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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

Diameter: 203 millimeter
Length: 3.85 meter
Wingspan: 674 millimeter
Max Maneuvering Load Factor: 38 g
Max Range: 70 kilometer
Top Speed: 4 mach (1,328 mps)
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


Grand Total ?2

PL-12 Links & Resources

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