以卫星充电为重点的雪崩光电二极管(APD)型空间电子测量装置的研制

K. Koga, H. Ueno
{"title":"以卫星充电为重点的雪崩光电二极管(APD)型空间电子测量装置的研制","authors":"K. Koga, H. Ueno","doi":"10.2322/tastj.17.380","DOIUrl":null,"url":null,"abstract":"Satellite charging causes anomalies and its effect still accounts for the main part of failure that occurs in the space environment. It is important to measure plasma particles in order to elucidate the interactions between such charging and the space environment. For this purpose, the Avalanche PhotoDiode (APD) type sensor is used to minimize instrument size and weight. The APD basically measures photons, but can also be used to measure electrons. This paper reports the performance of the APD sensor, and presents the instrument design results for flight investigation.","PeriodicalId":120185,"journal":{"name":"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN","volume":null,"pages":null},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Development of Avalanche PhotoDiode (APD) Type Electron Measurement Unit for Space Use Focused on Satellite Charging\",\"authors\":\"K. Koga, H. Ueno\",\"doi\":\"10.2322/tastj.17.380\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Satellite charging causes anomalies and its effect still accounts for the main part of failure that occurs in the space environment. It is important to measure plasma particles in order to elucidate the interactions between such charging and the space environment. For this purpose, the Avalanche PhotoDiode (APD) type sensor is used to minimize instrument size and weight. The APD basically measures photons, but can also be used to measure electrons. This paper reports the performance of the APD sensor, and presents the instrument design results for flight investigation.\",\"PeriodicalId\":120185,\"journal\":{\"name\":\"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.2322/tastj.17.380\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.2322/tastj.17.380","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

卫星充装会引起异常,其影响仍然是空间环境中发生故障的主要原因。对等离子体粒子的测量对于阐明等离子体电荷与空间环境的相互作用具有重要意义。为此,雪崩光电二极管(APD)型传感器用于最小化仪器尺寸和重量。APD基本上可以测量光子,但也可以用来测量电子。本文报道了APD传感器的性能,并给出了用于飞行调查的仪器设计结果。
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
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Development of Avalanche PhotoDiode (APD) Type Electron Measurement Unit for Space Use Focused on Satellite Charging
Satellite charging causes anomalies and its effect still accounts for the main part of failure that occurs in the space environment. It is important to measure plasma particles in order to elucidate the interactions between such charging and the space environment. For this purpose, the Avalanche PhotoDiode (APD) type sensor is used to minimize instrument size and weight. The APD basically measures photons, but can also be used to measure electrons. This paper reports the performance of the APD sensor, and presents the instrument design results for flight investigation.
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
自引率
0.00%
发文量
0
期刊最新文献
Allowable Initial Relative Velocity of a Net to Contact and Capture Space Debris A Smoothed Eclipse Model for Solar Electric Propulsion Trajectory Optimization Application of Machine Learning to the Particle Identification of GAPS Numerical Analysis on Reusable Rocket Aerodynamics with Reduced-Yaw-Force Configurations Investigation into Star Tracker Algorithms using Smartphones with Application to High-Precision Pointing CubeSats
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1