AESP 543

Aerospace Propulsion

University of South Carolina-Columbia · UGRD · Fall 2026

1 section

Catalog description

Propulsion system performance and cycle analysis. Momentum theorem, thrust and propulsive efficiency. Thermodynamics of compressible flow with heat and work addition. Combustion Processes. Components and principles of turbojet, turbofan, ramjet and SCRAM jet engines. Combustors and afterburners. Introduction to rocket engines.

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Class #south_carolina_columbia-AESP543Fall 2026UGRD3 credits

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Instructor: Staff

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