This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Manufacturer Name: RD-0217. 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. 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: Staged combustion cycle. Version of RD-0216 without tank pressurization system. Manufacturing until 1974, operational use until 1991.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .