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PL-8  
Initial Operational Capability (IOC): 1988
Total Production: ?
Also Known As: PiLi-8
Origin: China
Parent System: PL-8
Initial Operational Capability (IOC):
Total Production: ?
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Description: The PL-8 is an infrared-guided short-range air-to-air missile based upon the Python 3 missile introduced in the 1980s. It is very capable air-to-air missile and has been provided to the People's Liberation Army Air Force (PLAAF) J-7/F-7, Q-5, J-8/F-8, FBC-1/JH-7, FC-1/J-9 and J-10 fighter aircraft. The PL-9 short-range air-to-air missile leverages technologies from the PL-8.

PL-8 Applications


Combat Aircraft FBC-1 FC-1 FC-1B J-10A J-10B J-10S J-8 J-8 II Su-27

PL-8 Specifications

Dimensions
Diameter: 0.16 meter (6.30 inch)
Length: 2.99 meter (118 inch)
Wingspan: 0.81 meter (31.9 inch)
G-load
Max Maneuvering Load Factor: 35 g
Performance
Max Range: 15 kilometer (8.10 nautical mile)
Min Range: 500 meter (0.27 nautical mile)
Speed
Top Speed: 2 mach (2,391 kph)
Weight
Warhead: 11 kilogram (24.3 pound)
Weight: 115 kilogram (254 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)
Shaft-Horse-Power (shp)

Operators & Related Equipment


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