RD-192.3
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. Gas generator cycle. Gimbaling +/- 8 degree in two planes. Status 1998 was project based on RD-191 prototype, development estimated for four years.
Chamber Pressure: 245.00 bar. Oxidizer to Fuel Ratio: 3.
Related
- Country
- Russia
- Propellants
- Lox/LCH4
- Agency
- Glushko bureau