Introduction to Propulsion Systems

A white-hot flame surrounded by red hot exhaust shoots out from a J-2X engine gas generator.

A white-hot flame shoots out from a J-2X engine gas generator during a test at NASA's Marshall Space Flight Center. (Image courtesy of NASA/MSFC.)

Instructor(s)

MIT Course Number

16.50

As Taught In

Spring 2012

Level

Undergraduate

Cite This Course

Course Features

Course Description

This course presents aerospace propulsive devices as systems, with functional requirements and engineering and environmental limitations along with requirements and limitations that constrain design choices. Both air-breathing and rocket engines are covered, at a level which enables rational integration of the propulsive system into an overall vehicle design. Mission analysis, fundamental performance relations, and exemplary design solutions are presented.

Martinez-Sanchez, Manuel. 16.50 Introduction to Propulsion Systems, Spring 2012. (MIT OpenCourseWare: Massachusetts Institute of Technology), http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-50-introduction-to-propulsion-systems-spring-2012 (Accessed). License: Creative Commons BY-NC-SA


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