In this module students will be introduced to the means by which power is generated and distributed, and propulsion is used for manoeuvre control, in space applications. Examples include chemical and ion engines, nuclear sources, and solar cells and sails. Power distribution mechanisms and attitude and orientation control will be scrutinised. Students will choose a set of mission objectives and design appropriate power and propulsion systems to meet those objectives in a mini-project.
Learning Outcomes
By the end of the module students should be able to:
Demonstrate a comprehensive knowledge of the scientific and engineering principles by which key spacecraft power and propulsion subsystems and elements operate, including new technologies and drawing links to analogous terrestrial applications (M1).
Undertake calculations to evaluate the performance of spacecraft propulsion and power subsystems, making relevant and justified assumptions where information is uncertain or incomplete, and critiquing the methods used and answers obtained (M1, M2, M3).
Design power or propulsion subsystem architectures to meet a set of mission objectives, demonstrating a critical awareness of novel or emerging technology (M1).
Justify and critique the proposed architecture design with reference to the supporting analysis and modelling used to support this, specifically in uncertain or incomplete information (M2, M3).