There are 12 images added between 23 October 2013 and 26 January 2017
Initial Operational Capability (IOC):
Also Known As: SD-10 and SD-10A
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.
Diameter: 203 millimeter (7.99 inch)
Length: 3.85 meter (152 inch)
Wingspan: 674 millimeter (26.5 inch)
Max Maneuvering Load Factor: 38 g
Max Range: 70 kilometer (37.8 nautical mile)
Top Speed: 4 mach (4,782 kph)
Weight: 180 kilogram (397 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)
There are 3 news between
27 May 2016 and 26 Jan 2017
Operators & Related Equipment
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