16.50 Aerospace Propulsion
Presents aerospace propulsive devices as systems, with functional requirements and engineering and environmental limitations. Requirements and limitations that constrain design choices. Both air-breathing and rocket engines 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 presented.
Lecture occurs 9:30 AM to 11:00 AM on Mondays and Wednesdays in 37-212.
This class counts for a total of 12 credits.
MIT 16.50 Aerospace Propulsion Related Textbooks
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