Method for Determining Correlation Degree of Synergistic Effect of Space Environment

A space environment, technology to determine the method, applied in the direction of testing material strength, strength characteristics, material thermal analysis, etc. by applying a stable shear force

Active Publication Date: 2021-05-25
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the synergistic research on space environmental effects is still at the level of qualitative analysis

Method used

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  • Method for Determining Correlation Degree of Synergistic Effect of Space Environment
  • Method for Determining Correlation Degree of Synergistic Effect of Space Environment
  • Method for Determining Correlation Degree of Synergistic Effect of Space Environment

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Embodiment Construction

[0046] The following is a specific implementation manner of the content of the present invention, and the content of the present invention will be further clarified through the specific implementation mode below. Of course, the following specific embodiments are described only to illustrate different aspects of the present invention, and should not be construed as limiting the scope of the present invention.

[0047] see figure 1 , figure 1 It is a schematic diagram of the first step of test development in the method of the present invention, that is, the test layout process. The method for determining the correlation degree of the space environment synergy effect of the present invention includes the following process:

[0048] First, taking the orbital mission environment that the space station intends to experience for one year as an example, the cumulative flux of atomic oxygen experienced during the orbital period is calculated by using the MSISE90 model to be 1.5×10 2...

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Abstract

The invention discloses a method for determining the correlation degree of the synergy effect of the space environment. The method includes determining the high and low temperature alternating environment according to the orbital environment; selecting composite materials and subjecting them to several space environment states in groups; completing the environment according to the test plan. Effect test; according to the effect equivalent principle, determine the atomic oxygen test dose and test machine time; formulate thermal cycle test parameters; complete the two-factor environmental matrix test, and test the performance parameters of the test samples after the test; test the test data in the matrix table Carry out cross-comparison, respectively and the simple sum ratio of the single factor test results, namely the additivity coefficient. Through the understanding, processing, extrapolation and exploration of ground single factor and sequential action test data, the present invention can predict and predict the simultaneous action effect of on-orbit space environment factors, and effectively improve the effectiveness of space environment test research.

Description

technical field [0001] The invention belongs to the technical field of space environment and effect testing, in particular, the invention relates to a method for determining the correlation degree of synergy effects in a space environment. Background technique [0002] At present, the development of aerospace technology has led to the need to study the damage of spacecraft materials in the space environment, so that the spacecraft can achieve aerospace tasks in a safe situation, but in the space environment simulation conditions of spacecraft materials , requires a full understanding of the following correlation effects. [0003] 1) Space environment and its effects [0004] The influence and damage of the complex space environment on space structural materials are important factors that cannot be ignored, and it will directly affect the normal operation, work and service life of the spacecraft. Understanding the space environment and its effects, and mastering the influen...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N33/00G01N25/00G01N3/24
CPCG01N3/24G01N25/00G01N33/00G01N2033/0003G01N2203/0025
Inventor 翟睿琼沈自才王志浩杨东升田东波姜利祥夏彦刘涛
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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