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Thermal vacuum test suitable for space X-ray load whole-satellite

A technology of thermal vacuum test and X-ray, which is applied in the field of thermal vacuum test applicable to space X-ray load of the whole star, and can solve the problems affecting satellite test results, etc.

Inactive Publication Date: 2019-04-09
BEIJING INST OF SPACECRAFT SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the large field of view of the X-ray light tube, it will irradiate the space simulation room and the whole star, and will also generate undesired X-rays, which will form the redundant background of the detector and affect the test results of the satellite.

Method used

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  • Thermal vacuum test suitable for space X-ray load whole-satellite
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  • Thermal vacuum test suitable for space X-ray load whole-satellite

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Embodiment Construction

[0040] Aiming at the deficiencies of the prior art, this invention proposes a thermal vacuum test method suitable for space X-ray load whole star, which uses X-ray light tube to irradiate samples to generate required X-ray spectral lines, which can solve the problem of whole star thermal vacuum The safety and management of multiple radioactive sources during the test process, and at the same time determine the X-ray background and detector anti-pollution problems during the whole-star thermal vacuum test process.

[0041] This method utilizes the characteristics of single-energy X-rays produced by X-ray light tubes to irradiate different materials, and proposes a whole-stellar thermal vacuum test X-ray load thermal test method, which can realize the test and pollution control of X-ray detection loads in the state of the whole star without radioactive sources. The method is mainly divided into four parts:

[0042](1) Use the X-ray light tube to shoot the target twice, and gener...

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Abstract

The invention discloses a thermal vacuum test suitable for a space X-ray load whole-satellite. The method comprises the following steps: producing X-ray in a vacuum test tank by utilizing secondary targeting of an X-ray light pipe, and then determining that the secondary targeting of the X-ray light tube causes a background, and controlling pollutant in a test process, and finally accomplishing the performance test and processing on the load. Compared with the prior art, multiple radioactive sources can be replaced, different energy band spectral lines can be produced as required, and the on-off control can be performed according to a test demand; the performance test of the X-ray load and the excitation X-ray background control under the whole satellite state are guaranteed, and the pollution in the vacuum thermal test process is controlled, and the safety and the controllability in the whole-satellite thermal vacuum test process is realized.

Description

technical field [0001] The invention relates to a thermal vacuum test method applicable to a space X-ray load whole star, and is applicable to a performance test method during a thermal vacuum test of a whole space X-ray telescope satellite or a single space X-ray telescope. Background technique [0002] Since X-rays cannot penetrate the Earth's atmosphere, space X-ray experiments can only be carried out on rockets or satellites orbiting outside the atmosphere. The same problem also occurs in the ground performance test of space X-ray telescopes. In order to avoid the absorption of X-rays by the ground air, the general performance of X-ray telescopes requires the use of special radioactive sources and special test systems. For the radioactive source method, relevant X-ray radioactive sources need to be specially produced, and they need to be placed relatively close to the telescope detector to form an X-ray source of specific energy. At present, this method mostly uses low r...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01V13/00
CPCG01V13/00
Inventor 张龙张也弛刘欣李昂洪斌卢方军徐玉朋赵二鑫张雪
Owner BEIJING INST OF SPACECRAFT SYST ENG
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