AE 202
Fall 2012 Part of Term 1
Part of Term 1
Aug 27-Dec 12
Aug 27-Dec 12
Credit: 3 hours.
Fundamental principles of aerospace flight mechanics applied to spacecraft and aircraft. Orbital mechanics, rocket propulsion, and dynamics and control applied to spacecraft design. Aerodynamics, maneuvering, stability and flight performance applied to aircraft design. MATLAB examples and assignments.
Prerequisite: Credit or concurrent registration in TAM 212.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
55736
|
Lecture-Discussion
|
A
|
1:00PM
-1:50PM
|
MWF
|
218 Mechanical Engineering Bldg
|
Conway, B
|
|