FIELD: spacecraft equipment.
SUBSTANCE: device is designed to provide heat removal from the spacecraft equipment. The radiator-radiator, which is a panel, consists of a collector with a layer of carbon fiber wound between the heat pipes inserted into it, and a shell of heat-conducting carbon pitch fiber is put on each heat pipe installed in the collector with a coolant flowing through it, to which, through the layer high-temperature compound based on coal tar pitch, a heat-conducting carbon sheet is attached, forming a heat-radiating surface of the radiator-radiator.
EFFECT: mass of the cooler-radiator of the system for ensuring the thermal regime of the spacecraft decreases with an increase in the effective heat release.
2 cl, 1 dwg
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Authors
Dates
2022-11-23—Published
2022-08-04—Filed