SOLID-LIQUID PROPELLANT ROCKET ENGINE

摘要

FIELD: engines and pumps. ^ SUBSTANCE: proposed engine comprises housing with bottom and channel charge secured to housing. Said charge is provided with radial slots and transverse annular slot formed by thin-wall permanent element to fit radial slots. Said thin-wall permanent element mirrors the housing front bottom shape from the joint of said element with front bottom to charge channel. ^ EFFECT: increased filling of engine chamber with fuel, simplified production. ^ 1 dwg