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- W2016246635 abstract "In this paper thermal simulation of a satellite borne electric box is introduced. Structure was simplified and a finite element model was built. The analysis results showed that the temperature scopes of the box and the component cases are from 45°C to 67.3°C and all of junction temperatures of the components are lower than the derated maximum junction temperatures themselves and leave enough design margins, which match the requirements of thermal analysis." @default.
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- W2016246635 date "2014-11-01" @default.
- W2016246635 modified "2023-10-18" @default.
- W2016246635 title "Thermal Simulation of an Electric Box" @default.
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- W2016246635 doi "https://doi.org/10.4028/www.scientific.net/amm.687-691.597" @default.
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