FIELD: space engineering; devices for filling satellite temperature control systems with liquid heat-transfer agents. SUBSTANCE: heat-transfer agent pressurization line of proposed device is additionally provided with capillary evaporator mounted near level of lower part of reservoir. It includes vapor and liquid cavities which are communicated respectively with vapor cushion and lower part of reservoir and are divided by capillary partition to which electric heater is secured on side of vapor cavity. EFFECT: improved quality of filling the temperature control systems with deaerated heat-transfer agent, thus providing for required service life of systems. 2 dwg
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Authors
Dates
2000-01-27—Published
1998-05-18—Filed