AE 165 - Aerospace Flight Mechanics 3 unit(s) 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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