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A Research Method for the Effect of Electric Propulsion Plume on Solar Cell Arrays

A solar cell array and electric propulsion technology, applied in geometric CAD, design optimization/simulation, CAD numerical modeling, etc., can solve problems such as not meeting the development needs of solar cell arrays, and achieve the effect of improving comprehensive competitiveness and avoiding financial resources.

Active Publication Date: 2022-08-02
中电科蓝天科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, domestic and foreign studies on the effect of plumes on solar cell arrays mainly focus on the research on the sputtering corrosion effect on the glass cover and silver interconnects, the thermal simulation of the unsuperimposed space environment, and the space filling without considering the plume plasma. In terms of discharge effect research, with the continuous development of solar cell array development technology, the continuous superposition of space environment and plume effects, and the continuous expansion of the application of new materials on the surface of solar cell arrays, the original research methods will not meet the needs of solar cell arrays. development needs

Method used

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  • A Research Method for the Effect of Electric Propulsion Plume on Solar Cell Arrays
  • A Research Method for the Effect of Electric Propulsion Plume on Solar Cell Arrays
  • A Research Method for the Effect of Electric Propulsion Plume on Solar Cell Arrays

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Embodiment Construction

[0047] In order to make those skilled in the art better understand the solutions of the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are only The embodiments are part of the present application, but not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the scope of protection of the present application.

[0048] It should be noted that the terms "comprising" and "having" and any variations thereof are intended to cover non-exclusive inclusion, for example, a process, method, system, product or device comprising a series of steps or units is not necessarily limited to the explicit Instead, those steps or elements listed may inc...

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Abstract

The invention discloses a method for researching the influence of an electric propulsion plume on a solar cell array, belonging to the technical field of electric propulsion systems. Analysis method; S2. Analysis method for studying the effect of electric thruster plume on sputtering corrosion of solar cell array surface materials; S3. Analysis method for studying electric thruster plume on solar cell array heating effect; S4, Studying electric thruster plume An analytical method for charging and discharging effects of solar cell arrays. By adopting the above technical solutions, the present invention provides a comprehensive design basis for accurately evaluating the influence of different electric thrusters on the solar cell array in the space environment application. Avoid repetitive simulations, experiments and mechanism analysis. Avoid unnecessary waste of financial, human and material resources and enhance comprehensive competitiveness.

Description

technical field [0001] The invention belongs to the technical field of electric propulsion systems, and in particular relates to a research method for the influence of electric propulsion plumes on solar cell arrays. Background technique [0002] As we all know, an electric thruster is a device that uses electrical energy to heat, ionize, and accelerate a working medium to generate high-speed ions, thereby generating thrust. Compared with traditional chemical thrusters, electric thrusters have the advantages of high specific impulse, long life, compact structure and light weight. In recent years, they have been widely used in deep space exploration, satellite orbit maintenance, satellite attitude control and orbit transfer. . As an important part of the spacecraft energy system, the solar array is exposed outside the cabin for a long time. The thruster plume formed when the electric thrusters of different types, functions and installation positions work and the CEX backflo...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/25G06F30/10G06F111/10
CPCG06F30/25G06F30/10G06F2111/10
Inventor 张肖君程保义刘吉晔
Owner 中电科蓝天科技股份有限公司
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