帯電現象に関わる衛星材料の物性パラメータの計測

Material type: 文書・図像類

Author: 仁田, 工美ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-11-01

Material Format: Digital

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Note (General)：: The key parameters in modeling spacecraft charging are the secondary electron emission (SEE) coefficient and photoelectron emission (PE) coefficient o...

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Material Type: 文書・図像類
Title: 帯電現象に関わる衛星材料の物性パラメータの計測
Author/Editor: 仁田, 工美
川北, 史朗
高橋, 真人
艸分, 宏昌
岐部, 公一
三宅, 弘晃
石澤, 淳一郎
國中, 均
Nitta, Kumi
Kawakita, Shiro
Takahashi, Masato
Kusawake, Hiromasa
Kibe, Koichi
Miyake, Hiroaki
Ishizawa, Junichiro
Kuninaka, Hitoshi
Author Heading: 仁田, 工美
川北, 史朗
高橋, 真人
艸分, 宏昌
岐部, 公一
三宅, 弘晃
石澤, 淳一郎
國中, 均
Nitta, Kumi
Kawakita, Shiro
Takahashi, Masato
Kusawake, Hiromasa
Kibe, Koichi
Miyake, Hiroaki
Ishizawa, Junichiro
Kuninaka, Hitoshi
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-11-01
Publication Date (W3CDTF): 2006-11-01
Alternative Title: Material properties measurements related to engineering design optimization guidelines and spacecraft charging
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: 265-270
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 宇宙機帯電
宇宙機構造材料
2次電子
電子放出
光電子
低エネルギー電子
真空紫外放射
衛星設計
材料劣化
航空宇宙環境
spacecraft charging
spacecraft construction material
secondary electron
electron emission
photoelectron
low energy electron
vacuum ultraviolet radiation
satellite design
materials aging
aerospace environment
Target Audience: 一般
Note (General): The key parameters in modeling spacecraft charging are the secondary electron emission (SEE) coefficient and photoelectron emission (PE) coefficient of metals and insulating materials. This work is focused on the analysis and measurement of SEE and PE. A review is presented of methods to measure SEE and PE including the using SEM with short-pulsed electron for accelerating voltage of 600 V-5 kV, a vacuum chamber with a low energy electron beam for accelerating voltage 100 V-2 kV, a measurement system of photo-electron emission, and a photoelectron emission image by vacuum ultraviolet light (VUV). This review is based on joint studies conducted for Japan Aerospace Exploration Agency (JAXA) at High Energy Accelerator Research Organization (KEK), at Musashi Institute of Technology and at Saitama University to investigate the relation to spacecraft charging. This report summarizes some typical measurement results after briefly explaining the measurement project.
資料番号: AA0049500058
レポート番号: JAXA-SP-06-006
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6042&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6042&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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）
https://irdb.nii.ac.jp
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