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At a glance
Measured figures
Length · source measurement 1
Single sourceLength · source measurement 2
Single sourceConfiguration
| Specification | PL-2 | Zuni (rocket) |
|---|---|---|
| Type | Short-range air-to-air missile[source] | Air-to-surface rocket[source] |
| Place of origin | China[source] | United States[source] |
| In service | 1970s to present[source] | — |
| Used by | China[source] | United States military French Air Force Ukrainian Air Force[source] |
| Manufacturer |
Length · source measurement 3
Single source2.15–2.99 m (7 ft 1 in – 9 ft 10 in)[source]
Length
Single source77 inches (2,000 mm)[source]
Wingspan · source measurement 1
Single sourceWingspan · source measurement 2
Single sourceWingspan · source measurement 3
Single source528–609 mm (1 ft 9 in – 2 ft 0 in)[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)[source] |
| — |
| Produced | 1970s to 1980s[source] | 1957–present[source] |
|---|
| Warhead | 11.3 kg (25 lb) high explosive[source] | various[source] |
|---|
| Detonation mechanism | Impact / Proximity[source] | — |
|---|
| Engine | rocket 2668dN[source] | Solid-fuel rocket[source] |
|---|
| Propellant | solid fuel[source] | — |
|---|
| Flight ceiling | 15–21.5 km (9–13 mi)[source] | — |
|---|
| Guidance system | Nitrogen cooled passive InPb infrared seeker[source] | None[source] |
|---|
| Launch platform | aerial[source] | — |
|---|