SPACECRAFT THERMAL CONTROL SYSTEM Russian patent published in 2015 - IPC B64G1/50 B64G7/00 

Abstract RU 2541597 C2

FIELD: transport.

SUBSTANCE: invention relates to thermal control systems (TCS) of spacecrafts (SC), predominantly telecommunication satellites. TCS comprises two independent on-board circulation paths identical in composition with heat carrier, which are arranged next to each other in honeycomb panels (or on them). Each one of paths comprises inlet and outlet fluid connectors for connection with fluid connectors of detachable TCS unit. In the latter, liquid-liquid heat exchanger is installed which has cooling capacity exceeding its required value for one path not less than by 2.1-2.2 times. During SC electric testing the detachable unit is connected to one of circulation paths according to SC testing program. At the same time the other path is looped back by liquid path having the same hydraulic resistance as liquid path of detachable unit.

EFFECT: simplification of TCS detachable unit design, reducing its dimensions and mass which simplifies mounting and dismantling detachable unit on SC board.

3 dwg

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RU 2 541 597 C2

Authors

Khalimanovich Vladimir Ivanovich

Golovenkin Evgenij Nikolaevich

Sorokvasha Gennadij Grigor'Evich

Kolesnikov Anatolij Petrovich

Ankudinov Aleksandr Vladimirovich

Akchurin Georgij Vladimirovich

Volovikov Vitalij Gavriilovich

Shilkin Oleg Valentinovich

Akchurin Vladimir Petrovich

Dates

2015-02-20Published

2013-04-16Filed