FORCETALLY
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At a glance
Measured figures
Warhead weight
Single source5.4 kg (12 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | 9M17 Fleyta | MAX 1.2 AC |
|---|---|---|
| Type | Anti-tank missile[source] | ATGM[source] |
| Place of origin | Soviet Union[source] | Brazil[source] |
| In service | 1964-present[source] | — |
| Designer | Nudelman OKB-16[source] | — |
| Warhead | HEAT[source] | HMX in a non-tandem shaped charge HEAT warhead (at least 500 mm RHAe penetration, see #Penetration )[source] |
| Engine | Solid fuel rocket[source] | Two-stage engine[source] |
| Guidance system | Radio command[source] | Laser-guided semi-automatic command to line of sight[source] |
| Steering system | MCLOS[source] | — |
| Launch platform | Mi-4 , Mi-8 , Mi-24 , Mi-25 , BRDM-1 , BRDM-2[source] | Two-person infantry crew or vehicle-mounted[source] |
| Former operator · Afghanistan | Afghanistan[source] | — |
| Former operator · Bulgaria | Bulgaria[source] | — |
| Former operator · Czechoslovakia | Czechoslovakia[source] | — |
| Former operator · Czech Republic | Czech Republic[source] | — |
| Former operator · East Germany | East Germany[source] | — |
| Former operator · Egypt | Egypt[source] | — |
| Former operator · Iraq | Iraq[source] | — |
| Former operator · Libyan Arab Jamahiriya | Libyan Arab Jamahiriya[source] | — |
| Former operator · Peru | Peru[source] | — |
| Former operator · Poland | Poland[source] | — |
| Former operator · Russia | Russia[source] | — |
| Former operator · Romania | Romania[source] | — |
| Former operator · Slovakia | Slovakia[source] | — |
| Former operator · Soviet Union | Soviet Union[source] | — |
| Former operator · South Yemen | South Yemen[source] | — |
| Former operator · Syria | Syria[source] | — |
| Former operator · Yemen | Yemen[source] | — |
| Used by | — | Brazilian Armed Forces[source] |
| Designed | — | 1980s[source] |
| Manufacturer | — | SIATT[source] |
| Propellant | — | Two-stage solid propellant[source] |
| Reported operators |
| — |