Course Detail
Units:
3.0
Course Components:
Lecture
Enrollment Information
Enrollment Requirement:
Prerequisites: Graduate Status in Mechanical Engineering OR Instructor Consent.
Description
Meets with ME EN 5830. Analysis and design of propulsion systems for aerospace vehicles: solid and liquid chemical rocket systems, nuclear rocket engines, electrical rocket engines, nozzle theory, jet engine component analysis, turboprop engines, turbojet engines, ramjet engines, and turbofan engines. See ME EN 5830 prerequisites for expected undergraduate coursework.