Instructors:

Dr. Richard Eastes

(reastes@mail.ucf.edu)
Course Description: Orbital trajectory design; analysis of vehicle sustained g-forces; vehicle vibration analysis; orbital maneuvering; atmospheric re entery; lunch windows; rocket apogee and down range computations; wind corrections and lunch anagles.
Credit Hours: 3
Course Prerequisites: PHY 2053C, Calculus I, II, CAD.

Course Objectives:

 

 

 
Course links:
Class Schedule:
Tuesday and Thursday
15:00-16:15
ES1B KSC