@inproceedings{oai:jaxa.repo.nii.ac.jp:00016592,
 author = {鈴木, 信義 and 佐原, 宏典 and Suzuki, Nobuyoshi and Sahara, Hironori},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, We have been studying the generalized propulsion system based on green mono/bi-propellant since 2008. While, the last achievements prove feasibility of the propulsion system and conducted captive test with a breadboard model (BBM), no ignition was confirmed there. Accordingly, we modified the ejector in thruster and measured droplet diameter of liquid propellant in combustion chamber, and improved performance of propellant atomization., 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: AA0064741022},
 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 = {低毒性推進剤による二液式推進系の研究開発},
 volume = {平成21年度},
 year = {2010}
}