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Rapid response satellite structure

A satellite structure and fast response technology, applied in the direction of artificial satellites, etc., can solve the problems of long assembly cycle and weak load adaptability, and achieve the effect of strong load adaptability, light weight and simple structure

Active Publication Date: 2014-07-23
SHANGHAI SATELLITE ENG INST
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] In order to solve the problems of development, long assembly period, and weak adaptability to loads in the prior art, the purpose of the present invention is to provide a fast response satellite structure

Method used

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Embodiment Construction

[0016] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments.

[0017] refer to figure 1 , the specific embodiment adopts the following technical solutions: a fast-response satellite structure, including a body structure 1 and a propulsion cabin 2, the body structure 1 is composed of a carbon fiber frame containing a bottom plate 101, a lower partition 102, a middle plate 103, an upper partition Board 104, side boards 105 and top board 106 are used to provide the installation foundation for satellite instruments and equipment, and at the same time should be able to withstand various mechanical environments during satellite launch; during ground testing and assembly, it can be independently formed into a cabin. The carbon fiber frame including the bottom plate 101 is made of carbon fiber rods and carbon fiber j...

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Abstract

The invention discloses a rapid response satellite structure. The rapid response satellite structure comprises a body structure and a propelling module. The body structure is composed of a carbon fiber frame (comprising a bottom plate), a lower partition plate, a middle plate, an upper partition plate, a side plate and a top plate; the propelling module is composed of a force bearing cylinder and a propelling modular bottom plate. By the adoption of the rapid response satellite structure, the problems that a research and assembly period is long, and the adaptation to a load is poor are solved. The rapid response satellite structure has the advantages of being simple in structure, light in weight, rapid to assemble, high in expansibility, high in adaptability and the like.

Description

technical field [0001] The invention relates to a satellite structure configuration, in particular to a fast-response satellite structure. Background technique [0002] The satellite structure is a load-bearing structure that provides the installation space and location of the loaded instruments and equipment, bears the static and dynamic loads acting on the satellite, and supports it to complete the predetermined task on the predetermined orbit after entering orbit, and carries the main load of the satellite. It is a satellite system. important component. It has the characteristics of strict quality requirements, limited structural space, ability to adapt to special space environments, and high reliability. At present, the development of satellites is facing difficulties such as short development cycle and multiple tasks. Therefore, the structural design must consider the aspects of simple structure, light weight, rapid assembly, strong expandability, and strong adaptabili...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10
Inventor 吕凯陈占胜顾志悦黄业平
Owner SHANGHAI SATELLITE ENG INST
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