SOIID ROCKET MOTOR STEEL CASE FOR SPACE LAUNCH VEHICLES

摘要

The present invention relates to a metal combustion tube for a solid propellant for a space launch vehicle, and is equipped with a fastening part (200) for connecting to a projectile component on the outer circumferential surface of a spherical metal combustion tube (110) A plurality of spaced apart fastening brackets 140, 150 are included. The present invention has the advantage of lowering the structural ratio of the solid propellant metal combustion tube and increasing the structural stability when generating pressure in the combustion tube.