Classical orbital mechanics and dynamics of spacecraft. Application of this knowledge in mission design for achieving pre-specified objectives and adequate spacecraft pointing. Examples of past missions.
Systems engineering for aerospace systems design. Current practice and standard methods to reach a preliminary design review stage are taught, encompassing requirements translation, functional analysis, budgeting, and stakeholder engagement (including Mātauranga Māori perspectives). Overview of major aircraft and satellite subsystems (such as structure, propulsion, aerodynamics), initial vehicle sizing, and the impact of the operational environment on these vehicles.
Overview of the main issues to be addressed during the structural design process of aircraft and spacecraft, including space mechanisms. Includes requirements definition, analysis processes, materials selection, manufacturing, and typical aircraft and spacecraft configurations.