S-25  
Initial Operational Capability (IOC): 1988
Total Production: ?
Also Known As: S-25L, S-25O, S-25OF and S-25OFM
Origin: Russia
Parent System: S-25
Initial Operational Capability (IOC): 1988
Total Production: ?
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Description: The S-25 is a 340mm heavyweight air launched rocket developed by the former Soviet Union in the 1980s and utilized for the first time during the war in Chechnya in the 1990s. The rocket has a maximum range of 3-4 kilometers flying at supersonic speed. A single rocket carries a 190 kilogram warhead. The S-25OF variant is fitted with a high explosive (HE) fragmentation warhead, the S-25O is fitted with a fragmentation warhead with radio proximity fuze, the S-25OFM is intended to penetrate hardened targets such as bunker and buried fortification and the S-25L is laser-guided variant. The S-25 rocket has been designed to be launched from Su-25, Su-27, Su-30, Su-34 and Su-35 aircraft using the O-25 rocket launcher which carries one S-25.

S-25 Applications


Combat Aircraft Su-25 Su-25SM3 Su-27 Su-30MKI Su-34 Su-35S

S-25 Specifications

Dimensions
Caliber: 340 millimeter
Length: 3.31 meter (130 inch)
Performance
Max Range: 4,000 meter (2.16 nautical mile)
Speed
Top Speed: 700 mps (2,521 kph)
Weight
Warhead: 190 kilogram (419 pound)
Weight: 480 kilogram (1,058 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
 
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