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Learning Path
Thermodynamics and Fluid Mechanics Fundamentals → Capstone Propulsion Design Project
This path equips senior aerospace engineering students with the knowledge to design and analyze solid and liquid propellant rocket propulsion systems. It covers fundamental principles, performance metrics, nozzle theory, propellant chemistry, combustion, and system design considerations, culminating in a capstone design project.
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10 learning steps · 3 phases. Click any step to inspect it and see it on the Knowledge Map.