The principles and processes:

High performance satellite and launcher structures - Stiffness and mass performance are key Primary and secondary structures Integrated radiator functionalities Launch vehicle adapters (LVA) Manned space applications (ISS, Orion, Lunar Gateway) - fracture control and human factors design to be considered Primary and secondary structures Internal and exernal structures Rack structures Optical Payload structures and their sub-assemblies - dimensional stability is the main priority Telescope structures Optical benches Bipods / Hexpods Straylight baffles Electronic Equipment structures - good balance between structural and thermal performance required Power supply, control and distribution units (PSU/PCU/PDU) Data handling/processing units (DHU/DPU) Batteries Mechanical Ground Support Equipment (MGSE) - safety and cost drive the design Transport containers Lifting devices Multi-purpose trolleys and turning devices Integration stands, installation platforms and panel supports