AE 402
Fall 2018 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 202.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
29794
|
Lecture-Discussion
|
A
|
2:00PM
-3:15PM
|
TR
|
103 Transportation Building
|
Conway, B
|
|
|
|
63683
|
Online
|
ONL
|
ARRANGED
|
n.a.
|
n.a.
|
Conway, B
|
|