PL-5
From Wikipedia, the free encyclopedia
PL-5 | |
---|---|
Type | Short-range air-to-air missile |
Production history | |
Manufacturer | Luoyang Electro-Optics Technology Development Centre (EOTDC), Hanzhong Nanfeng Machine Factory |
Specifications | |
Weight | 148kg (PL-5B, PL-5C), 83kg (PL-5E) |
Length | 3.128m (PL-5B, PL-5C), 2.893m (PL-5E) |
|
|
Warhead | 6kg blast-frag, or expanding rod (RF-fuse) |
Detonation mechanism |
Active infrared |
|
|
Engine | Solid-fuel rocket |
Wingspan | 0.657m (PL-5B, PL-5C), 0.617m (PL-5E) |
Operational range |
1.3-16km (PL-5B, PL-5C), 0.5-16~18km (PL-5E) |
Speed | Mach 2.2 |
Guidance system |
Infrared homing |
Launch platform |
Aircraft, helicopter gunships |
The PL-5 (霹雳-5) air-to-air missile (PL stands for Pi Li, "Thunderbolt" in Chinese, the generic designation for all PRC air-to-air missiles) is a short-range, infra-red guided missile use by Chinese fighters. It is based on AA-2 Atoll technology and resembles the AIM-9 Sidewinder. The PL-5 was designed and developed at China's Luoyang Electro-Optics Technology Development Centre (EOTDC), also known as Institute 612; its designers included Huang Bin, Hu Rongchao (胡荣超), Dong Chunfeng, and Chen Jiali (陈家礼). It was reportedly produced at the Hanzhong Nanfeng Machine Factory (also known as the Hanzhong Air-to-Air Missile Factory).
[edit] Operators
[edit] Reference
|