並列タイトル等Study of water energy cycle space propulsion system
タイトル（掲載誌）宇宙航空研究開発機構特別資料: 平成18年度 宇宙航空研究開発機構 総合技術研究本部 宇宙科学研究本部 研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
一般注記Water-Energy-Cycle Space Propulsion System was defined as a space system supporting long-term and large-scale space activity. On the test stand which can change a posture, the principle model was assembled, the posture was changed in +/- 1 G, and the performance of a principle model was compared. As a result of experimenting in +/- 1 G, when it operated normally in any case and it did separation of gas and a liquid on the level of each subsystem, under terrestrial gravity environment, it came out enough and a certain thing was understood. The feel referred to as operating satisfactory also under the micro-gravity environment of space was acquired as a result of consideration. The Proton Exchange Membrane (PEM) electrolyzer and the fuel cell which were used for the experiment made the regenerative fuel cell as an experiment, and used the single cell for this research in normal temperature. The phenomenon of ignition delay has been improved by the device of injection structure, and adjustment of injection timing in the catalyst ignition experiment of hydrogen/oxygen thruster. Moreover, it turns out that water adheres to the catalyst layer surface after a combustion end.
資料番号: AA0049500064
レポート番号: JAXA-SP-06-006
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ