|
Aug 16, 2024
|
|
|
|
AE 242 - Orbital Mechanics and Mission Design 3 units Two-body problem, conic sections, time of flight. Gibb’s method of orbit determination, maneuver analysis for Earth orbiters and interplanetary flight. Euler-Hill equations. Mission design constraints on orbit geometry and launch window analysis.
Prerequisite(s): BSAE or Instructor Consent. Grading: Graded
Class Schedule | Syllabus Information | University Bookstore
Add to Favorites (opens a new window)
|
|