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Kh-31PK  
Initial Operational Capability (IOC): 2009
Total Production: ?
Origin: Russia
Corporations: Tactical Missiles Corporation (KTRV)
Parent System: Kh-31
Initial Operational Capability (IOC): 1988
Total Production: ?
Family Members: Kh-31A, Kh-31AD, Kh-31P and Kh-31PD
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Description: The Kh-31, AS-17 Krypton NATO-codename, is an advanced, long range, highly supersonic missile designed to withstand countermeasures effects. The Kh-31 propulsion system consists of a solid-fuel rocket engine which accelerates the missile to Mach 1.8 airspeed. Then this engine is dropped and a jet engine ignites using the missile's within space as a combustion chamber. The missile accelerates to Mach 3+ thanks to the jet engine.

The Kh-31PK derives from the Kh-31P anti-radiation missile and is fitted with a proximity fuze and a variety of passive radar seeker. It is intended to engage ground-based radars using continuous or pulse modes that make part of medium- and long-range air defense systems and stand along long-range surveillance radars.

Kh-31PK Specifications

Number of Stages: 2
Dimensions
Diameter: 360 millimeter (14.2 inch)
Length: 4.80 meter (189 inch)
Wingspan: 914 millimeter
Performance
Max Launch Altitude: 15,000 meter
Max Range: 110 kilometer (59 nautical mile)
Min Launch Altitude: 100 meter
Min Range: 15 kilometer
Speed
Max Launch Airspeed: 1,250 kph (1.05 mach)
Min Launch Airspeed: 650 kph (0.54 mach)
Weight
Weight: 605 kilogram (1,334 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)

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