This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com RD-0107

RD-0110 Engine
RD-0110 Engine - Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga.

Credit: © Mark Wade. 33,533 bytes. 294 x 467 pixels.



Manufacturer Name: RD-0107. Government Designation: 8D715K. Other Designations: RD-461, RO-9. Designer: Kosberg. Developed in: 1958-62. Application: R-9, Molniya 8K78, Voskhod 11A57 stage 3. Used on stages: Molniya 2. Propellants: Lox/Kerosene Thrust(vac): 30,380 kgf. Thrust(vac): 297.90 kN. Isp: 326 sec. Burn time: 250 sec. Mass Engine: 410 kg. Diameter: 0.6 m. Chambers: 4. Chamber Pressure: 68.20 bar. Country: Russia. Status: Out of Production. References: 177 . Comments: Gas generator cycle.
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 .