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Engine Model: Isayev V-750V. Designer: Isayev. Developed in: 1954-57. Application: SAM-missile V-750V. Propellants: Nitric acid/Amine. Thrust(vac): 30.400 kN (6,834 lbf). Mass Engine: 43 kg (94 lb). Diameter: 0.48 m (1.56 ft). Length: 0.93 m (3.04 ft). Chambers: 1. Thrust to Weight Ratio: 72.09. Country: Russia. Status: Out of Production. Designation unknown.
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