This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: Isayev. Developed in: 1954-57. Application: SAM-missile V-750V. Propellants: Nitric acid/Amine Thrust(vac): 3,100 kgf. Thrust(vac): 30.40 kN. Mass Engine: 43 kg. Diameter: 0.5 m. Length: 0.9 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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