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Initial Operational Capability (IOC):
Also Known As: PiLi-9, PL-9C and PL-9D
Parent System: PL-9
Initial Operational Capability (IOC): 1989
Total Production: ?
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Description: The PiLi-9 (PL-9) is a short-range air-to-air missile (AAM) developed in China for the export market based upon the PL-5, PL-7 and Python 3 missile technologies. The PL-9 utilizes a derivative of the Python 3's infrared seeker. The PL-9 missile program was launched in the mid-1980s and first deliveries occurred in 1989. The PL-9C is an improved variant introduced in the 1990s featuring extended range from 5 kilometers to 22 kilometers and increased launch weight (115 kg vs. 123 kg), warhead (10 kg vs. 12 kg) and G maneuvering factor (35g vs. 40g). The PL-9D is a surface-to-air missile variant also introduced in the 1990s. The PL-9D missile system has been ordered by the People's Liberation Army (PLA) ground forces. The PL-9 air-to-air missile did not receive export orders or they were not reported. Maybe Iran ordered the missile for their Chinese F-7 fighters. The PL-9C missile was ordered by Bangladesh in 2006 and 2008 for use on the F-7BG fighters.
Off-Boresight Capability: 40 �
Diameter: 157 millimeter (6.18 inch)
Length: 2.90 meter (114 inch)
Wingspan: 0.65 meter (25.6 inch)
Max Maneuvering Load Factor: 40 g
Max Range: 22,000 meter (11.9 nautical mile)
Min Range: 500 meter (0.27 nautical mile)
Top Speed: 2.10 mach (2,511 kph)
Warhead: 12 kilogram (26.5 pound)
Weight: 123 kilogram (271 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
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