0304-683 - Orbital Mechanics-Mission to Mars

Institution:

Rochester Institute of Technology

Subject:

Description:

This course introduces orbital mechanics and space fl ight dynamics theory with application for Earth, lunar, and planetary orbiting spacecraft. Content includes historical background and equations of motion, two-body orbital mechanics, orbit determination, orbit prediction, orbital maneuvers, lunar and interplanetary trajectories, orbital rendezvous and space navigation (time permitting). The two body orbital mechanics problem, fi rst approximation to all exploration orbits or trajectories, is covered with an introduction to the three body problem. Students develop computer based simulations of orbital mechanics problems including a fi nal mission project simulation from Earth to Mars and home again requiring a number of orbit phases and transfers between these phases. (registration preference is given to students enrolled in the aerospace option) Class 4, Credit 4

Credits:

4.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.rit.edu/

Phone Number:

(585) 475-2411

Regional Accreditation:

Middle States Association of Colleges and Schools

Calendar System:

Quarter

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