APPARATUS FOR COOLING COMPONENTS IN SPACECRAFT

The invention relates to an apparatus for cooling components in spacecraft, comprising a heat radiator (5) and a heat conductor (3; 3a, 3b). A versatile applicability is achieved in such a way that the heat conductor (3, 3a, 3b) penetrates an outside wall (1) of the spacecraft and is provided in the...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZHARKOV, JAROSLAV, LESHCHENKO, VOLODYMYR, KORPAN, NIKOLAI
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION HEAT EXCHANGE IN GENERAL HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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