人工衛星用20N推薬弁の国産開発

Material type: 文書・図像類

Author: 長田, 泰一ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-11-01

Material Format: Digital

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Note (General)：: The Japan Aerospace Exploration Agency (JAXA) is now developing a 20N-class thruster valve for spacecraft propulsion systems. We intend to develop thi...

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Material Type: 文書・図像類
Title: 人工衛星用20N推薬弁の国産開発
Author/Editor: 長田, 泰一
櫛木, 賢一
梶原, 堅一
Nagata, Taiichi
Kushiki, Kenichi
Kajiwara, Kenichi
Author Heading: 長田, 泰一
櫛木, 賢一
梶原, 堅一
Nagata, Taiichi
Kushiki, Kenichi
Kajiwara, Kenichi
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-11-01
Publication Date (W3CDTF): 2006-11-01
Alternative Title: The development of a Japanese 20N thruster valve for a spacecraft propulsion system
Periodical title: 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
No. or year of volume/issue: JAXA-SP-06-006
Volume: JAXA-SP-06-006
Pages: 285-290
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 推薬弁
宇宙機推進
衛星姿勢制御
宇宙機マヌーバ
ロケットノズル
ソレノイド弁
冗長部品
冗長性
応力分布
振動試験
共鳴周波数
thruster valve
spacecraft propulsion
satellite attitude control
spacecraft maneuver
rocket nozzle
solenoid valve
redundant component
redundancy
stress distribution
vibration test
resonant frequency
Target Audience: 一般
Note (General): The Japan Aerospace Exploration Agency (JAXA) is now developing a 20N-class thruster valve for spacecraft propulsion systems. We intend to develop this valve with the high reliability, and a robust and durable design. The suspended armature type was chosen for the base design of the new 20N valve based on the results of a trade-off study. Experiments and analysis were performed for the critical parts and manufacturing process. The results enabled us to manufacture a prototype model with single type 20N thruster valves. Good results were obtained in functional tests. We will now proceed to the next phase and complete the detailed design for series redundancy and prepare for the qualification test.
資料番号: AA0049500062
レポート番号: JAXA-SP-06-006
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6046&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6046&item_no=1&attribute_id=31&file_no=1
Access Restrictions: 限定公開
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