SA-4 GANEF
| Specifications | |
|---|---|
| Deployment | Russia, 9 other countries |
| Deployment Year | 1967 |
| Length | 8.8m (SA-4A), 8.4m (SA-4B) |
| Body Diameter | 86 cm |
| Launch Weight | 2,500 kg |
| Warhead | 135kg HE fragmentation effect |
| Guidance | Radio command, semiactive radar |
| Propulsion | Ramjet sustainer, 4 solid rocket boosters |
| Range | 55km (SA-4A), 50km (SA-4B) |
| Design | Lyulev Design Bureau |
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