RD-184
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/LCH4 rocket engine. Developed 1996-on. Attitude correction engine for apogee stage of Riksha-1 launcher project (together with RD-183). Gimbaling +/- 20 degree in two planes.
In 1996 prototype development was estimated to take four years from go-ahead.
Chamber Pressure: 2.00 bar. Oxidizer to Fuel Ratio: 2.5.
Related
- Country
- Russia
- Launch Vehicles
- Riksha
- Propellants
- Lox/LCH4
- Agency
- Glushko bureau
- Bibliography
- 402