2017
DOI: 10.11159/ichtd17.105
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Abstract: This contribution presents an approach for a mathematical model which is based on a detailed experimental characterization of a heat transport system as used in common satellite applications. The heat transported is being emitted from the electrical consumers inside the satellite. The present heat transport system consists of two loop heat pipes (LHP), which transport the heat obtained from four arterial heat pipes (AHP) to the heat sink outside the satellite using ammonia as a working fluid. Due to nonconstan… Show more

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