放电触发的卫星内部电场分布模拟

1999 Fifth European Conference on Radiation and Its Effects on Components and Systems. RADECS 99 (Cat. No.99TH8471) Pub Date : 1999-09-13 DOI:10.1109/RADECS.1999.858542

L. Varga, E. Horvath, D. Haslip

{"title":"放电触发的卫星内部电场分布模拟","authors":"L. Varga, E. Horvath, D. Haslip","doi":"10.1109/RADECS.1999.858542","DOIUrl":null,"url":null,"abstract":"This work examines an electrostatic charging/discharging cycle of a populated circuit board inside an equipment housing of a satellite at GEO. Component potentials and electric field strengths are examined before and after a structure ground discharge event. Field reversal after the discharge suggests that favourable conditions exist for charge dissipation from the internal dielectrics at this point in time. Electric field strength dependent, this can be either spontaneous or drift related. This work was realized using a tool of two components. The charging cycle is calculated using a modified ITS-ACCEPT code. The resulting charge distribution is used as input to a 3D Poisson equation solver.","PeriodicalId":135784,"journal":{"name":"1999 Fifth European Conference on Radiation and Its Effects on Components and Systems. RADECS 99 (Cat. No.99TH8471)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1999-09-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Modeling of discharge-triggered electric field redistribution on the interior components of a satellite\",\"authors\":\"L. Varga, E. Horvath, D. Haslip\",\"doi\":\"10.1109/RADECS.1999.858542\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"This work examines an electrostatic charging/discharging cycle of a populated circuit board inside an equipment housing of a satellite at GEO. Component potentials and electric field strengths are examined before and after a structure ground discharge event. Field reversal after the discharge suggests that favourable conditions exist for charge dissipation from the internal dielectrics at this point in time. Electric field strength dependent, this can be either spontaneous or drift related. This work was realized using a tool of two components. The charging cycle is calculated using a modified ITS-ACCEPT code. The resulting charge distribution is used as input to a 3D Poisson equation solver.\",\"PeriodicalId\":135784,\"journal\":{\"name\":\"1999 Fifth European Conference on Radiation and Its Effects on Components and Systems. RADECS 99 (Cat. No.99TH8471)\",\"volume\":\"1 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1999-09-13\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"1999 Fifth European Conference on Radiation and Its Effects on Components and Systems. RADECS 99 (Cat. No.99TH8471)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/RADECS.1999.858542\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"1999 Fifth European Conference on Radiation and Its Effects on Components and Systems. RADECS 99 (Cat. No.99TH8471)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/RADECS.1999.858542","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}

引用次数: 0

摘要

这项工作考察了地球静止轨道卫星设备外壳内电路板的静电充放电周期。在结构接地放电事件发生前后，研究了构件电位和电场强度。放电后的场反转表明，此时存在有利于内部介质的电荷耗散的条件。电场强度依赖，这可以是自发的或漂移相关。这项工作是使用两个组件的工具实现的。充电周期使用修改后的ITS-ACCEPT代码计算。所得电荷分布用作三维泊松方程求解器的输入。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Modeling of discharge-triggered electric field redistribution on the interior components of a satellite

This work examines an electrostatic charging/discharging cycle of a populated circuit board inside an equipment housing of a satellite at GEO. Component potentials and electric field strengths are examined before and after a structure ground discharge event. Field reversal after the discharge suggests that favourable conditions exist for charge dissipation from the internal dielectrics at this point in time. Electric field strength dependent, this can be either spontaneous or drift related. This work was realized using a tool of two components. The charging cycle is calculated using a modified ITS-ACCEPT code. The resulting charge distribution is used as input to a 3D Poisson equation solver.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

1999 Fifth European Conference on Radiation and Its Effects on Components and Systems. RADECS 99 (Cat. No.99TH8471)

自引率

0.00%

发文量