Initial Operational Capability (IOC): 1992
Total Production: ?
Origin: Russia
Corporations: Raduga JSC
Parent System: Kh-55
Initial Operational Capability (IOC): 1984
Total Production: ?
Family Members: Kh-55, Kh-555, Kh-65SE and RKV-500
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Description: The Kh-65 missile is a tactical derivative of Kh-55 cruise missile. Its range has been reduced to 500-600 km while retains the same navigation system of the Kh-55 missile. The Kh-65 missile has been designed to attack high value targets protected by air defense systems and aircraft. In fact, the Kh-65 can be considered as a conventional standoff weapon/cruise missile. The Russian attack aircraft, such as Su-24 Fencer and Su-30/32/34, will use the Kh-65 missile to attack ground targets from standoff ranges.

Kh-65 Applications

Combat Aircraft Su-30MK Su-30MKI Su-34

Kh-65 Specifications

Diameter: 510 millimeter (20.1 inch)
Length: 6.04 meter (238 inch)
Wingspan: 3.10 meter
CEP: 150 meter
Max Range: 600 kilometer (324 nautical mile)
Top Speed: 256 mps (922 kph)
Warhead: 450 kilogram (992 pound)
Weight: 1,250 kilogram (2,756 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)

Operators & Related Equipment


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