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On-orbit fault warning and screening device for spacecraft

A fault early warning and spacecraft technology, which is applied to measurement devices, electric devices, and spacecraft for space navigation, etc., can solve the problems of no spacecraft on-orbit fault early warning and screening device, and spacecraft on-orbit faults.

Active Publication Date: 2021-07-06
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0010] 4) The space radiation environment leads to the main reasons for spacecraft on-orbit failures
[0013] At present, there is no device for early warning and screening of spacecraft on-orbit failures at home and abroad, and it is impossible to realize a detection device for early warning and screening of spacecraft on-orbit failures

Method used

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  • On-orbit fault warning and screening device for spacecraft
  • On-orbit fault warning and screening device for spacecraft
  • On-orbit fault warning and screening device for spacecraft

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Embodiment Construction

[0031] The present invention will be described in further detail below in conjunction with the accompanying drawings, but this is only exemplary and not intended to limit the protection scope of the present invention. The present invention will be further described below in conjunction with the accompanying drawings and embodiments. It should be noted that the following embodiments are intended to facilitate the understanding of the present invention, and do not have any limiting effect on it.

[0032] see figure 1 , figure 1It shows a schematic structural diagram of a spacecraft on-orbit fault early warning and screening device according to a specific embodiment of the present invention, wherein the spacecraft on-orbit fault early warning detection device includes a rectangular chassis 1 (i.e., a detector housing), three groups of detection units, energy Analyzer 6, low-energy particle detector 7, high-energy particle detector 8, each detection unit is composed of temperatur...

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Abstract

The invention discloses an on-orbit fault early warning detection device for a spacecraft, comprising a detector housing, three groups of detection units, an energy analyzer, a low-energy charged particle detector, and a high-energy charged particle detector, wherein the three groups of detection units are composed of Composed of a temperature sensor and a total dose sensor, respectively detect the radiation effect under the unshielded state, the equivalent shielding thickness of the spacecraft bulkhead thickness, and the total equivalent shielding thickness inside the spacecraft; the energy analyzer is used to detect electrons below 100keV , the low-energy charged particle detector and the high-energy charged particle detector respectively detect low-energy and high-energy electrons / protons. The invention can realize the hierarchical detection of electrons and protons with different energies, obtain the total dose data and dose rate data at different positions on the surface and inside of the spacecraft at the same time, and has multiple functions, accurate on-orbit fault warning and fault screening of the spacecraft Features.

Description

technical field [0001] The invention belongs to the technical field of spacecraft on-orbit situation detection, and specifically relates to a spacecraft on-orbit fault early warning detection device. Background technique [0002] The space radiation environment mainly comes from stellar radiation belts, solar cosmic rays, and galactic cosmic rays, and its main components are electrons, protons and a small amount of heavy ions. Among them, the Earth's radiation belt environment is one of the most important radiation environments affecting spacecraft in low-Earth orbit, and can usually be divided into the inner radiation belt and the outer radiation belt. During solar flares, a large number of high-energy protons, electrons, and heavy nuclear particles are emitted, which are called solar cosmic rays. Most of them are composed of protons, so it is also known as the solar proton event. The energy of solar cosmic ray particles generally ranges from 10 MeV to tens of GeV. Its c...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01T1/02G01T1/29G01T1/36G01K7/22B64G1/66
CPCB64G1/66G01K7/22G01T1/02G01T1/29G01T1/36
Inventor 沈自才刘业楠丁义刚夏彦刘宇明王志浩田东波
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG