A t-configuration solar cell array applied to microsatellites
A solar cell array and micro-satellite technology, applied in space navigation equipment, space navigation vehicles, transportation and packaging, etc., can solve the problems of low deployment frequency, high price, complex system, etc. Simple and reliable, avoiding the effect of frequency coupling
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[0033] The present invention will be described in detail below with reference to specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that, for those skilled in the art, several changes and improvements can be made without departing from the inventive concept. These all belong to the protection scope of the present invention.
[0034] like figure 1 As shown in the figure, a T-configuration solar cell array applied to a microsatellite comprises: a connecting frame 1, a left panel of the solar cell array 3, a middle panel of the solar cell array 2, a right panel of the solar cell array 4, a hinge 6 between the panels, a root Hinge 5, left panel timing deployment mechanism 7 and right panel timing deployment mechanism 8; the left panel 3 of the solar cell array is connected to the left side of the middle panel 2 of the solar cell array t...
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