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Method of determining space environment synergistic effect relevancy

A technology of space environment and determination method, applied in the direction of testing material strength, strength characteristics, measuring devices, etc. by applying stable shear force, to achieve the effect of improving effectiveness

Active Publication Date: 2019-08-09
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

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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 of determining space environment synergistic effect relevancy
  • Method of determining space environment synergistic effect relevancy
  • Method of determining space environment synergistic effect relevancy

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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 of determining space environment synergistic effect relevancy. The method comprises the steps that a high and low temperature alternating environment is determined according to an in-orbit environment; a composite material is selected and is subject to several space environment states in groups; an environment effect test is completed according to a test scheme; according to the effect equivalent principle, an atomic oxygen test dose and test machine hours are determined; thermal circulation test parameters are made; a two-factor environment matrix test is completed, and a test sample performance parameter test after the two-factor environment matrix test is performed; and crossing comparison is performed on test data in a matrix table, and a simple adductratio, namely an additive coefficient, to a single-factor test result is obtained. According to the method, through understanding, processing, extrapolation and exploration of a ground single factor and the sequential action test data, the simultaneous acting effect of in-orbit space environment factors can be estimated and prejudged, and the effectiveness of space environment test research is effectively improved.

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 Applications(China)
IPC IPC(8): G01N33/00G01N25/00G01N3/24
CPCG01N33/00G01N25/00G01N3/24G01N2203/0025G01N33/0003
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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