RD-118

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RD-118

Part of RD-107

Glushko LOx/Kerosene rocket engine. In production. Update of RD-107, used in Soyuz ST launcher. Little performance change from RD-107, changes may mainly relate to use of all-Russian components. First flight 2001.

Status: In production. Number: 19 . Thrust: 999.60 kN (224,719 lbf). Specific impulse: 311 s. Specific impulse sea level: 245 s. Burn time: 300 s.

Chambers: 4. Oxidizer to Fuel Ratio: 2.39.

Country: Russia. Launch Vehicles: Soyuz-ST-B. Propellants: Lox/Kerosene. Stages: Soyuz ST-1. Agency: Glushko bureau. Bibliography: 318, 7498.

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