3units 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): Grade of “C” or better in MATH 31 or MATH 31X,and PHYS 50 with a grade of “C” or better, or graduate standing. Grading: Graded