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At a glance
Measured figures
Length
Single source597 cm (19 ft 7 in)[source]
PL-5B, PL-5C
Single sourceConfiguration
| Specification | Kh-28 | PL-5 |
|---|---|---|
| Speed | Mach 3.0[source] | Mach 2.5[source] |
| Type | air-launched anti-radiation missile[source] | Short-range air-to-air missile[source] |
| Place of origin | Soviet Union[source] | China[source] |
| In service | 1973–current[source] |
PL-5E
Single source3.128 m (PL-5B, PL-5C), 2.893m (PL-5E)[source]
Warhead weight
Single source160 kg (353 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by | FSU, Warsaw Pact, India, Iraq, Vietnam[source] | — |
|---|
| Designer | Alexander Yakovlevich Bereznyak[source] | — |
|---|
| Manufacturer | MKB Raduga[source] | Luoyang Electro-Optics Technology Development Centre (EOTDC), Hanzhong Nanfeng Machine Factory[source] |
|---|
| Warhead | Blast fragmentation[source] | 6kg blast-frag , or expanding rod (RF-fuse)[source] |
|---|
| Engine | Two-stage liquid-fuel rocket[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | Inertial guidance with passive radar seeker[source] | Infrared homing , multi-element, dual band detector(PL-5EII)[source] |
|---|
| Launch platform | Su-17M/Su-20/Su-22M, Su-24M, Tu-16, MiG-25BM, MiG-27, Tu-22M[source] | Aircraft, helicopter gunships[source] |
|---|
| Former operator · Soviet Union | Soviet Union[source] | — |
|---|
| Former operator · Afghanistan | Afghanistan[source] | — |
|---|
| Former operator · Hungary | Hungary[source] | — |
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| Former operator · Iraq | Iraq[source] | — |
|---|
| Former operator · Peru | Peru[source] | — |
|---|
| Former operator · Poland | Poland[source] | — |
|---|
| Former operator · South Yemen | South Yemen[source] | — |
|---|
| Produced | — | 1982[source] |
|---|
| Detonation mechanism | — | Active infrared , laser proximity fuse(PL-5EII)[source] |
|---|
| Reported operators |
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