並列タイトル等Development of the fuel cell for aerospace applications
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Japan Aerospace Exploration Agency (JAXA) is now developing polymer electrolyte fuel cell (PEFC) systems that can be applied to the high altitude balloon, transfer vehicle, and space craft. We designed the fuel cell system for low pressure environment where the working gases were supplied by the counter-flow method and the temperature of the system was passively controlled by the heat generated from the fuel cell stack. We assembled the system and are testing its performance under the thermal vacuum conditions. Furthermore, we started the development of a fuel cell system which can be operated by the propellants for spacecraft. We tried to operate the fuel cell using Hydrazine and Nitrogen Tetra Oxide. Through our measurements, stable generation of electricity was observed using PEFC. We also tried to measure the performance of the PEFC using the propellants with additives in order to decrease the melting point of the propellants.
資料番号: AA0049500056
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