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Military


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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