3 credits
Spring 2026 Lecture Distance Learning Upper Division
Survey of air-breathing and rocket propulsion systems for AAE students not in the propulsion option. Thermodynamic cycles, analysis of air-breathing systems and components. Rocket Equation, rocket cycles, liquid and solid propellants, chemical equilibrium.
Learning Outcomes1Knowledge of propulsion applications that use gas turbine engines and rockets.
2Understanding of the Brayton cycle and ability to calculate enthalpy and work balance.
3Ability to solve mass, momentum, and energy balances using a control volume approach.
4Ability to perform top-level performance and sizing calculations of gas turbine engines.
5Ability to apply Euler's work equation to compressors and turbines to calculate work.
6Ability to use the Rocket Equation to calculate impulse requirements and size rocket thrusters.
Prerequisites
made by Purdue students.