This page no longer updated from 31 October 2001. Latest version can be found at Isayev R-17

Designer: Isayev. Developed in: 1958-64. Application: R-17. Used on stages: R-17. Used on launch vehicles: Scud. Propellants: Nitric acid/Kerosene Thrust(vac): 13,379 kgf. Thrust(vac): 131.20 kN. Mass Engine: 120 kg. Diameter: 0.8 m. Length: 1.5 m. Chambers: 1. Country: Russia. Status: Out of Production. First Flight: 1961. References: 342 , 344 . Comments: Designation unknown.
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Last update 12 March 2001.
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© Mark Wade, 2001 .