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蠕動運動型混合搬送装置による固体推進薬の製造と燃焼試験
https://doi.org/10.20637/JAXA-RR-18-006/0006
https://doi.org/10.20637/JAXA-RR-18-006/0006eea2a778-f2e1-4f6c-a689-71c3da591f15
名前 / ファイル | ライセンス | アクション |
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AA1830031006.pdf (3.9 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 | 蠕動運動型混合搬送装置による固体推進薬の製造と燃焼試験 | |||||
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/JAXA-RR-18-006/0006 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Kneading of AP Composite Propellant by Peristaltic Muscle Mixer | |||||
著者 |
萩原, 大輝
× 萩原, 大輝× 芦垣, 恭太× 若松, 康太× 岩崎, 祥大× 野副, 克彦× 田上, 賢悟× 山田, 泰之× 羽生, 宏人× 中村, 太郎× Hagiwara, Daiki× Ashigaki, Kyota× Wakamatsu, Kota× Iwasaki, Akihiro× Nozoe, Katsuhiko× Tagami, Kengo× Yamada, Yasuyuki× Habu, Hiroto× Nakamura, Taro |
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著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所観測ロケット実験グループ(JAXA)(ISAS) | ||||||
著者所属 | ||||||
カーリットホールディングス株式会社 | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
東京電機大学 : 中央大学研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS) | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Sounding Rocket Research and Operation Group, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Carlit Holdings Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Denki University : Research and Development Initiative, Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo 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. 41-44, 発行日 2019-02-28 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 著者らは,固体ロケットモータの抜本的な低コスト化に向けて,蠕動運動型混合搬送装置を用いたコンポジット推進薬スラリの連続捏和技術の実現に取り組んできた.本報告では,連続化に向けた検討と,実組成の火薬材料を用いた捏和実験および燃焼試験について報告する.蠕動運動型混合搬送装置を,カーリットホールディングス株式会社の赤城工場にて設置し,1.65 kgの実組成火薬の捏和実験を行った.引張試験,ストランドバーナ試験などのラボレベルの性能試験に加えて,地上燃焼試験でその性能を評価した. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to drastically reduce the cost of solid rocket motors, we have been working on developing continuous kneading technology of composite propellant slurry using peristaltic motion type mixing and conveying equipment. In this report, we improve the equipment for continuousization. Then, a peristaltic motion type mixing and transporting device is installed at the Akagi Factory of Carlit HD Co., Ltd., and 1.65 kg of the actual composition powder is mixed. In addition to laboratory performance tests such as tensile tests and strand burner tests, the performance is confirmed in the ground burning test. | |||||
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: AA1830031006 | |||||
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 |