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Engine Model: S5.1. Other Designations: S5.1. Designer: Isayev. Developed in: 1950s late. Application: SAM-missiles 217M and 218. Propellants: Nitric acid/Amine. Thrust(vac): 167.000 kN (37,543 lbf). Throttled thrust(vac): 49.000 kN (11,015 lbf). Mass Engine: 122 kg (268 lb). Diameter: 0.62 m (2.05 ft). Length: 1.02 m (3.33 ft). Chambers: 1. Thrust to Weight Ratio: 139.34. Country: Russia. Status: Out of Production. Designation unknown.
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