S-125 Pechora
The S-125 is somewhat mobile, an improvement over the S-75 system. The missiles are typically deployed on fixed turrets containing two or four but can be carried ready-to-fire on ZIL trucks in pairs. Reloading the fixed launchers takes a few minutes.
Type
Role
Country of Origin
Introduction
Note
The S-125 Neva/Pechora (Russian: С-125 "Нева"/"Печора", NATO reporting name SA-3 Goa) Soviet surface-to-air missile system was designed by Aleksei Isaev to complement the S-25 and S-75. It has a shorter effective range and lower engagement altitude than either of its predecessors and also flies slower, but due to its two-stage design it is more effective against more maneuverable targets. It is also able to engage lower flying targets than the previous systems, and being more modern it is much more resistant to ECM than the S-75. The 5V24 (V-600) missiles reach around Mach 3 to 3.5 in flight, both stages powered by solid fuel rocket motors. The S-125, like the S-75, uses radio command guidance. The naval version of this system has the NATO reporting name SA-N-1 Goa and original designation M-1 Volna (Russian Волна – wave).
Mass: 953 kg
Length: 6.09 m
Diameter: 375 mm
Warhead: Frag-HE
Warhead weight: 60 kg
Detonation mechanism: Proximity fuse
Wingspan: 2.2 m
Propellant: Solid propellant rocket motor
Operational range: 35 kilometres (22 mi)
Flight altitude: 18,000 metres (59,000 ft)
Guidance system: RF CLOS
Type of packaging
Quantity per pack
Number in a wooden case
Dimensions of a wooden case
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Weight of wooden case
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UN Number
Hazard Class
S-125 Pechora
Description
Type
Role
Country of Origin
Introduction
Note
The S-125 is somewhat mobile, an improvement over the S-75 system. The missiles are typically deployed on fixed turrets containing two or four but can be carried ready-to-fire on ZIL trucks in pairs. Reloading the fixed launchers takes a few minutes.
The S-125 Neva/Pechora (Russian: С-125 "Нева"/"Печора", NATO reporting name SA-3 Goa) Soviet surface-to-air missile system was designed by Aleksei Isaev to complement the S-25 and S-75. It has a shorter effective range and lower engagement altitude than either of its predecessors and also flies slower, but due to its two-stage design it is more effective against more maneuverable targets. It is also able to engage lower flying targets than the previous systems, and being more modern it is much more resistant to ECM than the S-75. The 5V24 (V-600) missiles reach around Mach 3 to 3.5 in flight, both stages powered by solid fuel rocket motors. The S-125, like the S-75, uses radio command guidance. The naval version of this system has the NATO reporting name SA-N-1 Goa and original designation M-1 Volna (Russian Волна – wave).
Technical data and Packaging
Mass: 953 kg
Length: 6.09 m
Diameter: 375 mm
Warhead: Frag-HE
Warhead weight: 60 kg
Detonation mechanism: Proximity fuse
Wingspan: 2.2 m
Propellant: Solid propellant rocket motor
Operational range: 35 kilometres (22 mi)
Flight altitude: 18,000 metres (59,000 ft)
Guidance system: RF CLOS
Type of packaging
Quantity per pack
Number in a wooden case
Dimensions of a wooden case
Weight of the package
Weight of wooden case
Weight
Volume m3
UN Number
Hazard Class
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