@techreport{oai:jaxa.repo.nii.ac.jp:00002724,
 author = {後藤, 大亮 and 香河, 英史 and 梶原, 堅一 and Goto, Daisuke and Kagawa, Hideshi and Kajiwara, Kenichi},
 month = {Oct},
 note = {Catalytic monopropellant thrusters have been loaded in many satellites for reaction control system, because of the reliable simple structure and about 200 sec moderate specific impulse. Nowadays, satellites mass and lifetimes have been increasing, however, Japanese monopropellant thrusters designs were not improved basically. It is therefore thrusters lifetimes have little margin for satellite demand especially in the 1N thruster. During qualification firing test, some malfunctions (ex. misfiring) occurred. Activities for improving thruster reliability have been conducted since FY2000. The results of FY2003 are presented here., 資料番号: AA0048057033, レポート番号: JAXA-RM-04-010},
 title = {触媒スラスタの信頼性向上},
 year = {2004}
}