@techreport{oai:jaxa.repo.nii.ac.jp:00006042,
 author = {仁田, 工美 and 川北, 史朗 and 高橋, 真人 and 艸分, 宏昌 and 岐部, 公一 and 三宅, 弘晃 and 石澤, 淳一郎 and 國中, 均 and Nitta, Kumi and Kawakita, Shiro and Takahashi, Masato and Kusawake, Hiromasa and Kibe, Koichi and Miyake, Hiroaki and Ishizawa, Junichiro and Kuninaka, Hitoshi},
 month = {Nov},
 note = {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},
 title = {帯電現象に関わる衛星材料の物性パラメータの計測},
 year = {2006}
}