A solar wing layout structure of a high-precision spacecraft
A layout structure and spacecraft technology, applied in the field of spacecraft, can solve problems such as reducing the attitude stability of the spacecraft platform, reducing the attitude stability of the platform, and thermal flutter of the solar wing, so as to achieve simple configuration, improve attitude stability, Reduce the effect of micro-vibration
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[0014] The present invention will be described in detail below in conjunction with 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 those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.
[0015] Such as Figure 1-3 As shown, the embodiment of the present invention provides a solar wing layout structure of a high-precision spacecraft, including a top solar wing main board 1, a top solar wing side plate 2, a payload 3, a spacecraft platform 4, a bottom solar wing 5, The platform top plate 6, the platform side plate 7, the platform bottom plate 8, the top solar wing pressing rod 9 and the bottom solar wing pressing rod 10; the top solar wing main board 1 and the top solar wing side pl...
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