This page no longer updated from 31 October 2001. Latest version can be found at 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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .