@inproceedings{oai:jaxa.repo.nii.ac.jp:00016234,
 author = {近藤, 圭佑 and 堀澤, 秀之 and Kondo, Keisuke and Horisawa, Hideyuki},
 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, an investigation of an exotic pair or a mixture of non-hazardous materials was conducted, either in solid or liquid state substances, with higher heat releases through chemical reactions augmented by low-power continuous wave (CW) lasers. Numerical evaluation of exothermic energies or heat release, through chemical reactions of the target propellants was conducted with chemical equilibrium calculation code. From the results, some propellants showed temperature increase higher than conventional propellants., 形態: カラー図版あり, 形態: PDF, Translation title: Investigation on energetic propellant of laser-ablation propulsion, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856098, レポート番号: STEP-2012-015},
 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 = {レーザー推進用高エネルギー推進剤に関する基礎研究},
 year = {2013}
}