AE 202
Fall 2011 All Classes
All Classes
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
|
Engineering Hall
|
Chung, S
|
|