Isayev 218
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine.
Thrust (sl): 166.000 kN (37,318 lbf). Thrust (sl): 17,000 kgf. Propellant Formulation: AK27I/TG-02.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- S-25
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau