On-orbit assembly spacecraft based on pre-integrated truss

A spacecraft and truss technology, applied in the field of spacecraft that can be assembled on-orbit, can solve problems such as inconvenient maintenance in the later stage of design and operation, complex structural units, safety problems, etc., to enhance mission execution capabilities, overcome launch capabilities, and assembly efficiency. high effect

Inactive Publication Date: 2019-08-30
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the on-orbit assembly of ISS still has the following shortcomings: the structural units assembled on-orbit are too complex, such as various types of trusses, which make the versatility not strong, which brings a lot of inconvenience to design, operation and even later maintenance. place; on-orbit assembly is often attended by people, which brings safety issues

Method used

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  • On-orbit assembly spacecraft based on pre-integrated truss
  • On-orbit assembly spacecraft based on pre-integrated truss

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Embodiment Construction

[0023] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0024] The present invention provides an on-orbit assembling spacecraft based on a pre-integrated truss. The on-orbit assembling spacecraft is mainly composed of basic units such as a pre-integrated truss structure 1, a payload 8, and a mission support module 9. Extended docking interface. The pre-integrated truss structure 1 is the main load-bearing structure of the spacecraft that can be assembled in orbit, and the payload and mission support module 9 are externally connected to the pre-integrated truss structure 1 through the docking interface. The payload is configured according to the specific application task. The basic module of the platform ensures the normal operation of the spacecraft platform and supports the work of the payload. The mission support module is an essential tool for performing on-orbit assembly operation tasks.

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Abstract

The invention discloses an on-orbit assembly spacecraft based on a pre-integrated truss, and relates to the technical field of spacecraft on-orbit service. The on-orbit assembly spacecraft comprises apre-integrated truss structure, four solar battery arrays, a storage battery pack, two propelling modules, a pose measurement and control module and a digital management module; the pre-integrated truss structure is of a support structure with a Chinese character "jing" shape which is formed by four supports; the four solar battery arrays are symmetrically installed at the two ends of two opposite supports of the pre-integrated truss structure; the storage battery pack is installed on the outer side wall of one support of the pre-integrated truss structure; the pose measurement and controlling module is installed on the outer side wall of the support, which is opposite to the storage battery pack, of the pre-integrated truss structure; the two propelling modules are symmetrically installed on the outer side walls of the other two opposite supports of the pre-integrated truss structure; and the digital management module is installed on the inner side wall of one support of the pre-integrated truss structure. The on-orbit assembly spacecraft provides a novel means for on-orbit application of a large spacecraft, and can implement tasks such as on-orbit assembly and on-orbit functionexpansion.

Description

technical field [0001] The invention relates to the technical field of on-orbit service of spacecraft, in particular to an on-orbit assembling spacecraft based on a pre-integrated truss. Background technique [0002] Most of the current spacecraft are designed and assembled on the ground and launched into orbit to perform tasks. However, with the development of spacecraft technology, the requirements for the size and weight of spacecraft are getting higher and higher. Most of the current spacecraft are composed of multiple compartments or modules, and the size and weight are getting larger and larger. The total size of these spacecraft has far exceeded the launch capacity of the launch vehicle. Execution of on-orbit missions for large spacecraft. It is a good way to solve the series of problems by launching the spacecraft components into the orbit multiple times through the launch vehicle and implementing the assembly of the spacecraft on orbit. [0003] At the same time,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/22
CPCB64G1/22
Inventor 陈维春陈新龙宋琦陈大可
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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