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RLA-1200


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z 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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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