Initial Operational Capability (IOC): 1993
Total Production: ?
Origin: Russia
Parent System: S-13
Initial Operational Capability (IOC): 1983
Total Production: ?
Family Members: S-13, S-13DF and S-13T
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Description: The S-13 is a 122mm unguided rocket developed by the former Soviet Union for use by a wide variety of airborne platforms to engage targets on the ground. These rockets are deployed on B-13L external pods carrying five S-13s each and compatible with both fixed-wing and rotary-wing aircraft such as Su-24, Su-25, Su-30SM, Mi-28, Ka-52, Mig-29 and Mig-35. Its development started in the 1970s entering service with the Soviet Union Air Force in 1983.

The S-13OF is a variant introduced in 1993 and equipped with a high explosive (HE) fragmentation warhead. The 450 diamond-shaped fragments (25-30 grams each) produced by the S-13OF rocket can penetrate Armored Personnel Carriers (APCs) and Infantry Fighting Vehicles (IFVs).

S-13OF Applications

Combat Aircraft Ka-52 Alligator Su-24 Su-25 Su-25SM3 Su-34 Su-39

S-13OF Specifications

Number of Fragments: 450
Caliber: 122 millimeter
Length: 2.89 meter (114 inch)
Max Range: 3,000 meter (1.62 nautical mile)
Min Range: 1,600 meter (0.86 nautical mile)
Max Launch Airspeed: 1,200 kph
Min Launch Airspeed: 600 kph
Top Speed: 590 mps (2,125 kph)
Max Operating Temperature: +60 � Celsius
Min Operating Temperature: -60 � Celsius
Explosive Weight: 6.90 kilogram (15.2 pound)
Submunition Fragment Weight: 35 gram
Warhead: 31.7 kilogram (70 pound)
Weight: 69 kilogram (152 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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