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Manufacturer Name: RD-0206. Government Designation: 8D47. Designer: Kosberg. Developed in: 1961-64. Application: UR-200 stage 2. Used on stages: UR-200 stage 2. Propellants: N2O4/UDMH Thrust(vac): 59,350 kgf. Thrust(vac): 575.50 kN. Isp: 326 sec. Burn time: 150 sec. Diameter: 1.5 m. Chambers: 1. Chamber Pressure: 147.00 bar. Area Ratio: 81.30. Oxidizer to Fuel Ratio: 2.60. Country: Russia. Status: Developed 1961-64. First Flight: 1964. References: 309 , 320 . Comments: Staged combustion cycle.
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Last update 12 March 2001.
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