A cube satellite unit rapidly assembled by plug-and-pull

The invention discloses a cube satellite unit rapidly assembled by plug-and-pull, which includes a number of cube satellite frames, a cube satellite cover and male joints, in which the cube satelliteframe is made up of 12 edges of 10 cm in length, a female interface is arranged on each side, a cube...

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Bibliographic Details
Main Authors DENG YAOSHENG, LUO DAQIAN, LI HAORUI, ZHOU JUN, ZHANG JIAOLONG, JIA FEIRAN
Format Patent
LanguageChinese
English
Published 28.12.2018
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Summary:The invention discloses a cube satellite unit rapidly assembled by plug-and-pull, which includes a number of cube satellite frames, a cube satellite cover and male joints, in which the cube satelliteframe is made up of 12 edges of 10 cm in length, a female interface is arranged on each side, a cube satellite cover plate is arranged on six sides of the cube satellite frame, a male joint is arranged separately, the structure of the two ends is adapted to the structure of the cube satellite frame female interface and can be repeatedly inserted and pulled out with the female interface, and the adjacent cube satellite frame is connected and fixed through the male joint. The invention has the advantages that: (1) the size of the female interface is small, there is no protruding part, the payload and the space of the cube satellite are not occupied, and the original basic attributes of the cube satellite are retained; the male connector has the characteristics of simple structure, small size, light weight, standardi
Bibliography:Application Number: CN201810966171