@inproceedings{oai:jaxa.repo.nii.ac.jp:00006415,
 author = {Hilgers, A. and Thiebault, B. and Estublier, D. and Gengembre, E. and Gonzalez, J. and Roussel, J. F. and Tajmar, M. and Markelov, G. and Forest, J.},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: 9th Spacecraft Charging Technology Conference},
 month = {Aug},
 note = {Results from SMART-1 plasma measurements indicate that the spacecraft is in general floating 10 to 30 Volts negative with respect to the ambient plasma. An analytical model based on the interaction of the charge exchange plasma with the spacecraft and the solar panels is shown to be in good quantitative agreement with most of the observations. Progress for simulating the overall interaction between the thruster plume and the spacecraft by the use of PIC simulation codes is also presented., 資料番号: AA0049206100, レポート番号: JAXA-SP-05-001E},
 pages = {884--889},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Modeling of SMART-1 interaction with the electric thruster plume},
 volume = {JAXA-SP-05-001E},
 year = {2005}
}