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A Study of N2O4/Amine Injector Elements Part 2 Combustion Test
https://jaxa.repo.nii.ac.jp/records/45166
https://jaxa.repo.nii.ac.jp/records/45166ee1da845-30f0-4eb1-955d-4d1124987641
名前 / ファイル | ライセンス | アクション |
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naltr00907.pdf (1.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | A Study of N2O4/Amine Injector Elements Part 2 Combustion Test | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | 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 | |||||
著者 |
熊谷, 達夫
× 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 |
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著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
日産自動車株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Nissan Motor Co., Ltd. | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-907 巻 907, p. 21, 発行日 1986-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0907000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-907 |