AE 402
Summer 2025 Part of Term S2
(8 week) Jun 16-Aug 7
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.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
38842
|
Online
|
AO
|
ARRANGED
|
n.a.
|
n.a.
|
Panag, H
|
|
|
|
42270
|
Online
|
ONL
|
ARRANGED
|
n.a.
|
n.a.
|
Panag, H
|
|