Journal of Energetic Materials

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In order to preserve structure and also achieve the desired thrust rocket motor, engine Case temperature should be prevented increase excess.This operation the can be done by Insulation. EPDM rubber because of advantages such as low specific weight, improve aging properties, as long as thermal insulation for solid propellant motors case bond Introduced and its properties are investigated in this study. However these advantages, EPDM, a rubber is nonpolar and it weakens the adhesion composite solid propellant is based HTPB. According to importance of a strong connection between the insulation and solid propellant, different methods of modification of EPDM rubber surface and improve adhesion strength has been studied.

Keywords: EPDM, Insulation, Ablation, Surface Modification, Adhesion

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