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PL-12  
Initial Operational Capability (IOC): 2005
Total Production: ?
Also Known As: SD-10 and SD-10A
Origin: China
Corporations: AVIC I
Parent System: PL-12
Initial Operational Capability (IOC): 2005
Total Production: ?
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Description: The PL-12, SD-10 export designation, is an advanced beyond visual range air-to-air missile outfitted with an active homing head. It is powered by a rocket motor that provides a top speed of Mach 4 and a maximum range of 70 kilometers. It has been reported that this new missile has been developed with Russian (seeker) and Israeli (Derby missile) technical assistance. The PL-12 is intended to equip the latest generation Chinese-built fighter aircraft such as FC-1 and J-10.

PL-12 Applications


Strike & Fighter Aircraft F-10B F-16 FC-1 FC-1B J-10A J-10S Su-27

PL-12 Specifications

Dimensions
Diameter: 203 millimeter
Length: 3.85 meter
Wingspan: 674 millimeter
G-load
Max Maneuvering Load Factor: 38 g
Performance
Max Range: 70 kilometer
Speed
Top Speed: 4 mach (1,328 mps)
Weight
Weight: 180 kilogram
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


OperatorsItems

Grand Total ?2
 

PL-12 Links & Resources

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