Missile PL-9
Description
The PL-9 air-to-air missile program commenced in the mid-1980s within the People's Republic of China. Its airframe architecture is derived from the earlier PL-5 and PL-7 missiles, while its seeker head integrates sensor technology from the PL-8 and the Israeli Python-3 missile. Batch production is reported to have begun in 1989. The PL-9 has undergone several upgrades, resulting in variants like the PL-9B, certified in the early 1990s, and the PL-9C, certified in the early 2000s. The PL-9C also features a tactical low-altitude surface-to-air missile (SAM) application, this SAM version also being associated with the DK-9 designation, and was first publicly displayed in this role at the 1989 Paris Air Show. Further development has led to the PL-9D version.
The PL-9 is characterized as a short-range, infrared-homing air-to-air missile. It employs a multi-element infrared guidance system featuring a cryogenically cooled seeker, affording it significant off-boresight engagement capabilities. The missile's aerodynamic design incorporates pointed delta fins at the front for flight control, complemented by rollerons on the aft tail surfaces to ensure roll stability, thereby enhancing guidance system performance. It is equipped with a warhead designed for blast-fragmentation effects or an expanding rod mechanism, triggered by a laser proximity fuse. Propulsion is provided by a solid-fuel rocket motor, enabling the missile to achieve supersonic speeds. The PL-9 system demonstrates a high probability of successfully engaging targets, particularly those approaching head-on. Its surface-to-air variant, the DK-9, is engineered for tactical low-altitude air defence.
Entering service around the late 1980s, the PL-9 has been integrated onto a variety of launch platforms, including fixed-wing aircraft, helicopter gunships, and ground-based launchers. Primarily utilized by the People's Liberation Army Air Force and Naval Air Force in an air-to-air capacity, its surface-to-air derivative, the DK-9, has also seen service with PLA ground forces. The DK-9 system offers flexible deployment options, available in both towed configurations with four-rail launchers and self-propelled versions. The latter integrates a four-rail launcher with target acquisition radar and electro-optical directors onto an armored personnel carrier chassis, supported by truck-mounted ground equipment for maintenance and testing. The PL-9, in its SAM role, can operate independently or be incorporated into more comprehensive air defence systems, such as the Type 390 brigade-level combined AAA/SAM network. Beyond China, the PL-9 has been adopted by the air forces of several nations, including Bangladesh, Namibia, Nigeria, and Pakistan.
Summary
Category | Air-to-Air Missile |
Sub-type | Infrared-guided air-to-air missile |
Origin Country | 🇨🇳 China |
Status | In service |
Year of service | 1989 |
Technical specifications
Warhead | High Explosive |
Warhead Weight | 11 |
Diameter | 157 mm (6.2 in) |
Span | 856 mm (33.7 in) |
Length | 2900 mm (114.2 in) |
Flight altitude | 4500 m (14764 ft) |
Weight | 115 kg (254 lb) |
Range | 22 km (14 mi) |
Max. Speed | 2400 km/h (Mach 2.3) |