AE 165 - Aerospace Flight Mechanics

3 units
Trajectory dynamics of atmospheric flight (aircraft and missiles) and spaceflight (orbital mechanics). Influence of vehicle design on trajectory. Aircraft static performance, stability and control. Rocket launch and re-entry dynamics. Computer simulations.

Prerequisite(s): C or better in (MATH 31 or MATH 31X) and PHYS 50, or graduate standing.
Grading: Letter Graded

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