MULTISTAGE COMBUSTION CHAMBER FOR LIQUID ROCKET ENGINE

摘要

FIELD: rocket engines.SUBSTANCE: invention relates to rocket engines. Multi-stage liquid fuel rocket combustor engine consists of a sequence of elementary combustion chambers, each with its nozzles supplying working fluid and its igniters supplied working fluid.EFFECT: invention provides increased flow rate of spent working fluid by increasing flow rate of working body per unit time.1 cl, 1 dwg