HQ-10
| HQ-10 | |
|---|---|
HHQ-10 8-round launcher on a Type 056 corvette | |
| Type | Surface-to-air missile |
| Place of origin | China |
| Service history | |
| In service | 2013 |
| Used by | China |
| Production history | |
| Manufacturer | Shanghai Academy of Spaceflight Technology (SAST) |
| Specifications | |
| Mass | 20 kg |
| Length | 2 m |
| Diameter | 127 mm |
| Warhead | 3 kg HE FRAG |
Detonation mechanism | infrared proximity fuse |
| Engine | rocket motor |
| Propellant | solid fuel |
Operational range | 0.5 km to 9 km |
| Flight altitude | 1.5 m to 6 km |
Guidance system | Imaging infrared (IIR) |
The HQ-10 (simplified Chinese: 红旗-10; traditional Chinese: 紅旗-10; pinyin: Hóng Qí-10; lit. 'Red Banner-10') is a short range surface-to-air missile designed by China Aerospace Science and Technology Corporation (CASC), currently in service as a point defense missile system aboard PLA Navy warships.