ME-4234: Aerospace Propulsion Systems
Description: Design principles and performance analysis of atmospheric and space propulsion engines and systems. Application of thermodynamics, compressible fluid flow and combustion fundamentals to the design of gas turbine and rocket engines and components, including inlets, turbomachines, combustors, and nozzles. Matching of propulsion system to vehicle requirements. Must have a C- or better in pre-requisites ME 3404 and ME 3124 or AOE 3114 and AOE 3134.
Pathways: N/A
Course Hours: 3 credits
Sections Taught: 5
Average GPA: 2.82 (rounds to B-)
Strict A Rate (No A-) : 34.76%
Average Withdrawal Rate: 26.23%
| Gregory Young | 2024 | 11.9% | 20.3% | 15.6% | 5.4% | 7.8% | 39.0% | 2.38 | 3 |
| Kevin T Lowe | 2020 | 69.0% | 8.3% | 7.2% | 4.2% | 4.2% | 7.1% | 3.49 | 2 |