Method for carrying out spatial displacement damage effect evaluation test through high energy protons

A technology of spatial displacement and damage effect, applied in the direction of measuring devices, instruments, measuring electricity, etc., can solve the problems of not giving the best proton energy selection method for the internal environment of the spacecraft, and not applying the displacement damage effect, etc. performance, accurate evaluation results

Inactive Publication Date: 2015-01-21
CHINA ACADEMY OF SPACE TECHNOLOGY
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] In the prior art, the method of using neutrons to evaluate the displacement damage of the neutron environment is given, and there is an equivalent problem of different radiation sources in the evaluation of the displacement damage caused by space protons. At present, the equivalent problem of different radiation sources has not been completely solved; Using cobalt-60γ-rays to evaluate the ionizat

Method used

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  • Method for carrying out spatial displacement damage effect evaluation test through high energy protons
  • Method for carrying out spatial displacement damage effect evaluation test through high energy protons
  • Method for carrying out spatial displacement damage effect evaluation test through high energy protons

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Embodiment 1

[0037] A test method for evaluating the internal displacement damage effect of a low-earth orbit spacecraft with high-energy protons specifically includes the following steps:

[0038] Step 1. Calculation of the radiation environment inside the low earth orbit spacecraft

[0039] The space environment effect calculation software (such as Space Radiation, or CREME software) is used to calculate the orbital parameters of the earth-earth orbiting spacecraft. The proton model uses the AP8 model; the solar proton uses the ESP model (7 years of solar high years, 90% confidence level). The shielding thickness of the spacecraft is 3mm, 10mm, and 30mm aluminum respectively. The calculation results of proton differential energy spectrum inside the spacecraft can be found in image 3 .

[0040] Step 2, Select Proton

[0041] From image 3 The low-earth orbit (LEO) proton differential energy spectrum shown shows that in the interior of the low-earth orbit spacecraft, under the condit...

Embodiment 2

[0048] A test method for evaluating the internal displacement damage effect of a geosynchronous orbit spacecraft by using high-energy protons specifically includes the following steps:

[0049] Step 1. Calculation of the radiation environment inside the geosynchronous orbit spacecraft

[0050] Using the Space Radiation space environment effect calculation software, input the altitude and inclination of the spacecraft orbit (36000km, 0°), the space radiation environment model is: the AP8 model is used to capture protons; ). The shielding thickness of the spacecraft is 3mm, 10mm, and 30mm aluminum respectively. The calculation results of proton differential energy spectrum inside the spacecraft are as follows: Figure 4 shown.

[0051] Step 2, Select Proton

[0052] From Figure 4 The shown geosynchronous orbit (GEO) proton differential energy spectrum shows that inside the geosynchronous orbit spacecraft, under the condition of 3mm~30mm aluminum shielding, the proton energ...

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Abstract

The invention relates to a method for carrying out a spatial displacement damage effect evaluation test through high energy protons. The method includes the following steps that firstly, internal radiation environment of a spacecraft is calculated, space environment effect calculation software is used, track parameter values of the earth track spacecraft, a space radiation environment model, the shielding thickness of the spacecraft are input, and the internal proton differential energy spectrum of the spacecraft is calculated; secondly, the protons are selected, the worked-out internal proton differential energy spectrum of the spacecraft in the track has a proton fluence peak value as the protons are not evenly distributed along with energy, and the energy proton corresponding to the fluence peak value is selected as the proton for the evaluation test; thirdly, the proton fluence phi(EI) for the test is calculated; fourthly, the radiation test is carried out, and the energy protons determined through calculation are used for radiating an element to the specified fluence. After radiation, the electricity test is carried out according to product standards and requirements.

Description

technical field [0001] The invention relates to a method for evaluating the effect of space displacement damage by using high-energy protons, which can be used to guide the performance degradation of aerospace devices caused by the displacement damage effect in the space radiation environment, and obtain data on the ability of the device to resist displacement damage. The radiation resistance hardening design provides a basis, and also provides reference data for satellite designers to select devices with radiation resistance that meet the requirements and to carry out application hardening design. Background technique [0002] High-energy particles in the space radiation environment, such as protons, are incident on the devices in the electronic system of the spacecraft, which will produce displacement damage effects, resulting in performance degradation and even failure of spacecraft devices. Spacecraft devices need to undergo displacement effect test evaluation to obtain ...

Claims

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Application Information

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IPC IPC(8): G01R31/00
Inventor 于庆奎罗磊张洪伟孙毅祝名唐民
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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