In this module students will learn about spacecraft design and development. The course will cover typical mission requirements, such as payload and orbit and how these determine choices for the main spacecraft sub-systems and overall spacecraft design.
Learning Outcomes
By the end of the module students should be able to:
Be able to apply a systems engineering approach to spacecraft design
Design mission-specific components; specifying their materials and construction
Explain how space missions are designed given a set of requirements
Describe the main elements of a spacecraft (payload and bus)
These link to AHEP v4 learning outcomes:
Apply knowledge of mathematics, statistics, natural science and engineering principles to the solution of complex problems. Some of the knowledge will be at the forefront of the particular subject of study (C1)
Analyse complex problems to reach substantiated conclusions using first principles of mathematics, statistics, natural science and engineering principles (C2)
Apply an integrated or systems approach to the solution of complex problems (C6/M6)
Use a risk management process to identify, evaluate and mitigate risks (the effects of uncertainty) associated with a particular project or activity (C9/M9)
Adopt a holistic and proportionate approach to the mitigation of security risks (C10/M10)
Use practical laboratory and workshop skills to investigate complex problems (C12/M12)
Select and apply appropriate materials, equipment, engineering technologies and processes, recognising their limitations (C13/M13)
Apply a comprehensive knowledge of mathematics, statistics, natural science and engineering principles to the solution of complex problems. Much of the knowledge will be at the forefront of the particular subject of study and informed by a critical awareness of new developments and the wider context of engineering (M1)