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Measured figures
PL-5B, PL-5C
Single sourcePL-5E
Single source3.128 m (PL-5B, PL-5C), 2.893m (PL-5E)[source]
PL-5B, PL-5C
Single sourcePL-5E
Single source0.657m (PL-5B, PL-5C), 0.617m (PL-5E)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | AIM-260 JATM | PL-5 |
|---|---|---|
| Speed | Mach 5[source] | Mach 2.5[source] |
| Type | Beyond-visual-range air-to-air missile[source] | Short-range air-to-air missile[source] |
| Place of origin | United States[source] | China[source] |
| Designer | Lockheed Martin[source] | — |
| Produced | 2024–present[source] | 1982[source] |
| Warhead | High explosive blast-fragmentation[source] | 6kg blast-frag , or expanding rod (RF-fuse)[source] |
| Launch platform | Aircraft: Lockheed Martin F-22 Raptor Boeing F/A-18E/F Super Hornet Lockheed Martin F-35 Lightning II Boeing F-15EX Eagle II[source] | Aircraft, helicopter gunships[source] |
| Manufacturer | Lockheed Martin[source] | Luoyang Electro-Optics Technology Development Centre (EOTDC), Hanzhong Nanfeng Machine Factory[source] |
| Detonation mechanism | — | Active infrared , laser proximity fuse(PL-5EII)[source] |
| Engine | — | Solid-fuel rocket[source] |
| Guidance system | — | Infrared homing , multi-element, dual band detector(PL-5EII)[source] |
| Reported operators | — |
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