Государственное Предприятие «Конструкторское Бюро «Южное» Им М.К. Янгеля
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A gas generator of liquid-fuel rocket engine has a nozzle for supply of oxidizer, mixing head, outer bottom, nozzle for fuel supply, collector, cylindrical chamber, flange in outlet section of which gas swirler is installed, this is arranged as cylinder with conical bottom. In the bottom axial opening dis provided, in the cylindrical section – one or several rows of openings dtotal area of which is chosen from condition of provision of losses of pressure there equal to (3.55)% of rated pressure in gas generator and ratio between the value of area of axial opening and total area of tangent openings is 1.
UAA200600542A2006-01-202006-01-20Gas generator of liquid-fuel rocket engine
UA83232C2
(en)