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RD-117
Part of RD-107
Glushko LOx/Kerosene rocket engine. Soyuz ST stage 1. In production. Update of RD-107. Little performance change from RD-107, changes may mainly relate to use of all-Russian components. First flown 2001.

Status: In production. Number: 76 . Thrust: 1,021.10 kN (229,552 lbf). Specific impulse: 310 s. Specific impulse sea level: 264 s. Burn time: 130 s.

Chambers: 4. Oxidizer to Fuel Ratio: 2.47.

Country: Russia. Launch Vehicles: Soyuz-ST-B. Propellants: Lox/Kerosene. Stages: Soyuz ST-0. Agency: Glushko bureau. Bibliography: 318, 7497.
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