Kh-65  
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
Reviews
There are no reviews so far

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

Dimensions
Diameter: 510 millimeter (20.1 inch)
Length: 6.04 meter (238 inch)
Wingspan: 3.10 meter
Performance
CEP: 150 meter
Max Range: 600 kilometer (324 nautical mile)
Speed
Top Speed: 256 mps (922 kph)
Weight
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


OperatorsItems

Grand Total ?1
 
Copyright © 2003-2017 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.