Design and Analysis of Magnetoplasma Dynamic Thruster for Enhancing Propulsion in Space Craft
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Abstract
This report presents a detailed study of the performance analysis of the advanced propulsion technology in Magneto Plasma Dynamic (MPD) thruster designed for high performance space applications The MPD thruster uses electromagnetic force to accelerate ionized plasma, where the higher the specific impulse, The analysis of reduced propellant mass determines design criteria, including thruster geometry, magnetic field design, and power delivery parameters. Analysed results are shown, which explains the performance parameters of the thruster, such as thrust output, efficiency, and stable operation under different conditions
In addition, the report discusses the implications of MPD technology for the future of space missions, including deep space exploration and satellite operations, and highlights its potential to reduce logistics constraints and enable missions capabilities have advanced Conclusion MPD as a viable solution for next generation propulsion Underline the need for continued research and development in thruster technology Not only does this work contribute to a fundamental understanding of plasma energy not only in terms of electricity but also paving the way for new applications in aerospace engineering and enabling interest It is possible. Experimental results demonstrate the efficiency of the automated system under various conditions and demonstrate improvements in performance and stability compared to manually operated systems.