Engine Model: RD-184. Manufacturer Name: RD-184. Designer: Glushko. Developed in: 1996-. Application: Riksha (-0, -1, -2) apogee stage. Propellants: Lox/LCH4. Isp: 322 sec. Diameter: 0.0650 m (0.2130 ft). Length: 0.24 m (0.78 ft). Chambers: 1. Chamber Pressure: 2.00 bar. Oxidizer to Fuel Ratio: 2.50. Country: Russia. Status: Developed 1996-on. Probably attitude correction engine for apogee stage of Riksha-1 launcher project (together with RD-183). Gimbaling +/- 20 degree in two planes. Status 1996 was project, development estimated to take four years.
Bibliography:- Katorgin, B; Klepikov, I, Aviapanorama, "Metanovye ZhRD NPO Energomash im. V.P. Glushko", 7-8/98, Moscow, 1998.