Spaceflight thermal control system enhanced condensing device based on space dot-matrix foam metal

The invention relates to a spaceflight thermal control system enhanced condensation device based on space dot-matrix foam metal. The spaceflight thermal control system enhanced condensation device comprises a shell, condensation heat exchange pipes and the foam metal. Water circulates in the condens...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CHANG JINGYI, CHEN ZHENQIAN, XU BO, SHI JUAN
Format: Patent
Sprache:chi ; eng
Schlagworte:
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