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規格・テクニカルリポート類

帯電計測に関する研究

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帯電計測に関する研究

Material type
規格・テクニカルリポート類
Author
三宅, 弘晃ほか
Publisher
宇宙航空研究開発機構
Publication date
2006-11-01
Material Format
Digital
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出版タイプ: NAElectrical charge accumulation characteristics in dielectric materials for a spacecraft panel have studied for understanding of spacecraft ch...

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Material Type
規格・テクニカルリポート類
Author/Editor
三宅, 弘晃
松本, 晴久
五家, 建夫
仁田, 工美
Miyake, Hiroaki
Matsumoto, Haruhisa
Goka, Tateo
Nitta, Kumi
Publication, Distribution, etc.
Publication Date
2006-11-01
Publication Date (W3CDTF)
2006-11-01
Alternative Title
Study of measurement for charging on the materials for spacecraft
Periodical title
宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
No. or year of volume/issue
JAXA-SP-06-006
Volume
JAXA-SP-06-006
Pages
163-168
ISSN (Periodical Title)
ISSN : 1349-113X
Text Language Code
jpn
Target Audience
一般
Note (General)
出版タイプ: NA
Electrical charge accumulation characteristics in dielectric materials for a spacecraft panel have studied for understanding of spacecraft charging problem in high energy radiation environment. This study especially has focused on a spacecraft charging accident caused by internal charge accumulation in dielectric materials irradiated by proton beam. The internal charge accumulation of those bulks measurement was carried out using PEA (Pulsed Electro-Acoustic) method. As the results, we obtained a positive charge accumulation in the bulk of samples after proton beam irradiation. However, it was not observed a positive charge accumulation that a quartz glass has an Al evaporated layer on the surface of proton beam irradiation side. Therefore, in this paper, we compare between the PEA's internal charge measurement results and energy band model because of we discus the charge formation mechanism in the bulk irradiated by proton beam. Furthermore, we studied how to measure the secondary electron emission (SEE) of metal and insulating materials used for satellite thermal insulation or other such purposes. SEE yield measurement is very important for analyzing charge accumulation on the satellite surfaces due to the space environment because electron emission. Therefore, we tried to measure the SEE yield. In this report, we introduce the SEE yield measurement results of reference materials (Au, Ag and Quartz glass) and insulating materials. From those results, we discuss the characteristics of SEE that depend on each material.
資料番号: AA0049500035
レポート番号: JAXA-SP-06-006
Data Provider (Database)
国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
Original Data Provider (Database)
宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ