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S2.713
Isayev Nitric acid/Amine rocket engine. R-13 (SS-N-4). Out of Production. First engine to employ gas generator on main propellants. One main and four vernier thrusters. (Mixture derived ratio from tank content.)

Status: Out of Production. Date: 1956-61. Thrust: 252.20 kN (56,697 lbf).

Chambers: 1 + 4. Propellant Formulation: AK27I/TG-02. Oxidizer to Fuel Ratio: 3.48.

Family: Storable liquid. Country: Russia. Engines: S2.713. Launch Vehicles: R-13. Propellants: Nitric acid/Amine. Agency: Isayev bureau. Bibliography: 319, 340, 344.
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