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.
Status: Developed 1996-on. Date: 1996-. Thrust: 2,089.00 kN (469,625 lbf). Specific impulse: 341 s. Specific impulse sea level: 311 s. Height: 3.62 m (11.87 ft). Diameter: 1.45 m (4.75 ft).
Chamber Pressure: 245.00 bar. Oxidizer to Fuel Ratio: 3.