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RD-0107
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 | RD-0110 Engine
Credit - © Mark Wade
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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. Propellants: Lox/Kerosene. Thrust(vac): 297.900 kN (66,971 lbf). Isp: 326 sec. Burn time: 250 sec. Mass Engine: 410 kg (900 lb). Diameter: 0.64 m (2.09 ft). Chambers: 4. Chamber Pressure: 68.20 bar. Thrust to Weight Ratio: 74.09. Country: Russia. Status: Out of Production. Gas generator cycle.
Bibliography and Further Reading - Varfolomyev, Timothy, Spaceflight, "Soviet Rocketry that Conquered Space - 8K71 launches", 1996, Volume 38, page 31. 1: Sp 95/37-260; Sp 96/38-31 (8K71 launches); 2: Sp 96/38-48; 3: Sp 96/38-206; Sp 96/38-317 (designatons); 4: Sp 98/40-28; 5:Sp 98/40-85
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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