3D-C/C複合材の試験法標準化研究

Material type: 文書・図像類

Author: 青木, 卓哉ほか

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)：: Three-dimensionally reinforced carbon-fiber-reinforced carbon matrix (3D-C/C) composites have been applied to the nozzle throats of solid propellant r...

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Material Type: 文書・図像類
Title: 3D-C/C複合材の試験法標準化研究
Author/Editor: 青木, 卓哉
小笠原, 俊夫
八田, 博志
石川, 隆司
後藤, 健
Aoki, Takuya
Ogasawara, Toshio
Hatta, Hiroshi
Ishikawa, Takashi
Goto, Ken
Author Heading: 青木, 卓哉
小笠原, 俊夫
八田, 博志
石川, 隆司
後藤, 健
Aoki, Takuya
Ogasawara, Toshio
Hatta, Hiroshi
Ishikawa, Takashi
Goto, Ken
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: Standardization of test methods for evaluating the mechanical properties of 3D-C/C composites utilized for nozzle throats of solid rocket motors
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: 61-66
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: C/C複合材
ロケットノズル
ノズル設計
機械的性質
評価
固体燃料ロケットエンジン
ノズルスロート
標準化
性能試験
引張試験
C/C composite
rocket nozzle
nozzle design
mechanical property
evaluation
solid propellant rocket engine
nozzle throat
standardization
performance test
tensile test
Target Audience: 一般
Note (General): Three-dimensionally reinforced carbon-fiber-reinforced carbon matrix (3D-C/C) composites have been applied to the nozzle throats of solid propellant rockets such as SRB-A and M-V due to the excellent heat resistance exceeding 2,273 K. In order to assure the design reliability of the nozzle throats, the mechanical properties of the 3D-C/C composites are necessary from room temperature to elevated temperatures. However, no well-developed test method is available at present to evaluate the mechanical properties. The objective of this research is therefore placed upon the standardization of the test methods for evaluating the mechanical properties of the 3D-C/C composites utilized for the nozzle throats. The mechanical tests discussed in this research include tensile, compressive and shear tests of the 3D-C/C composites from room temperature to elevated temperatures exceeding 2,273 K.
資料番号: AA0049500012
レポート番号: JAXA-SP-06-006
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=5996&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=5996&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