Thermal Analysis of AlainSat-1: A 3U Cubesat for Earth Observation

Abstract

AlainSat-1 is a remote sensing CubeSat carrying earth observation payloads developed by student teams from three international universities. Planned for launch in 2023 it is a direct result from the collaborative effort between the IEEE Geoscience and Remote Sensing Society (GRSS) and the National Space Science and Technology Center (NSSTC) at UAE University. CubeSats are popular among the research and academic communities as a space platform from which to perform related research and academic work connected to space technologies due to their compact size, shorter development time, and relatively low cost. However, because most CubeSats are built using off-the-shelf components, their capacity to resist the harsh environments of space must be proven. Aside from ensuring that structural criteria are met, thermal analysis is critical for ensuring that components or payloads stay functioning in extreme hot or cold environments. The thermal analysis results of AlainSat-1’s finite element model (FEM) functioning under the projected thermal environment associated to its mission are presented in this study. Preliminary results from the analysis using SIEMENS NX show that temperature measurements are within an acceptable range. However, more modification of the simulated environment and FEM in terms of mesh sizes and radiative and conductive thermal couplings is needed before conclusive results may be obtained. The approved simulated results and parameters will be tested experimentally in a Thermal Vacuum Chamber. In addition, challenges identified throughout the analysis and their remedies are discussed.