A device for the recovery of a proportion of the energy which is dissipated, by the Joule effect, by the equipment of a predetermined satellite in a vacuum atmosphere, includes at least one radiative panel (10) which is designed to permit the cooling of the satellite (20) payload, and a thermoelectric generator, the heat source (12) of which is supplied with infrared photons by the radiative panels (10), whereby the latter are configured to concentrate the infrared photons towards the heat source (12).
Dispositif de récupération d'énergie thermique dissipée par un satellite placé dans le vide
Device for recovering thermal energy dissipated by a satellite placed in a vacuum
Vorrichtung zur Rückgewinnung von Wärmeenergie, die von einem im Vakuum befindlichen Satelliten abgegeben wird
2017-12-06
Patent
Electronic Resource
French
Navire pourvu de moyens de récupération d'énergie thermique
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