This page no longer updated from 31 October 2001. Latest version can be found at RD-192

Manufacturer Name: RD-192. Designer: Glushko. Developed in: 1996-. Propellants: Lox/LCH4 Thrust(vac): 218,015 kgf. Thrust(vac): 2,138.00 kN. Isp: 356 sec. Isp (sea level): 330 sec. Mass Engine: 3,300 kg. Diameter: 2.0 m. Length: 4.0 m. Chambers: 1. Chamber Pressure: 257.00 bar. Oxidizer to Fuel Ratio: 3.50. Country: Russia. Status: Developed 1996-. References: 325 . Comments: Proposed methane-variant of RD-191. Gimbaling +/- 8 degree in two planes. Status 1996 was project based on RD-191 prototype, development estimated for four years. Nozzle expansion ratio is 262/0.75=349.
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Last update 12 March 2001.
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© Mark Wade, 2001 .