A radiator (1) comprises at least one heat conductive layer (2) having an in-plane heat conductivity of at least 500 W/mK and at least one heat emission layer (3) in contact with the heat conductive layer, wherein the emission layer has an exposed surface with an emissivity of at least 0,7. Preferably, the heat conductive layer comprises pyrolytic graphite material. The radiator is to be used in combination with a space vehicle structure, and due to its flexible character may be conformed to the particular shapes of such structure (18).
Radiator, as well as space vehicle structure comprising such a radiator
Kühler, sowie Raumfahrzeugsstruktur mit solch einem Kühler
Radiateur, ainsi qu'une structure de véhicule spatial comprenant ce radiateur
2017-08-02
Patent
Elektronische Ressource
Englisch
IPC: | F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION / B64G Raumfahrt , COSMONAUTICS / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT / H05K PRINTED CIRCUITS , Gedruckte Schaltungen |
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