FORCETALLY
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At a glance
Measured figures
Length
Single source102 cm (40 in)[source]
Launch pad
Single sourceConfiguration
| Specification | AT4 | TAipers |
|---|---|---|
| Type | Disposable anti-tank launcher[source] | Anti-tank guided missile[source] |
| Place of origin | Sweden United States[source] | South Korea[source] |
| In service | 1987–present[source] | 2024–present[source] |
| Used by | See Operators[source] | Republic of Korea Army Republic of Korea Marine Corps[source] |
Missile
Single sourceMissile: 1,735 millimeters (5 ft 8.3 in) Launch pad: 1,855 millimeters (6 ft 1.0 in)[source]
Diameter
Single source150 millimeters (5.9 in)[source]
Launch pad
Single sourceMissile
Single sourceMissile: 35 kilograms (77 lb) Launch pad: 9 kilograms (20 lb)
Maximum; Mach 0.59
Single sourceMaximum; Maximum speed · source measurement 1
Single sourceMaximum; Maximum speed · source measurement 2
Single source200 m/s (720 km/h; 450 mph; Mach 0.59)[source]
CS
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.
| Wars | See Wars[source] | — |
|---|
| Designer | Förenade Fabriksverken[source] | Agency for Defense Development[source] |
|---|
| Manufacturer | Saab Bofors Dynamics (Swedish version) Alliant Techsystems (U.S. version)[source] | Hanwha Aerospace[source] |
|---|
| Unit cost | US$1,480 (In 1999) US$2,857 (2025)[source] | — |
|---|
| No. built | 600,000+[source] | — |
|---|
| Variants | See Variants[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 | — | 2015–2022[source] |
|---|
| Produced | — | 2024–present[source] |
|---|
| Warhead | — | Tandem-charge HEAT[source] |
|---|
| Blast yield | — | 1,000 mm (39 in) RHA[source] |
|---|
| Propellant | — | Smokeless solid-propellant[source] |
|---|
| Guidance system | — | Fire-and-forget dual-mode seeker with fiber-optic datalink MITL[source] |
|---|
| Launch platform | — | LAH-1 Miron MAH Marineon[source] |
|---|
| Reported operators |
| — |
|---|
