This page no longer updated from 31 October 2001. Latest version can be found at RD-0108

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-0108. Government Designation: 8D715P. Other Designations: RD-461, 11D55, 8D715K, RO-8. Designer: Kosberg. Developed in: 1961-65. Application: Voskhod 11A57, Molniya 8K78 stage 3. Used on stages: Molniya 8K78-2, Voskhod 11A57-2. Used on launch vehicles: Molniya 8K78, Voskhod 11A57. 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. First Flight: 1960. Last Flight: 1976. Flown: 331. References: 177 .
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Last update 12 March 2001.
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