R-101B.36000-0
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine. Single chamber engine designed for use in the R-101B and R-108 (derivative of German Wasserfall).
Never flown in this application but developed for use in the V-300 SAM and R-11 SSM.
Thrust (sl): 83.300 kN (18,727 lbf). Thrust (sl): 8,500 kgf. Propellant Formulation: AK20K/TG-02.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau