Pioneering rocket design for future space expedition

The paper presents a design conceptualization of a supply rocket intended for low-Earth orbit missions using state-of-the-art systems integration concepts, material sciences, and aeronautical engineering. Maximizing the optimization of rocket design along with hassle-free payload integration is the main aim of the work. The study compares two supply rocket designs, namely MSHS-11 and SHNK-24, concerning material selection, structural design, the choice of the propulsion system, and aerodynamic analysis. This research will be the pathway to innovative space exploration by developing cost-effective rockets that have improved aerodynamics and stability through optimized propulsion systems, focusing on sustainability, smart engineering and low cost.