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Manufacturer Name: RD-184. Designer: Glushko. Developed in: 1996-. Application: Riksha (-0, -1, -2) apogee stage. Propellants: Lox/LCH4 Isp: 322 sec. Diameter: 0.1 m. Length: 0.2 m. Chambers: 1. Chamber Pressure: 2.00 bar. Oxidizer to Fuel Ratio: 2.50. Country: Russia. Status: Developed 1996-on. References: 402 . Comments: 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.
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Last update 12 March 2001.
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