*483. Space Flight and Orbital Mechanics (3)
- Prerequisites: MATH 370A, MAE 371.
- Two-body problem. Predicting orbital positions. Kepler’s equation. Orbital elements. Lambert’s problem. Rocket dynamics. Rocket payloads and staging. Impulsive orbital transfer. Interplanetary mission analysis. Projects are assigned and written reports are required.
- (Lecture-problems 3 hours). Letter grade only (A-F).
Course Outline
Class Schedules
View the current course offerings:
Mechanical Engineering (MAE)
Engineering Technology (ET)
Engineering (ENGR)
Official Program Information
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year you enter(ed) the program.