H-2Aロケットフェアリング断熱材の施工工程改善

Material type: 文書・図像類

Author: 馬場, 尚子ほか

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)：: H-2A launch vehicle general review revealed reduction in strength of thermal insulator on the fairing. Sealant which adheres sheet insulator was found...

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: H-2Aロケットフェアリング断熱材の施工工程改善
Author/Editor: 馬場, 尚子
石澤, 淳一郎
南, 伸太朗
島村, 宏之
今川, 吉郎
宇治野, 功
松永, 浩史
土橋, 昭彦
大坊, 俊彰
Baba, Naoko
Ishizawa, Junichiro
Minami, Shintaro
Shimamura, Hiroyuki
Imagawa, Kichiro
Ujino, Takumi
Matsunaga, Hiroshi
Tsuchihashi, Akihiko
Daibo, Toshiaki
Author Heading: 馬場, 尚子
石澤, 淳一郎
南, 伸太朗
島村, 宏之
今川, 吉郎
宇治野, 功
松永, 浩史
土橋, 昭彦
大坊, 俊彰
Baba, Naoko
Ishizawa, Junichiro
Minami, Shintaro
Shimamura, Hiroyuki
Imagawa, Kichiro
Ujino, Takumi
Matsunaga, Hiroshi
Tsuchihashi, Akihiko
Daibo, Toshiaki
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: Process improvement for thermal insulator on the fairing of H-2A launch vehicle
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: 115-120
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 断熱材
H-2Aロケット
フェアリング
複合材料
硬化
熱真空試験
シリコーンシーラント
シリカマイクロバルーン
thermal insulator
H-2A rocket
fairing
composite material
curing
thermal vacuum test
silicone sealant
silica microballoon
Target Audience: 一般
Note (General): H-2A launch vehicle general review revealed reduction in strength of thermal insulator on the fairing. Sealant which adheres sheet insulator was found incurable also. Mechanical tests and SEM (Scanning Electron Microscope) observations suggested that incomplete mixing of the raw materials was the reason of lower strength due to degraded uniformity of the insulator. By improving mixing process, well performed, firm insulator was achieved. Evaluation of cure processes proved that alcohol released during insulator cure obstructed hardening of sealant resulting in insufficient cure time. Adequate cure time assured reduced alcohol release and mature vulcanization of sealant. The process was improved based on these findings, and this resulted in more reliable insulator.
資料番号: AA0049056023
レポート番号: JAXA-SP-05-010
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6254&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6254&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