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At a glance
PL-10larger figure on 2 of 2
Zuni (rocket)
Measured figures
Length
Single source3.0 m (9 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | PL-10 | Zuni (rocket) |
|---|---|---|
| Type | Short-range air-to-air missile[source] | Air-to-surface rocket[source] |
| Place of origin | People's Republic of China[source] | United States[source] |
| In service | 2015–present[source] | — |
| Used by | People's Liberation Army Air Force Pakistan Air Force[source] | United States military French Air Force Ukrainian Air Force[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
77 inches (2,000 mm)[source]
motor only
Single source79.5 pounds (36.1 kg) (motor only)[source]
Maximum; Maximum speed
Single source1,615 miles per hour (2,599 km/h)[source]
Operational; Operational range
Single source5 miles (8.0 km)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer |
|---|
Luoyang Electro-Optics Technology Development Centre (EOTDC)[source] |
| — |
| Produced | 2013–present[source] | 1957–present[source] |
|---|
| Warhead | Blast-frag , or expanding rod (RF-fuse)[source] | various[source] |
|---|
| Detonation mechanism | Laser proximity fuze and impact[source] | — |
|---|
| Engine | Thrust-vectoring solid-propellant rocket[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | Multi-element imaging infrared (IIR) Active radar seeker[source] | None[source] |
|---|
| Launch platform | Aircraft[source] | — |
|---|