Date of Publication :17th January 2024

Abstract: The major goal of this study is to design and build a solid rocket motor. Which is used as experimental sounding rocket. This paper mainly focus on fundamentals of rocket casing, solid propellant and grain cross sections. Based on the values and parameters the material are selected accordingly. SRM uses different grain cross sections to analyse higher burning rate (star, circular, double anchor). Design and analysis configuration using CATIA and open rocket software. This paper is manly concerned about to find high burning rate grain cross section.

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