FIELD: space technology; spacecraft.
SUBSTANCE: invention relates to the field of space technology, and more specifically to spacecraft (SC). The spacecraft contains a thermal control system with devices for the selection, supply and discharge of heat. In addition, the spacecraft includes a power supply system with solar batteries, an automation and voltage stabilization complex, and storage batteries. There is an onboard control complex with an onboard computer. A microturbine is inserted between the heat supply devices and the heat release devices of the thermal control system. An electric generator is connected to it, the output terminals of which are connected with a cable to the automation and voltage stabilization complex of the power supply system.
EFFECT: mass of the spacecraft is reduced.
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---|---|---|---|
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Authors
Dates
2021-06-21—Published
2020-05-13—Filed