16.82 Flight Vehicle Engineering
Design of an atmospheric flight vehicle to satisfy stated performance, stability, and control requirements. Emphasizes individual initiative, application of fundamental principles, and the compromises inherent in the engineering design process. Includes instruction and practice in written and oral communication, through team presentations and a written final report. Offered alternate Spring and Fall terms.
This class has no prerequisites.
Lecture occurs 2:00 PM to 5:00 PM on Mondays and Wednesdays in 33-419.
This class counts for a total of 12 credits. This class counts as a CI-M.
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