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This study evaluates propulsion options for attitude control in spacecraft, focusing on two primary systems: pressure regulated tanks and blowdown tanks. It analyzes their performance, efficiency, and operational characteristics in various mission scenarios. The findings aim to assist engineers and decision-makers in selecting optimal tank pressurization methods, balancing factors such as reliability, complexity, and responsiveness. This research contributes to advancing spacecraft attitude control systems, ensuring precise maneuverability in space.
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