2010-2011 Catalog 
    
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2010-2011 Catalog [ARCHIVED CATALOG]

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MAE 5391 - Rocket Propulsion

3 Credits (Minimum) 3 Credits (Maximum)
Basic theory of rocket propulsion, nozzle performance, propellant characteristics. Primary emphasis on the engine system design process, based on mission requirements. Chemical, as well as nuclear, electric, and advanced propulsion concepts are treated. Prer., MATH 3400 and MAE 2301. Meets with MAE 4316.


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