セラミックスラスタの開発

Material type: 文書・図像類

Author: 中塚, 潤一ほか

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)：: In recent days, the propulsion subsystem of spacecraft is required to achieve higher reliability and performance simultaneously. The performance of th...

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Material Type: 文書・図像類
Title: セラミックスラスタの開発
Author/Editor: 中塚, 潤一
澤井, 秀次郎
Nakatsuka, Junichi
Sawai, Shujiro
Author Heading: 中塚, 潤一
澤井, 秀次郎
Nakatsuka, Junichi
Sawai, Shujiro
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: Development of ceramic thruster
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: 281-284
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 宇宙機推進
セラミック
スラスタ
推力測定
窒化珪素
燃焼試験
ロケットノズル
機械的性質
振動試験
衝撃試験
比推力
spacecraft propulsion
ceramic
thruster
thrust measurement
silicon nitride
firing test
rocket nozzle
mechanical property
vibration test
shock test
specific impulse
Target Audience: 一般
Note (General): In recent days, the propulsion subsystem of spacecraft is required to achieve higher reliability and performance simultaneously. The performance of thrusters has a great impact to the weight budget of the propulsion subsystem, because high performance thruster can reduce the quantity of propellant by high-temperature combustion. If the Thruster improves performance, the spacecraft can save the weight. Ceramics is one of the most promising materials for the spacecraft on-board thrusters because of their superior performance on heat resistance. However they are brittle, and thus they have not been used in the real flight missions so far. It might be fractured due to mechanical vibration at launch, thermal shock at firing, or by collision of space debris. This paper summarizes the status of development, in which a prototype 500 N bipropellant thruster made of Si-based monolithic ceramic has been developed.
資料番号: AA0049500061
レポート番号: JAXA-SP-06-006
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