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Satellite payload thermal analysis
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2 Geometries
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2 Simulation setups
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2 Geometries 0 Meshes 2 Simulation setups 0 ResultsAbout this project
I am evaluating the thermal environment and control strategies for a small satellite operating in Low Earth Orbit (LEO). The payload in the satellite consists of a small camera whose operational temperature is between 20 °C and 25 °C.
