Orbital Mechanics

AER E 551 XE


Course Description

Review of 2-body problem. Orbital maneuvers. Relative motion in orbit. Orbit perturbation analysis. Gravity field expansions and effects on orbiters. 3-body problem with applications.

3 credits

Questions

Instructor Contact

Ossama Omark Abdelkhalik

Registration Information

Course Dept
AER E
Course Number
551
Section
XE
Credit Hours
3
Semester
Fall 2018
Dates
Aug 20 - Dec 14
Prerequisites
AER E 351
Delivery Fee
$570.00 *
* Delivery Fee is additional to Tuition & Fees.

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