AE 402
Fall 2009 All Classes
All Classes
Credit: 3 OR 4 hours.
Analysis of orbits in an inverse-square gravitational field; elementary rocket dynamics, impulsive orbit transfer and rendezvous, and Lambert's Theorem with applications; patched-conic trajectories, planetary gravity-assist maneuvers, and linearized orbit theory with application to simplified analytical models; perturbations.
3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 302.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
29794
|
Lecture-Discussion
|
A
|
11:00AM
-11:50AM
|
MWF
|
Engineering Hall
|
Conway, B
|
|