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固体推進薬の捏和へ向けた蠕動運動型混合搬送機Mark. IIIの開発と性能評価
https://doi.org/10.20637/JAXA-RR-17-008/0009
https://doi.org/10.20637/JAXA-RR-17-008/0009eea3123b-4a8c-451d-a264-2ae145ff2a1f
名前 / ファイル | ライセンス | アクション |
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AA1730012009.pdf (2.0 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 | 2018-02-06 | |||||
タイトル | ||||||
タイトル | 固体推進薬の捏和へ向けた蠕動運動型混合搬送機Mark. IIIの開発と性能評価 | |||||
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/JAXA-RR-17-008/0009 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development and performance evaluation of peristaltic mixing transporter Mark. III for continuous kneading of solid propellant | |||||
著者 |
芦垣, 恭太
× 芦垣, 恭太× 山田, 泰之× 岩崎, 祥大× 松本, 幸太郎× 羽生, 宏人× 中村, 太郎× Ashigaki, Kyota× Yamada, Yasuyuki× Iwasaki, Akihiro× Matsumoto, Kotaro× 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 | ||||||
総合研究大学院大学(SOKENDAI) | ||||||
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 | ||||||
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 | ||||||
The Graduate University for Advanced Studies (SOKENDAI) | ||||||
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 | ||||||
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29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 (2017) 巻 JAXA-RR-17-008, p. 57-60, 発行日 2018-01-10 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 我々は固体ロケットモータの低コスト化に向け蠕動運動型混合搬送機による推進薬スラリの連続捏和に取り組んできた. これまでに本装置を用いて捏和した推進薬スラリが従来のプラネタリミキサで捏和した推進薬と同等の性能であることを燃焼実験にて確認した. 次の目標は実際のロケットモータ製造に向けた生産効率, 安全性, 品質である. 本論文ではその第一段階として動作速度, 加温性能の向上, 材料投入方法の改善した新型蠕動運動型混合搬送機を開発し模擬推進薬スラリの捏和からその性能向上を確認した. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We have studied the continuous mixing of propellant slurry with peristaltic mixing transporter to reduce the cost of a solid rocket motor. In the previous study, we confirmed that the propellant slurry mixed with peristaltic mixing transporter had the same performance as a planetary mixer in combustion experiment. The next target is the production efficiency, safety, and quality for actual rocket motor manufacturing. In this paper, as a first step of the target, we report that we developed a new peristaltic mixing transporter with improved motional speed, heating performance and material input. And we confirmed its performance improvement from mixing of simulated propellant slurry. | |||||
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: AA1730012009 | |||||
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-17-008 |