@inproceedings{oai:jaxa.repo.nii.ac.jp:00007977,
 author = {橋本, 保成 and 田中, 孝治 and 嶋田, 貴信 and 石井, 忠司 and Hashimoto, Yasunari and Tanaka, Koji and Shimada, Takanobu and Ishii, Tadashi},
 book = {宇宙エネルギーシンポジウム, Space Energy Symposium},
 month = {Feb},
 note = {第29回宇宙エネルギーシンポジウム(2010年2月26日, 宇宙航空研究開発機構宇宙科学研究本部相模原キャンパス), The twenty-ninth Space Energy Symposium (February 26, 2010, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara), In general, the hydrazine system is used as attitude control engine for the satellite. However, it is poisonous, and protective wear is necessary for hydrazine for handling in the launch range.Water-Energy-Cycle Space Propulsion System can be used as a harmless attitude control engine that uses hydrogen/oxygen as a propellant.It replaces the hydrazine system here, and it introduces hydrogen/oxygen engine that uses the catalyst ignition that becomes attitude control engine for the satellite., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0064737005},
 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 = {水サイクル宇宙推進システムは小型衛星に利用できるか},
 volume = {29},
 year = {2010}
}