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9M311  
Initial Operational Capability (IOC): 1990
Total Production: ?
Origin: Russia
Parent System: 9M311
Initial Operational Capability (IOC): 1990
Total Production: ?
Family Members: 9M311-1
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Description: The 9M311 is a Surface-to-Air Missile (SAM) featuring a semi-active radar guidance system. It is intended against rotary and fixed wing aircraft flying at a maximum speed of Mach 1.5 and at altitudes between 15 and 3,500 meters. The 9M311 missile is associated to the Tunguska-M and Kashtan weapon systems.

9M311 Applications


Artillery Systems Tunguska-M Fighting Ships Project 1143.5 Project 1144.2 Project 1154.0 Project 11541 Project 1155 Project 20380 Protection Systems Kashtan

9M311 Specifications

Dimensions
Length: 2.80 meter (110 inch)
Performance
Max Range: 10,000 meter (5.40 nautical mile)
Min Range: 2,500 meter (1.35 nautical mile)
Target's Max Altitude: 3,500 meter (2.18 mile)
Target's Min Altitude: 15 meter
Speed
Top Speed: 3,230 kph (2,007 mph)
Weight
Warhead: 9 kilogram (19.8 pound)
Weight: 57 kilogram (126 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 ?6
 
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