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Cedarville University · 3 credits

This course introduces each type of propulsion system that is commonly used in modern aerospace vehicles: e.g., rockets, piston aero engines, gas turbine engines, ramjets, and scramjets. This course presents a balance of theory, fundamental performance analysis, and design. Engineering principles and functionality mechanisms are used in assignments, including a group design project, requiring students to analyze the performance of each type of these propulsion systems. Prerequisites: EGME-3110 Thermodynamics; EGME-3210 Fluid Mechanics. (odd years)
Fall 2026 · 1 section
Aug 19 – Dec 11
| Section | Days & time | Location | Instructor |
|---|---|---|---|
| 01Class #156429 | Tu Th · 2:00 – 3:15 PM | Engineering and Science Ctr 342 | Dr. Joseph D. Miller |