衛星用1液スラスタの信頼性向上活動について(FY16)

Material type: 文書・図像類

Author: 後藤, 大亮ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

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Note (General)：: Catalytic monopropellant thrusters have been loaded in many satellites for reaction control system, because of the reliable simple structure and about...

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Material Type: 文書・図像類
Title: 衛星用1液スラスタの信頼性向上活動について(FY16)
Author/Editor: 後藤, 大亮
香河, 英史
増田, 井出夫
梶原, 堅一
Goto, Daisuke
Kagawa, Hideshi
Masuda, Ideo
Kajiwara, Kenichi
Author Heading: 後藤, 大亮
香河, 英史
増田, 井出夫
梶原, 堅一
Goto, Daisuke
Kagawa, Hideshi
Masuda, Ideo
Kajiwara, Kenichi
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-20
Publication Date (W3CDTF): 2006-01-20
Alternative Title: Reliability improvement of catalytic monopropellant thrusters (FY16)
Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems
No. or year of volume/issue: JAXA-SP-05-008
Volume: JAXA-SP-05-008
Pages: 125-128
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 衛星姿勢制御
ヒドラジン
1液推薬スラスタ
触媒
構造信頼性
金網
推薬分解
satellite attitude control
hydrazine
monopropellant thruster
catalyst
structural reliability
wire mesh
propellant decomposition
Target Audience: 一般
Note (General): 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. We conducted the FMEA in order to investigate the method of lengthen the lifetime of 1N thruster. Then we found out these weak points: (1) Strength of catalyst bed metal mesh, and (2) Lifetime of catalyst granules. We conducted the material analysis of catalyst bed mesh wire that is removed from a life-tested thruster and firing test with the thruster imitation equipment.
資料番号: AA0049054025
レポート番号: JAXA-SP-05-008
Access Restrictions: 限定公開
Periodical Title (NCID): AA11984031
https://ci.nii.ac.jp/ncid/AA11984031
Data Provider (Database): 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）
https://irdb.nii.ac.jp
Original Data Provider (Database): 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