AESP 420 - Flight and Orbital Mechanics

Institution:

University of South Carolina-Columbia

Subject:

Description:

Derivation of the general equations of motion (EoM) for aircraft and space flight. Solution of Aircraft EoM for cruise flight and flight maneuvers including coordinated turns, takeoff and landing. Solution of EoM for orbital mechanics problems including transfer trajectories. Calculation of required specific impulses. Design of interplanetary trajectories. Prerequisite: D or better in EMCH 310 or ENCP 210. FS: 02/02/2022.

Credits:

3.00

Credit Hours:

Prerequisites:

Corequisites:

Exclusions:

Level:

Instructional Type:

Lecture

Notes:

Additional Information:

Historical Version(s):

Institution Website:

www.sc.edu/

Phone Number:

(803) 777-7000

Regional Accreditation:

Southern Association of Colleges and Schools

Calendar System:

Semester

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