FIELD: rocket technics.
SUBSTANCE: invention relates to rocket engineering. Low-thrust liquid-propellant engine chamber consisting of mixing head with nozzles, chamber housing with subcritical and supersonic nozzle parts, wherein the housing of the chamber is formed by concentric shells with gaps between them, which are interconnected with the areas of successively decreasing pressure from the internal gap to the external one.
EFFECT: invention reduces thermal stresses in the combustion chamber housing.
1 cl, 1 dwg
| Title | Year | Author | Number |
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|
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|
RU2204047C2 |
