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加熱反応試験による低毒性推進剤に関する燃焼特性評価
https://doi.org/10.20637/00047349
https://doi.org/10.20637/0004734952455518-4c37-450d-96e8-258d652f8ad3
名前 / ファイル | ライセンス | アクション |
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AA2030016003.pdf (4.4 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 | 2021-02-10 | |||||
タイトル | ||||||
タイトル | 加熱反応試験による低毒性推進剤に関する燃焼特性評価 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | |||||
ID登録 | ||||||
ID登録 | 10.20637/00047349 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Evaluation of Green Monopropellant Combustion Characteristics by Heat Reaction Test | |||||
著者 |
尾松, 来基
× 尾松, 来基× 半澤, 佳祐× 伊藤, 尚義× 勝身, 俊之× 門脇, 敏× OMATSU, Raiki× HANZAWA, Keisuke× ITO, Hisayoshi× KATSUMI, Toshiyuki× KADOWAKI, Satoshi |
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著者所属 | ||||||
長岡技術科学大学 | ||||||
著者所属 | ||||||
長岡技術科学大学 | ||||||
著者所属 | ||||||
長岡技術科学大学 | ||||||
著者所属 | ||||||
長岡技術科学大学 | ||||||
著者所属 | ||||||
長岡技術科学大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Nagaoka University of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nagaoka University of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nagaoka University of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nagaoka University of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Nagaoka University of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
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2年度研究成果報告書 en : JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2020) 巻 JAXA-RR-20-007, p. 9-13, 発行日 2021-02-10 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hydrazine has been used as a propellant in monopropellant thrusters for the spacecraft attitude control, but due to its high toxicity, research on low-toxic monopropellants based on Ammonium Dinitramide (ADN) and Hydroxylammonium Nitrate (HAN) has become active in recent years. Since these low-toxicity propellants contain oxidant components and have high combustion temperatures, there is an urgent need to develop a catalyst and combustion control technologies with high thermal resistance. Therefore, we wondered if the kick-off temperature could be controlled by using a catalyst. In this study, combustion tests of ADN-based low toxicity propellants (from now on will be referred as AMU-based) were carried out to understand the basic combustion characteristics of the propellants using a droplet heating and combustion tester. In the test, we designed and manufactured a droplet heating combustion test device, and worked on the acquisition of combustion characteristics using a catalyst to confirm the reactivity of the propellant in each temperature range. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2216 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2030016003 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-20-007 |