| 摘要 |
FIELD: astronautics.SUBSTANCE: invention relates to space engineering and may be used to provide power to spacecraft (SC) and stations. Power supply system is intended for use on spacecraft and stations in a space environment. In present invention into existing fluid temperature control system comprising a housing within which is located cooling circuit and heating, consisting of series-connected heat exchanger to reservoir coolant, having a control valve, radiator etching valve magneto-hydrodynamic pump for circulating coolant in kennel, after heat exchanger is introduced turbine connected to an electric generator, via a control system which is connected to battery and load.EFFECT: use of thermal control system for obtaining additional energy.1 cl, 1 dwg |
