Isayev R-17
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Kerosene rocket engine. R-17. Out of production. Designation unknown. First flight 1961.
Thrust (sl): 131.210 kN (29,497 lbf). Thrust (sl): 13,380 kgf. Engine: 120 kg (260 lb). Propellant Formulation: AK27I/TM185. Thrust to Weight Ratio: 111.49.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-17
- Propellants
- Nitric acid/Kerosene
- Stages
- R-17 stage
- Agency
- Isayev bureau