@inproceedings{oai:jaxa.repo.nii.ac.jp:00016294,
 author = {山田, 修 and 堀澤, 秀之 and 小林, 治貴 and 大井川, 祐治 and 細川, 大志 and Yamada, Osamu and Horisawa, Hideyuki and Kobayashi, Haruki and Oigawa, Yuji and Hosokawa, Taishi},
 book = {平成24年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2012},
 month = {Jan},
 note = {平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, In this study, we perform fundamental researches of laser-assisted pulsed plasma thruster used plasma generation by the laser ablation. We observed behavior of the plasma using ICCD camera and measured ion current by Faraday cup. As the result, the airspeed of the plasma calculate by Faraday cup was 134 km/s when charge voltage 1,000 V charged in a condenser and irradiate laser energy 190 mJ and it was 216 km/s when 2000 V., 形態: カラー図版あり, 形態: PDF, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856158, レポート番号: STEP-2012-075},
 pages = {1--6},
 publisher = {宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {矩形型レーザアシストPPT排気プルームのプローブ計測},
 year = {2013}
}