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Engine Model: RD-0206. Manufacturer Name: RD-0206. Government Designation: 8D47. Designer: Kosberg. Developed in: 1961-64. Application: UR-200 stage 2. Propellants: N2O4/UDMH. Thrust(vac): 575.500 kN (129,378 lbf). Isp: 326 sec. Burn time: 150 sec. Diameter: 1.47 m (4.82 ft). 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. Staged combustion cycle.
Bibliography:- Golubev, A A, KB KhimAvtomatiki - Straniy Istorii, Vol. 1, Voronezh 1995 via Dietrich Haeseler.
- Glushko, V P, Albom Konstruktsiy ZhRD, Vol. 1 1968, Vol. 3 & 4 1969 via Dietrich Haeseler.
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