A Study of N2O4/Amine Injector Elements Part 2 Combustion Test

Material type: 文書・図像類

Author: 熊谷, 達夫ほか

Publisher: 航空宇宙技術研究所

Publication date: 1986-06

Material Format: Digital

Capacity, size, etc.: -

NDC: -

View All

Notes on use

Note (General)：: Effect of reactive stream separation on combustion performances were experimentally investigated by conducting firing tests of a N2O4/MMH propellant i...

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: A Study of N2O4/Amine Injector Elements Part 2 Combustion Test
Author/Editor: 熊谷, 達夫
毛呂, 明夫
日下, 和夫
木皿, 且人
阿部, 登
佐藤, 政裕
宮島, 博
小坂, 勝明
KUMAGAI, Tatsuo
MORO, Akio
KUSAKA, Kazuo
KISARA, Katsuto
ABE, Noboru
SATO, Masahiro
MIYAJIMA, Hiroshi
KOSAKA, Katsuaki
Author Heading: 熊谷, 達夫
毛呂, 明夫
日下, 和夫
木皿, 且人
阿部, 登
佐藤, 政裕
宮島, 博
小坂, 勝明
KUMAGAI, Tatsuo
MORO, Akio
KUSAKA, Kazuo
KISARA, Katsuto
ABE, Noboru
SATO, Masahiro
MIYAJIMA, Hiroshi
KOSAKA, Katsuaki
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1986-06
Publication Date (W3CDTF): 1986-06
Alternative Title: N2O4/アミンインジェクタエレメントの実験その2 燃焼試験結果
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-907
No. or year of volume/issue: 907
Volume: 907
Pages: 21-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: eng
Target Audience: 一般
Note (General): Effect of reactive stream separation on combustion performances were experimentally investigated by conducting firing tests of a N2O4/MMH propellant in a small scale combustion chamber with unlike doublet element injectors. Characteristics velocity efficiencies and specific impulses were parametrically obtained by varying the chamber pressure, the mixture ratio and the length of the combustion chamber. A distinct deterioration of the performance was observed in the region of the reactive stream separation correlated by Lawver. The most significant deterioration of the performance due to reactive stream separation occurs at a mixture ratio where otherwise the performance is at a peak.
資料番号: NALTR0907000
レポート番号: NAL TR-907
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