Apparatus for cooling components in spacecraft
a, ba, bThe invention relates to an apparatus for cooling components in spacecraft, comprising a heat radiator and a heat conductor. A versatile applicability is achieved in such a way that the heat conductor penetrates an outside wall of the spacecraft and is provided in the interior of the spacecr...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | a, ba, bThe invention relates to an apparatus for cooling components in spacecraft, comprising a heat radiator and a heat conductor. A versatile applicability is achieved in such a way that the heat conductor penetrates an outside wall of the spacecraft and is provided in the interior of the spacecraft with several coupling places for components to be cooled and/or for other heat conductors. |
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