The magnetic torquer creates a magnetic moment to control the satellite attitude by interfacing with the magnetic field of the earth. The product designed interiorly with soft magnetic materials and enameled copper wires of a high reliability and exteriorly carbon fibers of high rigidity, has already been applied and verified to many of the in-orbit satellites of Jilin-1 series.
|Rated output magnetic moment||15Am²|
|Remnant magnetic moment||≤0.1Am²|
|Environment suitability||Temperature: -10℃～+45℃|
|External envelope dimension||280mm×56mm×53.5mm|
|Designed lifecycle||15 Years|
|Delivery cycle||3 Months|
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