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HYPERGOLIC IGNITION MECHANISM OF HYDRAZINE/NITROGEN TETROXIDE CO-FLOWING JETS AT LOW TEMPERATURES
https://jaxa.repo.nii.ac.jp/records/22541
https://jaxa.repo.nii.ac.jp/records/22541ba250fec-0a28-437d-938e-eb312ab1edc9
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-07-07 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | HYPERGOLIC IGNITION MECHANISM OF HYDRAZINE/NITROGEN TETROXIDE CO-FLOWING JETS AT LOW TEMPERATURES | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypergolic ignition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hydrazine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nitrogen tetroxide | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | detailed chemical reaction | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
Tani, Hiroumi
× Tani, Hiroumi× Terashima, Hiroshi× Daimon, Yu× Koshi, Mitsuo |
|||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
出版者(英) | ||||||
出版者 | Begell House | |||||
書誌情報 |
en : International Journal of Energetic Materials and Chemical Propulsion 巻 14, 号 1, p. 71-84, 発行日 2015 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hydrazine (N2H4)/nitrogen tetroxide (NTO) co-flowing jets were simulated to explore the hypergolic ignition processes in N2H4/NTO bipropellant thrusters. The Navier−Stokes equations with a detailed chemical kinetics mechanism were solved by direct numerical simulation to reveal the influence of the distinct chemical reaction; i.e., hydrogen abstraction by nitrogen dioxide (NO2). In the ignition processes, the hydrogen abstraction sequence, especially the reaction of N2H3 and NO2, played a significant role in preheating the mixture gases and it was significant in the NTO-rich conditions rather than in the specifically stoichiometric conditions. Thus, in the N2H4/NTO co-flowing jets, the preheated regions correspond to the regions where the NTO-rich flows existed and contacted the N2H4 jet. The ignition eventually occurred in the region where NTO has sufficient concentration. Hence, it was found that the ignition timing and position strongly depend on whether the unsteady behavior of the NTO jet provides appropriate environments for the hydrogen abstraction reactions. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2150-766X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA12707900 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.1615/IntJEnergeticMaterialsChemProp.2015011276 | |||||
関連名称 | info:doi/10.1615/IntJEnergeticMaterialsChemProp.2015011276 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1510040000 |