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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 | Panzerfaust 3 |
|---|---|---|
| Type | Anti-tank missile[source] | Disposable anti-tank rocket - propelled grenade launcher[source] |
| Place of origin | Soviet Union[source] | West Germany[source] |
| In service | 1974–present[source] | 1987–present[source] |
| Used by | See operators[source] | See Operators |
Panzerfaust 3larger 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 source950 mm (3 ft 1 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]
Bunker-buster warhead
Single sourceConfiguration: Hollow charge warhead
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]
Maximum; automatic self-destructs once beyond the range
Single sourceMaximum; Panzerfaust 3 · maximal · Kampfentfernung
Single sourcebarrel
Single sourcePanzerfaust 3 · Calibre · Gefechtskopf (warhead)
Single sourcePanzerfaust 3 · Calibre · Rohr (launcher tube)
Single sourcewarhead
Single source60 mm (2.4 in) barrel, 110 mm (4.3 in) warhead[source]
60 mm[source]Panzerfaust 3 · Rohr (launcher tube)
110 mm[source]Panzerfaust 3 · Gefechtskopf (warhead)
Muzzle velocity
Single source115.0 m/s (377 ft/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] | War in Afghanistan (2001–2021) Syrian Civil War War in Iraq (2013–2017) Russo-Ukrainian War[source] |
|---|
| Designed | 1970[source] | 1978–1985[source] |
|---|
| Manufacturer | Tula Machinery Design Bureau (Tula KBP) – Tulsky Oruzheiny Zavod Bharat Dynamics Limited[source] | Dynamit Nobel AG IHI Aerospace (Licensed)[source] |
|---|
| Variants | 9M113M[source] | Panzerfaust 3-T, Panzerfaust 3-IT600, Panzerfaust 3LW, Panzerfaust 3LW-HESH, Bunkerfaust, 110 mm (4.3 in) anti-tank weapon[source] |
|---|
| Warhead | 2.7 kg (6.0 lb) 9N131 HEAT[source] | 110 mm (4.3 in)[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 | — | Dynamit Nobel AG[source] |
|---|
| Sights | — | Hensoldt Wetzlar ZF 2.5 X 10 Telescopic sight[source] |
|---|
| Penetration | — | 700 mm Panzerstahl[source]Panzerfaust 3 · Durchschlagsleistung Panzerfaust |
|---|
| Reported operators |
| — |
|---|
Panzerfaust 3 · circa · Gewicht (je nach Munition) · Approximate (circa/ca.)
Single sourceReady to fire
Single sourceTandem hollow charge warhead
Single sourceUnloaded firing unit
Single sourceConfiguration: Hollow charge warhead : 12.9 kg (28 lb 7 oz ) Tandem hollow charge warhead : 13.3 kg (29 lb 5 oz) Bunker-buster warhead: 13.3 kg (29 lb 5 oz) Unloaded firing unit: 2.3 kg (5 lb 1 oz) Ready to fire: 15.2 - 15.6 kg (34 lb 6 oz)[source]
circa 13 kg[source]Panzerfaust 3 · Gewicht (je nach Munition) · Approximate (circa/ca.)