Apparatus for cooling components in spacecraft

摘要

The invention relates to an apparatus for cooling components in spacecraft, comprising a heat radiator ( 5 ) and a heat conductor ( 3; 3 a, 3 b). A versatile applicability is achieved in such a way that the heat conductor ( 3, 3 a, 3 b) penetrates an outside wall ( 1 ) of the spacecraft and is provided in the interior of the spacecraft with several coupling places ( 8 ) for components to be cooled ( 20 ) and/or for other heat conductors ( 10 ).