S2.713
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.)
Chambers: 1 + 4. Propellant Formulation: AK27I/TG-02. Oxidizer to Fuel Ratio: 3.48.
Related
- Family
- Storable liquid
- Country
- Russia
- Engines
- S2.713
- Launch Vehicles
- R-13
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau