AEE 3263

Space Flight Mechanics

Florida Institute of Technology · UGRD · Fall 2026

1 section

Catalog description

Provides an understanding of the motion of celestial objects and spacecraft under gravity. Includes analysis of the two-body and restricted three-body problems and orbital transfer using impulsive forces. Also includes designing interplanetary spacecraft trajectories for given specifications. Uses MATLAB for numerical analyses and dynamic simulation. Prerequisite: MEE 2082 and ( MTH 2201 or MTH 3200

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Class #florida_online-0039Fall 2026UGRD3 credits

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