A radiator comprises at least one heat conductive layer having an in-plane heat conductivity of at least 500 W/mK and at least one heat emission layer 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.
RADIATOR, AS WELL AS SPACE VEHICLE STRUCTURE COMPRISING SUCH RADIATOR
15.09.2016
Patent
Elektronische Ressource
Englisch
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