AE 402

Fall 2017 Part of Term 1

Part of Term 1
Aug 28-Dec 13

Orbital Mechanics

SHOW FINAL EXAM SCHEDULE

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.

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AE 402 class schedule data for fall 2017
	CRN	Type	Section	Time	Day	Location	Instructor	Section Details
	29794	Lecture-Discussion	A	12:00PM -12:50PM	MWF	Transportation Building	Prussing, J Conway, B Putnam, Z	Part of Term: 1 Date Range: 08/28/17-12/13/17
	63683	Online	ONL	ARRANGED	n.a.	n.a.	Prussing, J Conway, B Putnam, Z	Part of Term: 1 Date Range: 08/28/17-12/13/17 Section Info: Restricted to online non-degree, online, MSAE, online MSME, online MSCEE and online MCS students. For more details on this course section, please see http://engineering.illinois.edu/online/courses/. Non-Degree students may enroll on a space-available basis with consent of Program Coordinator, Staci Tankersley (tank@illinois.edu). Restriction(s): Restricted to MS: Civil Engr - Online - UIUC, MCS:Computer Sci Online -UIUC, MS:Mechanical Engineerng -UIUC, MS: Aerospace Engr-Online-UIUC, NDEG:Grad Nondegree-CE-UIUC, NDEG:Undergrad Nondeg-CE-UIUC, or MENG:Mech Engineering Onl-UIUC.