Credit
Varga Attila · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Kh-25larger figure on 1 of 1
Zuni (rocket)larger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Kh-25ML
Single sourceKh-25MP 1VP
Single sourceConfiguration
| Specification | Kh-25 | Zuni (rocket) |
|---|---|---|
| Type | tactical air-to-surface missile[source] | Air-to-surface rocket[source] |
| Place of origin | Soviet Union[source] | United States[source] |
| In service | 1975–present[source] | — |
| Designed | 1971–75[source] | — |
| Manufacturer | Zvezda-Strela[source] |
Kh-25MP 2VP
Single sourceKh-25ML :370.5 cm (12 ft 2 in) Kh-25MP 1VP :425.5 cm (167.5 in) Kh-25MP 2VP :435.5 cm (171.5 in)[source]
Length
Single source77 inches (2,000 mm)[source]
Kh-25MP
Single sourceKh-25MR
Single sourceKh-25MP :89.6 kg (198 lb), Kh-25MR :140 kg (309 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Produced | 1975–present[source] | 1957–present[source] |
|---|
| Warhead | High explosive, shell-forming[source] | various[source] |
|---|
| Guidance system | Laser guidance , passive radiation , TV guidance , IIR , Satellite guidance , active radar homing depending on variant[source] | None[source] |
|---|
| Launch platform | MiG-21, MiG-23/27, MiG-29, Ka-52, Su-17/20/22, Su-24, Su-25, Su-27, Yakovlev Yak-130 Kh-25MP : MiG-23/27, Su-17/22, Su-24, Su-25 Ka-50[source] | — |
|---|
| Used by | — | United States military French Air Force Ukrainian Air Force[source] |
|---|
| Engine | — | Solid-fuel rocket[source] |
|---|
| Reported operators |
| — |
|---|