@inproceedings{oai:jaxa.repo.nii.ac.jp:00016791,
 author = {岸田, 佳晃 and 綾部, 友洋 and 堀澤, 秀之 and 船木, 一幸 and Kishida, Yoshiaki and Ayabe, Tomohiro and Horisawa, Hideyuki and Funaki, Ikko},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), A fundamental study of newly developed PPT type laser-electromagnetic hybrid thrusters was conducted, in which laser-induced plasma was induced through laser beam irradiation onto a solid target and accelerated by electrical means instead of direct acceleration only by using a laser beam. The performance of the thrusters was evaluated by measuring the mass shot and the impulse bit, and calculating the Specific impulse and the propulsion efficiency. In a rectangular type, it experimented on the laser energy as 1 J and the charge energy as 0 - 8.6 J. As a result, specific impulse was 5300 - 7100 second and the propulsion efficiency was 11.8 - 21.3 %., 形態: カラー図版あり, 資料番号: AA0064292098},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {レーザ・電磁加速複合推進機の形状と推進剤が推進性能に及ぼす影響},
 volume = {平成20年度},
 year = {2009}
}