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Utah State University

Aug 21, 2017

2017-2018 Academic Year

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2017-2018 Academic Year

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MAE 6530 - Propulsion Systems

3 credits

Fundamentals of turbine and rocket propulsion, including nozzle theory and thermodynamic relations, combustion processes, and flight performance. Rocket propulsion topics, including solid, liquid, and hybrid rocket engines; and advanced engine concepts. Turbine engine propulsion systems, including turbojets, turbofans, afterburners, and advanced unducted fan concepts.

Prerequisite/Restriction: MAE 5420

Semester(s) Traditionally Offered: Spring

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UTAH STATE UNIVERSITY

MAE 6530 - Propulsion Systems