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Engine Model: RD-0217. Manufacturer Name: RD-0217. Government Designation: 15D2. Designer: Kosberg. Developed in: 1963-66. Application: UR-100, UR-100K / RS-10 (SS-11) stage 1. Propellants: N2O4/UDMH. Thrust(vac): 219.000 kN (49,233 lbf). Isp: 313 sec. Chambers: 1. Chamber Pressure: 147.00 bar. Country: Russia. Status: Out of Production. First Flight: 1966.

Staged combustion cycle. Version of RD-0216 without tank pressurization system. Manufacturing until 1974, operational use until 1991.

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