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At a glance
Kh-28larger figure on 3 of 3
Zuni (rocket)larger figure on 0 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
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.
Configuration
| Specification | Kh-28 | Zuni (rocket) |
|---|---|---|
| Type | air-launched anti-radiation missile[source] | Air-to-surface rocket[source] |
| Place of origin | Soviet Union[source] | United States[source] |
| In service | 1973–current[source] | — |
| Used by | FSU, Warsaw Pact, India, Iraq, Vietnam[source] | United States military French Air Force Ukrainian Air Force[source] |
| Designer | Alexander Yakovlevich Bereznyak[source] | — |
| Manufacturer | MKB Raduga[source] | — |
| Warhead | Blast fragmentation[source] | various[source] |
| Engine | Two-stage liquid-fuel rocket[source] | Solid-fuel rocket[source] |
| Guidance system | Inertial guidance with passive radar seeker[source] | None[source] |
| Launch platform | Su-17M/Su-20/Su-22M, Su-24M, Tu-16, MiG-25BM, MiG-27, Tu-22M[source] | — |
| Former operator · Soviet Union | Soviet Union[source] | — |
| Former operator · Afghanistan | Afghanistan[source] | — |
| Former operator · Hungary | Hungary[source] | — |
| Former operator · Iraq | Iraq[source] | — |
| Former operator · Peru | Peru[source] | — |
| Former operator · Poland | Poland[source] | — |
| Former operator · South Yemen | South Yemen[source] | — |
| Produced | — | 1957–present[source] |
| Reported operators |
| — |