THERMAL CONDITIONS CONTROL SYSTEM Russian patent published in 2000 - IPC

FIELD: space engineering; thermal conditions control systems of communication satellites. SUBSTANCE: proposed system includes heat-transfer agent liquid loop. Heater is mounted immediately before inlet of heat-transfer agent temperature regulator. Section of liquid between its outlet and regulator inlet is connected by means of bypass line with section of liquid passage between first outlet of temperature regulator and inlet of cooler. Bypass line includes adjustable throttle valve; inlet and outlet of liquid loop are connected together via valve. Flexible pipe lines connected to inlet and outlet of this loop are provided with hydraulic connectors at their ends. Inlet and outlet pipe lines are passed through additional cover at end sections. EFFECT: facilitated adjustment of system; improved service characteristics of system due to enhanced accuracy of maintenance of temperature at satellite inlet. 4 cl, 9 dwg