Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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-600
Glushko LOx/Kerosene rocket engine. Design 1972. Two-chamber version of RLA-300. Proposed for the RLA series launch vehicles and the UR-700M Mars booster.

Status: Design 1972. Date: 1972-1975. Thrust: 6,370.00 kN (1,432,030 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 UR-700M version would use two chambers for a total thrust of 600 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 and Vulkan.

Chambers: 2.



Country: Russia. Launch Vehicles: UR-700M. Propellants: Lox/Kerosene. Stages: UR-700M-2, UR-700M-1. Agency: Glushko bureau. Bibliography: 443.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use