Design and development of HSU-SAT 1 structural system

Abstract

The first HSU-SAT is a 1U size Cubesat. In this paper, we designed and developed a satellite structure using Autodesk Inventor to develop the thermal structure of HSU-SAT1. In addition, structural analysis and thermal analysis of the satellite were performed using Excel and Autodesk Nastran in cad. We verified whether the satellite can withstand the launch environment and whether the onboard equipment is within the allowable temperature range.