Stationary orbit ultra-large type assembling satellite platform configuration and assembling method

A satellite platform and geostationary orbit technology, applied in the satellite field, can solve problems such as modular design of super-large satellite platforms that have not yet been involved in high-orbit, and achieve the effects of facilitating on-orbit maintenance and attitude control, good lighting conditions, and reducing development costs.

Inactive Publication Date: 2020-08-25
SHANGHAI SATELLITE ENG INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

At present, these domestic studies have not yet involved the modular design and on-orbit assembly of high-orbit ultra-large satellite platforms.

Method used

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  • Stationary orbit ultra-large type assembling satellite platform configuration and assembling method
  • Stationary orbit ultra-large type assembling satellite platform configuration and assembling method
  • Stationary orbit ultra-large type assembling satellite platform configuration and assembling method

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Embodiment Construction

[0035]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 changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0036] Such as Figure 1~6 The purpose of the present invention is to provide a geostationary orbit ultra-large assembling satellite platform configuration, including: a mother platform 1, the mother platform 1 comprehensively manages and controls the entire satellite; the first module module 2 and the second module cabin 7, the first module cabin 2 and the second module cabin 7 are connected with the mother platform 1, and provide an installation platform for the super-large platform stand-alone module;...

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Abstract

The invention provides a stationary orbit ultra-large type assembling satellite platform configuration. The configuration comprises a mother platform, a first module cabin, a second module cabin, a first functional cabin, a second functional cabin, a first connecting truss, a second connecting truss, a first energy module, a second energy module, a first mechanical arm and a second mechanical arm,wherein the mother platform carries out comprehensive management and control on a whole satellite; the first module cabin and the second module cabin are connected with the mother platform and are used for providing a mounting platform for a ultra-large platform single-machine module; the first functional cabin and the second functional cabin are connected with the first module cabin and the second module cabin and are used for carrying a working load; the first connecting truss and the second connecting truss are mounted on the first energy module and the second energy module respectively; and the first mechanical arm and the second mechanical arm are installed on an east side and a west side of the mother platform correspondingly. The configuration can be used for an ultra-large comprehensive satellite platform, on-orbit maintenance of the satellite platform is facilitated, development cost is low, a platform configuration space is open, and energy utilization efficiency is high.

Description

technical field [0001] The invention relates to satellite technology, in particular to a super-large assembling satellite platform configuration. Background technique [0002] In recent years, major aerospace countries have continued to increase their investment in the aerospace industry, and the number of satellite launches has been increasing year by year. Due to the advantages of fixed-point continuous observation, geostationary satellites have become the focus of satellite development in the fields of communication, relay, meteorology, and earth observation. However, geostationary orbit resources are very scarce, and high-orbit satellites will face increasingly tight orbit resources. Therefore, it is urgent to develop ultra-large satellite platforms with greater carrying capacity. Limited by the carrying envelope and launch capability, the launch cost of existing large high-orbit satellites is very high, and the satellite platform that can be assembled in orbit has beco...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/22B64G1/64
CPCB64G1/10B64G1/22B64G1/646
Inventor 杨丽丽李文龙孔祥龙许浩钱勇
Owner SHANGHAI SATELLITE ENG INST
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