S09.502
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine. Four chamber engine designed for use in the R-101 (derivative of German Wasserfall). Abandoned by 1950 in favor of single-chamber engine.
Chambers: 4. Thrust (sl): 78.400 kN (17,625 lbf). Thrust (sl): 8,000 kgf. Propellant Formulation: AK20K/TG-02.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-101
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau