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Designed for short range firing.
A single stage, liquid fuel, theater ballistic missile with an inseparable warhead. Put into service in 1962.
The missile is fired from tracked and wheeled launchers used to transport a fueled missile. On delivery of a missile to the firing site prelaunch tests, preparation procedures, targeting, fueling and launch are performed.
| Basic characteristics |
| Takeoff mass, t |
5.8 |
| Maximum range, km |
300 |
| Warhead |
inseparable |
| Number of RVs |
1 |
| Guidance system |
inertial |
| Number of stages |
1 |
| Length, m |
11.2 |
| Diameter, m |
0.88 |
| Propellant |
liquid |
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