform | — | AH-1W SuperCobra T129 ATAK SH-60B Seahawk TAI Hürkuş TAI Hürjet IOMAX Archangel Mil Mi-8[source] |
|---|
| References | — | Janes[source] |
|---|
| Reported operators |
| — |
|---|
UMTAS/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]
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]