Prerequisites: ME 370 and ME 390, or equivalent background. Flight environment. Mission propulsive requirements, staging and optimization. Chemical rockets. Thrust chamber design, nozzle design, propellant storage and pressurization systems. Liquid propellant combustion and expansion; monopropellant systems. Solid propellant grain design. Combustion instabilities. Multiple phase, reacting nozzle flow. Ram/rocket hybrid engines. Energy limited vs. power limited systems. Introduction to electrical rocket propulsion.

Fall-2022 - Schedule of Classes

AE 572

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