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Initial Operational Capability (IOC): 1980
Total Production: ?
Also Known As: AS-11 Kilter and Kh-58E
Origin: Russia
Corporations: Tactical Missiles Corporation (KTRV)
Parent System: Kh-58
Initial Operational Capability (IOC): 1980
Total Production: ?
Family Members: Kh-58UShKA and Kh-58UShKE
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Description: The Kh-58 is a supersonic, anti-radiation missile developed by the Soviet Union to counter enemy air defenses and radar sites operating in A/A', B/B' and C frequency bands. The missile can receive target indication and guidance from the aircraft onboard sensors or from an external pod carrying a sensor set. Equipped with a passive homing head the missile can engage radar emitters day/night and in adverse weather conditions. It was designed as the replacement for older Kh-28 missiles.

The basic Kh-58E missile range varies from 8 kilometers to 200 kilometers depending on the flight path. Typically, the missile was launched from a Mig-25BM, Su-22M4, Su-25TK, and/or Su-24MK aircraft in the Russian/Soviet air force. The Mig-25BM is able to release this missile flying at Mach 2+ at altitudes of 20,000 meters.

Kh-58 Applications

Combat Aircraft Su-17 Su-24

Kh-58 Specifications

Diameter: 380 millimeter (15.0 inch)
Length: 4.80 meter (189 inch)
Wingspan: 1.17 meter
Max Launch Altitude: 20,000 meter
Max Range: 200 kilometer (108 nautical mile)
Min Launch Altitude: 200 meter
Min Range: 8 kilometer
Max Launch Airspeed: 2.35 mach (2,810 kph)
Min Launch Airspeed: 0.47 mach (562 kph)
Top Speed: 1,195 mps (4,303 kph)
Warhead: 149 kilogram (328 pound)
Weight: 650 kilogram (1,433 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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