Saturday, October 11, 2008

PL-12

IOC: 2005

Also Known As
SD-10 (export designation)

Origin
China

Contractor/s
AVIC I

Applications
FC-1
J-10A
J-10S

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.

Specifications
Dimensions: Diameter 203 mm, Length 3.9 m, Wingspan 674 mm

Weights: Max Weight 180 kg (397 lb)

Performance: Max Range 70 km (38 nm), Top Speed Mach 4 (4,780 kph)

G Loads: Max Maneuvering Load Factor 38 g

Operators

China

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)

Last Updated: Friday, October 10, 2008

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