This page no longer updated from 31 October 2001. Latest version can be found at 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. Used on stages: UR-100 Stage 1. Used on launch vehicles: UR-100. Propellants: N2O4/UDMH Thrust(vac): 22,330 kgf. Thrust(vac): 219.00 kN. Isp: 313 sec. Chambers: 1. Chamber Pressure: 147.00 bar. Country: Russia. Status: Out of Production. First Flight: 1966. References: 313 , 342 , 344 . Comments: 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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .