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At a glance
9M113 Konkurslarger figure on 1 of 1
Measured figures
Length
Single sourcewithout gas generator
Single sourceConfiguration
| Specification | 9M113 Konkurs | AT4 |
|---|---|---|
| Type | Anti-tank missile[source] | Disposable anti-tank launcher[source] |
| Place of origin | Soviet Union[source] | Sweden United States[source] |
| In service | 1974–present[source] | 1987–present[source] |
| Used by | See operators[source] | See Operators[source] |
AT4larger figure on 0 of 1
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 source102 cm (40 in)[source]
9P135 launching post
Single sourceMissile weight
Single source14.6 kg (32 lb) (Missile weight) 22.5 kg (50 lbs) (9P135 launching post)[source]
AT4
Single sourceAT4-CS
Single source6.7 kg (14.8 lb ) (AT4) 8 kg (18 lb) (AT4-CS)
Maximum; Maximum speed
Single source208 m/s (680 ft/s)[source]
Operational; Operational range
Single sourceOperational; to
Single source70 m (230 ft) to 4 km (2.5 mi)[source]
Effective; point target
Single sourceMaximum
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.
| 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] | See Wars[source] |
|---|
| Designed | 1970[source] | — |
|---|
| Manufacturer | Tula Machinery Design Bureau (Tula KBP) – Tulsky Oruzheiny Zavod Bharat Dynamics Limited[source] | Saab Bofors Dynamics (Swedish version) Alliant Techsystems (U.S. version)[source] |
|---|
| Variants | 9M113M[source] | See Variants[source] |
|---|
| Warhead | 2.7 kg (6.0 lb) 9N131 HEAT[source] | — |
|---|
| Detonation mechanism | Contact[source] | — |
|---|
| Engine | Solid-fuel rocket[source] | — |
|---|
| Guidance system | Wire-guided SACLOS[source] | — |
|---|
| Steering system | Two control surfaces[source] | — |
|---|
| Launch platform | Individual, vehicle[source] | — |
|---|
| Designer | — | Förenade Fabriksverken[source] |
|---|
| Unit cost | — | US$1,480 (In 1999) US$2,857 (2025)[source] |
|---|
| No. built | — | 600,000+[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] |
|---|
| Reported operators |
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|---|
Maximum; area target