Initial Operational Capability (IOC): 1994
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-65 and RKV-500
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Description: The Kh-65SE is a derivative of Kh-65 cruise missile intended as a long range, aircraft-launched anti-ship missile. It features an active radar seeker added to the Kh-55/65 navigation system for the terminal phase of the flight engagement. The Kh-65SE has been designed to perform as a sea-skimming anti-ship missile with terminal active radar homing.

Kh-65SE Applications

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

Kh-65SE Specifications

Diameter: 510 millimeter (20.1 inch)
Length: 6.04 meter (238 inch)
Wingspan: 3.10 meter
CEP: 150 meter
Max Range: 280 kilometer (151 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)

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