低毒性一液推進剤の触媒点火特性向上のための添加物選定に関する実験的研究

Material type: 文書・図像類

Author: 伊藤, 尚義ほか

Publisher: 宇宙航空研究開発機構 (JAXA)

Publication date: 2024-01-30

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: This report introduces the experimental study on improving the catalytic ignition characteristics of green monopropellants for RCS thruster systems co...

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 Institutional Repositories DataBase(IRDB)(Institutional Repository) is linked at the site of Institutional Repositories DataBase(IRDB)(Institutional Repository).
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: 低毒性一液推進剤の触媒点火特性向上のための添加物選定に関する実験的研究
Author/Editor: 伊藤, 尚義
川端, 健心
早田, 和義
濁川, 淳
得丸, 翔平
勝身, 俊之
門脇, 敏
Author Heading: 伊藤, 尚義
川端, 健心
早田, 和義
濁川, 淳
得丸, 翔平
勝身, 俊之
門脇, 敏
Publication, Distribution, etc.: 宇宙航空研究開発機構 (JAXA)
Publication Date: 2024-01-30
Publication Date (W3CDTF): 2024-01-30
Alternative Title: Experimental Study on Improvement of Catalytic Ignition Characteristics of Green Monopropellant by Additive Materials
Periodical title: 宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 令和5年度研究成果報告書
No. or year of volume/issue: JAXA-RR-23-005
Volume: JAXA-RR-23-005
Pages: 13-16
ISSN (Periodical Title): EISSN : 2433-2216
Text Language Code: jpn
Subject Heading: Green Propellant
hydroxyl Ammonium Nitrate
Ammonium Dinitramide
Thruster Ignition
Atomization
Target Audience: 一般
Note (General): This report introduces the experimental study on improving the catalytic ignition characteristics of green monopropellants for RCS thruster systems conducted at Nagaoka University of Technology. Our group focuses on two candidates for green monopropellants: HAN (Hydroxyl ammonium nitrate)-based SHP163 propellants and ADN (Ammonium dinitramide)-based AMU propellants. To improve the catalytic ignition characteristics of those propellants, some additive materials are tested. Acetone was added to SHP163 to improve its atomization characteristics, and hydrogen peroxide was added to AMU631 to improve its combustion efficiency. The injection test of acetone-adding SHP163 revealed how the ambient density and the saturation vapor pressure of the propellant affect the breakup mechanism of propellant flow from the injector. The thruster combustion test of hydrogen peroxide-adding AMU631 revealed the influence of additive material on the combustion characteristics and appropriate hydrogen peroxide additive ratio.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
レポート番号: JAXA-RR-23-005
DOI: 10.20637/0002000217
Access Restrictions: インターネット公開
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