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Isayev V-750V
Isayev Nitric acid/Amine rocket engine. SAM-missile V-750V. Out of Production. Designation unknown.

Status: Out of Production. Date: 1954-57. Thrust: 30.40 kN (6,834 lbf). Unfuelled mass: 43 kg (94 lb). Height: 0.93 m (3.04 ft). Diameter: 0.48 m (1.56 ft).

Engine: 43 kg (94 lb). Propellant Formulation: AK20K/TG-02. Thrust to Weight Ratio: 72.09.



Family: Storable liquid. Country: Russia. Launch Vehicles: S-75. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 342, 344.

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