Loading the evidence…
Preparing your view.
Preparing your view.


At a glance
Measured figures
Length
Single sourcewithout gas generator
Single sourceConfiguration
| Specification | 9M113 Konkurs | M90 Stršljen |
|---|---|---|
| Type | Anti-tank missile[source] | Anti-tank rocket launcher[source] |
| Place of origin | Soviet Union[source] | Serbia / North Macedonia[source] |
| In service | 1974–present[source] | 2002–present[source] |
| Used by | See operators[source] | Serbia North Macedonia Iraq Syria Hamas |
1,150 mm (45 in) 875 mm (34.4 in) without gas generator[source]
launcher, in firing position
Single sourcelauncher loaded, sealed
Single source1,350 mm (launcher loaded, sealed) 1,300 mm (launcher, in firing position)[source]
9P135 launching post
Single sourceMissile weight
Single source14.6 kg (32 lb) (Missile weight) 22.5 kg (50 lbs) (9P135 launching post)[source]
launcher
Single sourceLoaded
Single sourceMaximum; 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; Effective firing range
Single sourceMaximum; Maximum firing range
Single sourceMuzzle velocity
Single source205 m/s[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] | Syrian Civil War War in Iraq (2013-17)[source] |
|---|
| Designed | 1970[source] | — |
|---|
| Manufacturer | Tula Machinery Design Bureau (Tula KBP) – Tulsky Oruzheiny Zavod Bharat Dynamics Limited[source] | Sloboda[source] |
|---|
| Variants | 9M113M[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] | — |
|---|
| Former operator · Chechen Republic of Ichkeria | Chechen Republic of Ichkeria[source] | — |
|---|
| Former operator · East Germany | East Germany[source] | — |
|---|
| Former operator · Czechoslovakia | Czechoslovakia[source] | — |
|---|
| Former operator · Finland | Finland[source] | — |
|---|
| Former operator · Soviet Union | Soviet Union[source] | — |
|---|
| Source measurement | The original 9M113 with a single-charge warhead can penetrate 600 mm of rolled homogeneous armor (RHA).[source]9M113 Konkurs · Development; only the objects and conditions stated in this passage The system uses a gas generator to push the missile out of the launch tube. The gas also exits from the rear of the launch tube in a similar manner to a recoilless rifle . The missile leaves the launch tube at 80 meters per second, and is quickly accelerated to 200 meters per second by its solid fuel motor. This initial high speed reduces the missile's deadzone, since it can be launched directly at the target, rather than in an upward arc. In flight, the missile spins at between five and seven revolutions per second.[source]9M113 Konkurs · Design; only the objects and conditions stated in this passage 9M113M Konkurs-M (NATO: AT-5B Spandrel B ) Tandem warhead – with extended explosive probe. The warhead penetration is 750–800 mm vs RHA. Adopted in 1991. Missile 9M113M 1990. Tandem (800 mm (behind a layer of ERA)). 4,000 m (3500 m night (passive)).[source]9M113 Konkurs · Models; only the objects and conditions stated in this passage | — |
|---|
| Country of origin | Soviet Union[source]Inventory Origin column; table 1, row 77, cell 4; revision 1377727163; retrieved 2026-10-02 | — |
|---|
| Designer | — | Military Technical Institute[source] |
|---|
| Produced | — | 2002–present[source] |
|---|
| No. built | — | 1,010+[source] |
|---|
| Action | — | 800 mm RHA[source] |
|---|
| Sights | — | Iron sights[source] |
|---|
| Reported operators |
|
|
|---|
rocket
13.00 kg (loaded) 5.70 kg (launcher) 7.30 kg (rocket)[source]