Satellite assembly composed of solar panel and antenna and satellite
A technology for solar panels and antenna elements, applied in the field of satellite components and satellites, can solve the problems of high energy consumption and the reduction of the rigidity of the overall structure of the satellite platform, and achieve the effect of alleviating the reduction in the rigidity of the overall structure
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[0023] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.
[0024] see figure 1 , the embodiment of the present invention provides a satellite assembly 10 composed of a solar panel and an antenna, and the term "satellite assembly" here should be understood as an assembly for satellites. The satellite assembly 10 may include: a sheet-shaped solar panel unit 11 connected to the main body 20 of the satellite 1, as shown in figure 1 Schematically shown by an unfilled plate-shaped block in the figure 2 Schematically shown by grey-filled flat-shaped blocks. Here, "slab-like" means that the solar panel element 11 and the antenna element 12 extend in a two-dimensional plane, as in figure 1 is specifically shown in extending in a two-dimensional plane, but can also represent figure 1 What is not shown in extends in a two-dimension...
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