RLA-600
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- Country
- Russia
- Launch Vehicles
- UR-700M
- Propellants
- Lox/Kerosene
- Agency
- Glushko bureau
- Bibliography
- 443