Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Configuration
| Specification | 9K114 Shturm | MAX 1.2 AC |
|---|---|---|
| Speed | — | 274 m/s[source] |
| Type | ATGM[source] | ATGM[source] |
| Place of origin | Soviet Union[source] | Brazil[source] |
| Used by | Soviet Union Russia Ukraine[source] | Brazilian Armed Forces[source] |
| Wars | Soviet–Afghan War Russo-Ukrainian war |
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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Developed into | 9M120 Ataka[source] | — |
|---|
| Former operator · Brazil | Brazil[source] | — |
|---|
| Former operator · Croatia | Croatia[source] | — |
|---|
| Former operator · Moldova | Moldova[source] | — |
|---|
| Former operator · Poland | Poland[source] | — |
|---|
| Former operator · Soviet Union | Soviet Union[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 |
| — |
|---|