ロケットエンジン高信頼化設計手法の研究:概念設計品質の最適化方法.起動過渡における故障シミュレーション

Material type: 文書・図像類

Author: 青木, 宏ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: In past, the Design for Space Systems has conducted accumulating the optimum design results for each device. 'System Reliability Level' was measured a...

Search by Bookstore

Holdings of Libraries in Japan

This page shows libraries in Japan other than the National Diet Library that hold the material.

List of Cooperating Institutions and Databases

Please contact your local library for information on how to use materials or whether it is possible to request materials from the holding libraries.

other

JAXA Repository
Digital
You can check the holdings of institutions and databases with which 学術機関リポジトリデータベース（IRDB）（機関リポジトリ） is linked at the site of 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）.
JAXA Repository

Search by Bookstore

Bibliographic Record

You can check the details of this material, its authority (keywords that refer to materials on the same subject, author's name, etc.), etc.

Digital

Material Type: 文書・図像類
Title: ロケットエンジン高信頼化設計手法の研究:概念設計品質の最適化方法.起動過渡における故障シミュレーション
Author/Editor: 青木, 宏
田口, 秀之
倉谷, 尚志
岡井, 敬一
小島, 孝之
長谷川, 卓也
苅田, 丈士
Aoki, Hiroshi
Taguchi, Hideyuki
Kuratani, Naoshi
Okai, Keiichi
Kojima, Takayuki
Hasegawa, Takuya
Kanda, Takeshi
Author Heading: 青木, 宏
田口, 秀之
倉谷, 尚志
岡井, 敬一
小島, 孝之
長谷川, 卓也
苅田, 丈士
Aoki, Hiroshi
Taguchi, Hideyuki
Kuratani, Naoshi
Okai, Keiichi
Kojima, Takayuki
Hasegawa, Takuya
Kanda, Takeshi
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: Integrated design methodology for highly reliable liquid rocket engine: Optimizing process of concept design quality. Failure simulation at start trangent
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:宇宙輸送系基盤技術 = 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 Space Transportation Systems
No. or year of volume/issue: JAXA-SP-05-010
Volume: JAXA-SP-05-010
Pages: 25-30
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 宇宙輸送システム
液体推薬ロケットエンジン
ロケットエンジン設計
概念設計
設計最適化
シミュレーション
過渡応答
感度分析
制御弁
冗長性
space transportation system
liquid propellant rocket engine
rocket engine design
concept design
design optimization
simulation
transient response
sensitivity analysis
control valve
redundancy
Target Audience: 一般
Note (General): In past, the Design for Space Systems has conducted accumulating the optimum design results for each device. 'System Reliability Level' was measured as the results of long time development tests. Recently, the new design method is required. It is necessary to predict 'System Reliability Level' at Concept Design Phase, to grasp the distribution of 'Risks and Margins', to control 'Total Reliability Level' and to optimize 'Risk Distribution' because 'Attained Reliability Level depends on its basic Concept' consequently. This paper describes the results of study to measure 'Design Quality' unifying 'FMEA', 'FMECA', 'PRA', 'PDA' and 'Simulation Tools'. Some design parameters are picked up to understand where and how their dispersion makes an effect in the whole systems and to control the total system robustness.
資料番号: AA0049056005
レポート番号: JAXA-SP-05-010
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6236&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6236&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