METHOD FOR THE PRODUCTION OF A COMBUSTION CHAMBER FOR SOLID PROPELLANT ROCKET MOTOR

摘要

The method comprises placing around the propellant 12, with interposition of a glue of sectors of the tube 22 that juxtaposed edge to edge, constitute a cylindrical tube and the embodiment of the tube of a winding at least in the circumferential direction. The front and rear bearing a base 17 and a tuyere 15 may be assembled the tubular structure formed by the sectors of the tube, by adhesive bonding to the inside of said structure, or in a variant, by a helical winding carried out simultaneously on the bottom and on the tubular structure.