Commenced in January 2007
Paper Count: 30840
Satellite Thermal Control: Cooling by a Diphasic Loop
Abstract:In space during functioning, a satellite will be heated up due to the behavior of its components such as power electronics. In order to prevent problems in the satellite, this heat has to be released in space thanks to the cooling system. This system consists of a loop heat pipe (LHP), in which a fluid streams through an evaporator and a condenser. In the evaporator, the fluid captures the heat from the satellite and evaporates. Then it flows to the condenser where it releases the heat and it condenses. In this project, the two mains parts of a cooling system are studied: the evaporator and the condenser. The study of the diphasic loop was done starting from digital simulations carried out under Matlab and Femlab.
Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1335424Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 1682
 Chanwoo Park, Aparna Vallury, Jon Zuo, Jeffrey Perez, and Paul Rogers, Thermal Spacecraft Management using Advanced Hybrid Two- Phase Technology Loop, in Proc. AIP Conf. vol 880, pp. 11-18, January 2007
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