S5.3M
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine. R-9 (SS-8) missile stage 1. Out of Production. Proposed for R-9 missile stage 1. Four engines per stage. 396,7 kN sea-level.
Chambers: 4. Engine: 433 kg (954 lb). Chamber Pressure: 66.00 bar. Area Ratio: 9.55. Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 93.42. Oxidizer to Fuel Ratio: 3.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau