Generated by DeepSeek V3.2| Chinese PL-2 | |
|---|---|
| Name | PL-2 |
| Caption | A PL-2 missile on display. |
| Type | Short-range, infrared homing air-to-air missile |
| Origin | People's Republic of China |
| Service | 1967–1990s |
| Used by | People's Liberation Army Air Force |
| Designer | China Academy of Launch Vehicle Technology |
| Manufacturer | China Aerospace Science and Industry Corporation |
| Production date | 1967–1980s |
| Variants | PL-2, PL-2A, PL-2B |
| Weight | 76 kg (168 lb) |
| Length | 2.99 m (9 ft 10 in) |
| Diameter | 0.127 m (5 in) |
| Wingspan | 0.53 m (1 ft 9 in) |
| Warhead | Blast-fragmentation |
| Warhead weight | 11.3 kg (25 lb) |
| Detonation | Proximity fuze |
| Engine | Solid-fuel rocket |
| Speed | Mach 2.5 |
| Guidance | Infrared homing |
| Launch platform | Shenyang J-6, Chengdu J-7, Nanchang Q-5 |
Chinese PL-2 is a short-range, infrared homing air-to-air missile developed by the People's Republic of China during the 1960s. It was the first indigenously produced guided air-to-air missile to enter service with the People's Liberation Army Air Force, marking a significant milestone in the development of Chinese aerospace industry. Based heavily on the Soviet K-13 missile, the PL-2 provided Chinese fighter aircraft with a beyond-visual-range engagement capability for the first time.
The development of the PL-2 was initiated in the early 1960s following the Sino-Soviet split, which severely disrupted the supply of advanced Soviet weapons to China. Chinese engineers obtained examples of the Soviet Vympel K-13 missile, a reverse-engineered version of the American AIM-9 Sidewinder acquired during the Second Taiwan Strait Crisis. The task of replicating and adapting this technology was assigned to the China Academy of Launch Vehicle Technology under the broader Third Front campaign to develop self-sufficient defense industries. The program faced significant challenges in mastering the infrared homing seeker technology and the complex rocket motor, but successful testing was completed by 1964. Official state acceptance and entry into service with the People's Liberation Army Air Force occurred in 1967, providing a critical stopgap weapon during a period of heightened tension with both the Soviet Union and the United States.
The PL-2 is a first-generation, passive infrared homing missile with a design nearly identical to its Soviet progenitor, the K-13. Its airframe consists of a cylindrical body with four large delta-shaped control fins at the rear and four smaller fixed wings at the mid-body. The missile is powered by a single-stage, solid-propellant rocket engine that accelerates it to a maximum speed of approximately Mach 2.5. The infrared homing seeker in the nose cone, sensitive to the heat emissions from aircraft engine exhausts, required the launching aircraft to maneuver into the target's rear hemisphere for a successful lock. The warhead is an 11.3 kg blast-fragmentation type triggered by an active proximity fuze or impact fuze. With a launch weight of 76 kg and a length of 2.99 meters, the missile had an effective range of about 7 kilometers and could engage targets at altitudes up to 21,500 feet.
The PL-2 entered operational service with the People's Liberation Army Air Force in 1967, primarily arming the Shenyang J-6 and later the Chengdu J-7 fighter aircraft, as well as the Nanchang Q-5 attack plane. It became the standard short-range air-to-air missile for the People's Republic of China throughout the 1970s and 1980s, seeing no confirmed combat use by China itself. The missile's limitations, including its need for a rear-aspect launch, susceptibility to countermeasures, and relatively poor performance in cloud cover, became apparent as more advanced Western and Soviet missiles like the AIM-9L Sidewinder and R-73 entered service. During the Soviet–Afghan War, PL-2 missiles supplied to the Afghan Air Force were reportedly used in engagements against Mujahideen forces. By the late 1980s, the PL-2 was largely relegated to training roles and was progressively replaced by more advanced domestic designs like the PL-5 and PL-8.
* **PL-2:** The original baseline production model, a direct copy of the Soviet K-13 missile. * **PL-2A:** An improved variant introduced in the 1970s featuring a more sensitive cooled infrared homing seeker, offering better performance against low-infrared-signature targets and a slight increase in effective range. * **PL-2B:** A further upgrade developed in the 1980s, incorporating a new proximity fuze and improved resistance to simple infrared countermeasures like flares. It represented the final evolution of the PL-2 family before the design was superseded.
The primary operator of the PL-2 was the People's Liberation Army Air Force. The missile was also exported to several allied and client states during the Cold War, consistent with China's foreign policy of supporting revolutionary movements and non-aligned nations. Known export customers included Albania under Enver Hoxha, Pakistan, Bangladesh, Tanzania, and the Democratic Republic of Afghanistan. Many of these exported missiles were used on Chinese-supplied aircraft such as the Shenyang J-6 and Chengdu J-7. The PL-2 has long been retired from active frontline service in China, though it may have remained in limited storage or training use with some export customers into the 1990s.
Category:Air-to-air missiles of China Category:Cold War missiles of China