Initial Operational Capability (IOC):
Also Known As: AS-9 Kyle
Parent System: Kh-28
Initial Operational Capability (IOC): 1971
Total Production: ?
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Description: Kh-28 is a two-stage liquid fuel rocket engine powered supersonic anti-radiation missile used on the Su-7/17/22, Su-24 and Tu-22M strike aircraft. Kh-28 builds on the technology and knowledge previously utilized on the Kh-22 and KSR-5 missiles. It uses a passive radar homing seeker to track the enemy radar transmitter emissions. The Kh-28 was retired by the Russian/Soviet Air Force in the 1990s.
Number of Stages: 2
Diameter: 430 millimeter (16.9 inch)
Length: 5.97 meter (235 inch)
Wingspan: 1.93 meter
Max Range: 120 kilometer (65 nautical mile)
Top Speed: 972 mps (3,500 kph)
Warhead: 160 kilogram (353 pound)
Weight: 720 kilogram (1,587 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)
Operators & Related Equipment
Grand Total ?1
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