This page no longer updated from 31 October 2001. Latest version can be found at S5.1

Other Designations: S5.1. Designer: Isayev. Developed in: 1950s late. Application: SAM-missiles 217M and 218. Propellants: Nitric acid/Amine Thrust(vac): 17,000 kgf. Thrust(vac): 167.00 kN. Mass Engine: 122 kg. Diameter: 0.6 m. Length: 1.0 m. Chambers: 1. Country: Russia. Status: Out of Production. References: 342 , 344 . Comments: Designation unknown.
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Last update 12 March 2001.
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© Mark Wade, 2001 .