FIELD: cosmonautics.
SUBSTANCE: use for orientation of nano- and micro-satellites. Essence of the invention consists in the fact that the nano- and microsatellites orientation system comprises a tubular casing, in which there is a core from a soft magnetic material with a coil wound on it, wherein a tubular structure of external elements is used as a tubular casing, in the inner volume of which there is a core from a magnetically soft material and a coil, and an electric insulator is installed between the coil and inner surfaces of the tubular structure.
EFFECT: increased efficiency of active magnetic orientation system operation due to saving of on-board electric power while maintaining the main functions of the system, as well as increasing the functionality of nano- and microsatellites by freeing up additional space inside them to accommodate other service systems.
1 cl, 2 dwg
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Authors
Dates
2024-07-31—Published
2023-11-21—Filed