FIELD: rocket technics.
SUBSTANCE: invention relates to missile technology, specifically to provision in liquid thruster of low thrust of a high degree by agitation of self-igniting fuel components. Chamber consists of a mixing head body with channels for supplying fuel components, a two-component mixing element made in the form of two coaxial capillary tubes, combustion chamber with a transverse partition located opposite the outlet of the mixing element and having channels on the periphery for the passage of the vapor gas. According to the invention, partition is in the form of turbulator with a central shaft with a flat end face facing the outlet of the mixing element and a minimum of two rows of blades with the opposite direction of twist. Additionally, the output edges of the first row of blades may be aligned with the input edges of the second row of blades, and the blades of the latter from the mixing element of the row at the outlet may have angle close to the generators of the combustion chamber.
EFFECT: invention provides intensification of process of mixture formation and obtaining high energy and dynamic characteristics of a liquid thruster of low thrust.
3 cl, 3 dwg
