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Thermal control: Case study of 3U CubeSat
In this paper, we present a thermal analysis of university 3U CubeSat in critical cases of orbit using the software COMSOL Multiphysics. First, the thermal environment and thermal modelling are presented in order to describe the method, the equations and the assumptions used by the numerical software to model the behaviour of temperature in each node of the nanosatellite. Second, an overview of the satellite is given to describe the design of the CubeSat, the mission and to fix the assumptions and boundary conditions. Finally, the results, based on the software, are presented for the two cases with and without a thermal control. The analysis has been used to validate the importance of the passive thermal control techniques.
Thermal control: Case study of 3U CubeSat
In this paper, we present a thermal analysis of university 3U CubeSat in critical cases of orbit using the software COMSOL Multiphysics. First, the thermal environment and thermal modelling are presented in order to describe the method, the equations and the assumptions used by the numerical software to model the behaviour of temperature in each node of the nanosatellite. Second, an overview of the satellite is given to describe the design of the CubeSat, the mission and to fix the assumptions and boundary conditions. Finally, the results, based on the software, are presented for the two cases with and without a thermal control. The analysis has been used to validate the importance of the passive thermal control techniques.
Thermal control: Case study of 3U CubeSat
Narimane, Blanchete (author) / Bah, Abdellah (author)
2023-02-20
1718852 byte
Conference paper
Electronic Resource
English
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