AAnti-tank weapons
Loading the evidence…
Preparing your view.
Preparing your view.
AAnti-tank weapons
Measured figures
Configuration
| Specification | 3M6 Shmel | MAX 1.2 AC |
|---|---|---|
| Speed | — | 274 m/s[source] |
| Former operator · Afghanistan | Afghanistan[source] | — |
| Former operator · Algeria | Algeria[source] | — |
| Former operator · Bulgaria | Bulgaria[source] | — |
| Former operator · Cyprus | Cyprus[source] | — |
| Former operator · Czechoslovakia | Czechoslovakia |
15 or missile
Single sourcefiring unit
Single sourcemissile + launch tube
Single sourcetotal
Single source15 or 15.2 kg (missile) 24 kg (missile + launch tube) 28 kg (firing unit) 52 kg (total)[source]
Operational; At least see #Range
Single sourceAt least 2,000 m, see #Range[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Former operator · East Germany | East Germany[source] | — |
|---|
| Former operator · Egypt | Egypt[source] | — |
|---|
| Former operator · Hungary | Hungary[source] | — |
|---|
| Former operator · Iraq | Iraq[source] | — |
|---|
| Former operator · Israel | Israel[source] | — |
|---|
| Former operator · Mongolia | Mongolia[source] | — |
|---|
| Former operator · Poland | Poland[source] | — |
|---|
| Former operator · Romania | Romania[source] | — |
|---|
| Former operator · Soviet Union | Soviet Union[source] | — |
|---|
| Former operator · Syria | Syria[source] | — |
|---|
| Former operator · Yugoslavia | Yugoslavia[source] | — |
|---|
| Country of origin | USSR[source]Inventory Origin column; table 3, row 3, cell 3; revision 1367546664; retrieved 2026-09-30 | — |
|---|
| Type | — | ATGM[source] |
|---|
| Place of origin | — | Brazil[source] |
|---|
| Used by | — | Brazilian Armed Forces[source] |
|---|
| Designed | — | 1980s[source] |
|---|
| Manufacturer | — | SIATT[source] |
|---|
| Warhead | — | HMX in a non-tandem shaped charge HEAT warhead (at least 500 mm RHAe penetration, see #Penetration )[source] |
|---|
| Engine | — | Two-stage engine[source] |
|---|
| Propellant | — | Two-stage solid propellant[source] |
|---|
| Guidance system | — | Laser-guided semi-automatic command to line of sight[source] |
|---|
| Launch platform | — | Two-person infantry crew or vehicle-mounted[source] |
|---|
| Reported operators |
| — |
|---|