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At a glance
Measured figures
launcher loaded
Single sourcerocket
Single sourceConfiguration
| Specification | M79 Osa | MPATGM |
|---|---|---|
| Type | Anti-tank rocket launcher[source] | Anti-tank guided missile[source] |
| Place of origin | Yugoslavia[source] | India[source] |
| Used by | See Operators[source] | — |
| Wars | Yugoslav Wars Syrian Civil War Yemeni Civil War[source] | — |
| Designer | Military Technical Institute[source] |
1.91 m (launcher loaded) 0.67 m (rocket)[source]
Length
Single source1,300 mm (4 ft 3 in)[source]
launcher
Single sourceLoaded
Single sourcerocket
Single source11.2 kg (loaded) 6.2 kg (launcher) 3.5 kg (rocket)[source]
Mass
Single sourceMissile Command Launch Unit (CLU)
Single sourceRate of fire
Single source6 rounds per minute[source]
Muzzle velocity
Single source250 m/s[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Defence Research and Development Organisation[source] |
| Designed | 1979[source] | 2015[source] |
|---|
| Manufacturer | Sloboda[source] | Bharat Dynamics Limited Bharat Electronics Limited[source] |
|---|
| Sights | CN-6 (3.5× optical sight) or flip up iron sights[source] | Digital sight with laser designator[source] |
|---|
| Blast yield | 400 mm RHA[source] | Penetration: 660 mm of RHA + ERA 710 mm of RHA[source] |
|---|
| Role | portable 90 mm anti-tank weapon[source] | — |
|---|
| Warhead | — | Tandem-charge HEAT[source] |
|---|
| Engine | — | Dual-thrust rocket with blast tube ejection motor[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Guidance system | — | Dual mode mid-wave IIR direct drive with real-time target identification + Edge AI image processing[source] |
|---|
| Launch platform | — | Launch tube, tripod-mount[source] |
|---|
| Reported operators |
| — |
|---|
Missile: 14.50 kg (32.0 lb) Command Launch Unit (CLU): 14.25 kg (31.4 lb)[source]