One of the most important parameters in the dimensioning stages of communication satellites is the calculation of the areas where the heat to be released into space is located. The satellite thermal control system calculates these areas. Thermal analyses are performed for the north and south panels where the payload equipment is located in three-axis geostationary satellites. It is important to calculate these areas where the heat to be released into space is located correctly. In this study, thermal analysis calculations were performed for a three-axis geostationary satellite with an area of 1 to 10 m2. In the calculations, the absorptance of external surfaces at the end of the satellite's life was calculated by considering 0.27. The radiator area temperature was taken as 30 oC in the calculations.
Primary Language | English |
---|---|
Subjects | Energy |
Journal Section | Research Article |
Authors | |
Publication Date | January 17, 2025 |
Submission Date | November 12, 2024 |
Acceptance Date | January 13, 2025 |
Published in Issue | Year 2024 Volume: 1 Issue: 2 |
This journal is licensed under Creative Commons Attribution-NonCommercial 4.0 International License.