MAE 5510

MAE 5510

Course information provided by the 2026-2027 Catalog.

Introduction to air and rocket propulsion. Emphasis on air-breathing gas-turbines. Chemical rocket propulsion. Brief discussion of of ramjets and of propellers. Application of thermodynamic and fluid-mechanical principles to analysis of performance and design, including fuel efficiency and environmental impacts.


Prerequisites background equivalent to: ENGRD 2210 or MAE 2210; MAE 3230.

Enrollment Information Recommended prerequisites: MAE 3050.

Last 4 Terms Offered 2026SP, 2025SP, 2024SP, 2023SP

Learning Outcomes

  • Students will be able to describe and interpret the types, characteristics, and performance measures of combustion engines used in propulsion, power generation, and road vehicles.
  • Students will be able to apply thermodynamic and fluid mechanical principles to quantitatively describe engine operation.
  • Students will be able to predict how their performance depends on design parameters and operating conditions.

View Enrollment Information

Syllabi: none
  •   Regular Academic Session.  Combined with: MAE 4510

  • 4 Credits Graded

  • 11493 MAE 5510   LEC 001

    • MWF
    • Jan 25 - May 11, 2027
    • Staff

  • Instruction Mode: In Person