LAUSR

Abstract In this study, a dense particles erosion test motor which can simulate the erosion state of a solid rocket motor under high acceleration was developed. Subsequently, erosion experiments were carried out for the ethylene propylene diene monomer composite insulation and the microstructure of the char layer analysed. A turning point effect was found from the influence of the particle impact velocity on the ablation rate, and three erosion modes were determined according to the micro-morphology of the char layer. A reasonable explanation for the different structures of the char layer in the three modes was presented based on the formation mechanism of the compact/loose structure of the char layer.