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RLA-1200
Glushko LOx/Kerosene rocket engine. Design 1974. Proposed engines for the RLA series launch vehicles. This version would use four chambers. 'Down-sized' to 200 metric tons thrust for Energia.

Status: Design 1974. Date: 1972-1975. Thrust: 12,700.00 kN (2,855,000 lbf).

In 1972 to 1974 Glushko proposed lox/kerosene engines for the RLA series launch vehicles and the UR-700M Mars booster with a lift-off thrust of 300 metric tons per chamber. The RLA version would use four chambers for a total thrust of 1200 metric tons. Following rejection of the RLA and the adoption of the Energia design, this chamber design was 'down-sized' to 200 metric tons thrust for Energia.

Chambers: 4.



Country: Russia. Launch Vehicles: RLA-120, RLA-150, RLA-135. Propellants: Lox/Kerosene. Stages: RLA-1. Agency: Glushko bureau. Bibliography: 367.

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