Engine Model: RD-0216. Manufacturer Name: RD-0216. 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: Design 1964. First Flight: 1965. Last Flight: 1984. Flown: 1,128. Date is that of the authorizing Decree. Actual development earlier, since first launch occured November 1963.. Staged combustion cycle. Includes tank pressurization system (RD-0217 without tank press.). Manufacturing until 1974, operational until 1991.
RD-0216 used on Rocket Stages
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