Credit
Srđan Popović · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Length
Single source2,720 mm[source]
PL-5B, PL-5C
Single sourceConfiguration
| Specification | ALAS (missile) | PL-5 |
|---|---|---|
| Speed | 130–150m/s[source] 130–150 m/s (mid-course)[source] | Mach 2.5[source] |
| Type | Multi-purpose surface-to surface missile[source] | Short-range air-to-air missile[source] |
| Place of origin | Serbia[source] | China[source] |
| Manufacturer | EDePro , Yugoimport SDPR |
PL-5E
Single source3.128 m (PL-5B, PL-5C), 2.893m (PL-5E)[source]
Operational; (PL-5B, PL-5C), 0.5-16~
Single sourceOperational; PL-5E
Single source1.3–16km (PL-5B, PL-5C), 0.5-16~18km (PL-5E)[source]
Warhead weight
Single source10.5 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Luoyang Electro-Optics Technology Development Centre (EOTDC), Hanzhong Nanfeng Machine Factory[source] |
| Engine | solid fuel boost phase motor, EDePro TMM-404 single-shaft turbojet[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | optical IR or TV[source] | Infrared homing , multi-element, dual band detector(PL-5EII)[source] |
|---|
| Accuracy | less than 1 meter CEP[source] | — |
|---|
| Produced | — | 1982[source] |
|---|
| Warhead | — | 6kg blast-frag , or expanding rod (RF-fuse)[source] |
|---|
| Detonation mechanism | — | Active infrared , laser proximity fuse(PL-5EII)[source] |
|---|
| Launch platform | — | Aircraft, helicopter gunships[source] |
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| Reported operators |
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