Issue |
E3S Web Conf.
Volume 477, 2024
International Conference on Smart Technologies and Applied Research (STAR'2023)
|
|
---|---|---|
Article Number | 00020 | |
Number of page(s) | 11 | |
DOI | https://doi.org/10.1051/e3sconf/202447700020 | |
Published online | 16 January 2024 |
Thermal Analysis of AlainSat-1: A 3U Cubesat for Earth Observation
1 Department of Mechanical and Aerospace Engineering, College of Engineering, United Arab Emirates University, Al-Ain, United Arab Emirates.
2 Department of Electrical Engineering, College of Engineering, United Arab Emirates University, Al-Ain, United Arab Emirates.
3 National Space Science and Technology Center, United Arab Emirates University, Al-Ain, Unite Arab Emirates.
* Corresponding author: samrajgopal@outlook.com
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.
© The Authors, published by EDP Sciences, 2024
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.