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N2O供給により燃焼制御が可能な硝酸アンモニウム/過塩素酸アンモニウム系固体推進薬の調製
https://doi.org/10.20637/JAXA-RR-18-006/0008
https://doi.org/10.20637/JAXA-RR-18-006/0008b4017f02-3897-4da7-92e9-b6b0b17deb3c
名前 / ファイル | ライセンス | アクション |
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AA1830031008.pdf (53.8 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 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | N2O供給により燃焼制御が可能な硝酸アンモニウム/過塩素酸アンモニウム系固体推進薬の調製 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Incombustible AN/AP-based propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | control of combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | N2O supply | |||||
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/JAXA-RR-18-006/0008 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Preparation of ammonium nitrate/ammonium perchlorate-based solid propellant for combustion control by N2O supply | |||||
著者 |
中迫, 友康
× 中迫, 友康× 東, 英子× 松永, 浩貴× 橘, 武史× 加藤, 勝美× Nakasako, Tomoyasu× Higashi, Eiko× Matsunaga, Hiroki× Tachibana, Takeshi× Kato, Katsumi |
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著者所属 | ||||||
福岡大学 | ||||||
著者所属 | ||||||
福岡大学 | ||||||
著者所属 | ||||||
福岡大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
福岡大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuoka University | ||||||
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: 平成30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 (2018) 巻 JAXA-RR-18-006, p. 49-55, 発行日 2019-02-28 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | N2O供給により燃焼をON/OFF制御できる非自律燃焼性(非自燃性)固体推進薬の調製を試み,その燃焼性を調査した.本研究では,スプレードライにより防湿処理を施した硝酸アンモニウム(AN)と過塩素酸アンモニウム(AP)を酸化剤とし,末端水酸基ポリブタジエン(HTPB)をバインダとした固体推進薬を調製した.HTPBを23.5 wt%とし,酸化剤中のAN/AP比を40/60,50/50,60/40 とした推進薬についてN2雰囲気0.3-6.0 MPa で燃焼試験を行ったところ,AN/AP=40/60 はすべての圧力範囲で燃焼が完結したが,50/50 および60/40 では0.5-0.7 MPa 以下で着火しなかった.これら2 種類の推進薬は,N2O供給下,0.3 MPa での燃焼試験では燃焼が持続し,N2O供給を止めると燃焼が停止したため,本実験で調製したAN/AP 系推進薬はN2O供給により燃焼をON/OFF制御できる可能性が示唆された. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this study, in an attempt to prepare propellants capable of on/off control of combustion by oxidizing gas supply, we prepared incombustible propellants in a N2 atmosphere composed of moisture-proof ammonium nitrate (AN) prepared by spray drying and ammonium perchlorate (AP) as oxidizers and hydroxyl-terminated polybutadiene (HTPB) as a fuel, and investigated their combustibility by N2O supply. The burning tests performed under a N2 atmosphere for the propellants having different AN/AP mass ratios (AN/AP = 40/60, 50/50, and 60/40) with 23.5 wt% HTPB revealed that the AN/AP=50/50 and 60/40 samples did not ignite under pressures less than 0.5-0.7 MPa, whereas the AN/AP=40/60 sample burned under the entire tested pressure range (0.3-6.0 MPa). Moreover, it was confirmed that the AN/AP=50/50 and 60/40 samples stably burned under N2O supply at 0.3 MPa. However, when the N2O supply was stopped, their combustion was interrupted with a little time delay, suggesting that combustion of the prepared propellants can be controlled by regulating the N2O supply. | |||||
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 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1830031008 | |||||
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-18-006 |