RUBBER COMPOSITION ADDED CARBON FABRIC FOR SOLID ROCKET MOTOR INSULATION

摘要

The present invention relates to a rubber composition for heat resistance materials of a solid propulsion system, which protects the inside of a combustion chamber from a stronger flow of gas by inserting carbon fibers in an EPDM based rubber composition. The heat resistance material of the present invention has effects of improving abrasion of the heat resistance material in a multiple pulse rocket motor having the stronger flow of gas compared with in an existing rocket propulsion system having a generous combustion gas flow.