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• W3149624804 abstract "Thermal control is a key factor in protecting the low earth orbit satellites from the severe space environment and thermal uncertainties throughout their lifetime. However, the exact effects of temperature and temperature change on satellite reliability are still unclear. This paper provides a comprehensive satellite thermal failure analysis model to simulate the thermal environment and calculate the satellite temperature. Combining the model with fuzzy inference, the relationship between temperature and thermal failure probability can be analyzed. Calculation results reveal that high duty cycles of the internal heat flux will increase the failure probability of all satellite components. Subsequently, numeric simulations are performed to examine the effect of absorptivity and emissivity of shell material on the thermal failure probability in different parts of the satellite. It is also verified that the adoption of special aerospace material with low absorptivity and high emissivity, such as Teflon, will significantly decrease the failure probability and prolong its lifetime. These findings are helpful in designing the reliable thermal control subsystem of low earth orbit satellites." @default.
• W3149624804 created "2021-04-13" @default.
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• W3149624804 date "2021-03-26" @default.
• W3149624804 modified "2023-10-02" @default.
• W3149624804 title "Fuzzy-based analysis of thermal effects on component failure for LEO satellites" @default.
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• W3149624804 doi "https://doi.org/10.1109/icbaie52039.2021.9389885" @default.
• W3149624804 hasPublicationYear "2021" @default.
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