This structural component is a mounting bracket for solar panel actuators, part of the NeoSAT platform. The conventionally manufactured assembly consists of five individual parts (milled and bent sheet metal components). The aim is to evaluate the use of additive manufacturing (3D printing) and test it using functional prototypes to save weight and minimize assembly and storage costs. It is essential that the 3D-printed version also passes all required tests for component qualification in the aerospace industry. The 3D-printed version must also pass all necessary tests for component qualification in the aerospace industry.
Completion of component manufacturing and start of preparation for the testing phase
Completion of all necessary preparations for the testing phase
Project completion