RD-192.2
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. Proposed variant of RD-192. Staged combustion cycle with fuel-rich gas generator. Gimbaling +/- 8 degree in two planes.
In 1998 prototype development was estimated to take four years from go-ahead.
Chamber Pressure: 196.00 bar. Oxidizer to Fuel Ratio: 3.5.
Related
- Country
- Russia
- Propellants
- Lox/LCH4
- Agency
- Glushko bureau