@techreport{oai:jaxa.repo.nii.ac.jp:00006048,
 author = {橋本, 保成 and Hashimoto, Yasunari},
 month = {Nov},
 note = {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},
 title = {水サイクル宇宙推進システムの研究},
 year = {2006}
}