Spacecraft and Satellite Design (AERO5760)
UNIT OF STUDY
This course aims to introduce the students to the engineering aspects of spacecraft and mission design, covering the space environment and spacecraft sub-systems, including thermal control, power systems, attitude decision and control system, tracking, telemetry & telecommand, and on-board data handling.
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Further unit of study information
2 hours of lectures and 3 hours of project work in class per week.
Through semester assessment (100%)
Faculty/department permission required?
Study this unit outside a degree
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