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RD-192S
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Manufacturer Name: RD-192S. Designer: Glushko. Developed in: 1996-. Propellants: Lox/LCH4. Thrust(vac): 2,128.000 kN (478,393 lbf). Isp: 372 sec. Diameter: 2.40 m (7.80 ft). Length: 4.82 m (15.81 ft). Chambers: 1. Chamber Pressure: 196.00 bar. Oxidizer to Fuel Ratio: 3.50. Country: Russia. Status: Developed 1996-on. Proposed variant of RD-192. Staged combustion cycle with oxidizer-rich gas generator. Gimbaling +/- 8 degree in two planes. Status 1998 project based on RD-191 protoype, development estimated for four years.
Bibliography and Further Reading - Katorgin, B; Klepikov, I, Aviapanorama, "Metanovye ZhRD NPO Energomash im. V.P. Glushko", 7-8/98, Moscow, 1998.
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