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  1. 学術雑誌論文
  2. 5 技術(工学)

Time-resolved fuel regression measurement function of a hybrid rocket solid fuel integrated by multi-material additive manufacturing

http://hdl.handle.net/10228/0002000007
http://hdl.handle.net/10228/0002000007
848f13b2-e868-41da-926e-1f53a138e7af
名前 / ファイル ライセンス アクション
10366584.pdf 10366584.pdf (5.2 MB)
アイテムタイプ 学術雑誌論文 = Journal Article(1)
公開日 2023-07-24
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
タイトル
タイトル Time-resolved fuel regression measurement function of a hybrid rocket solid fuel integrated by multi-material additive manufacturing
言語 en
言語
言語 eng
著者 小澤, 晃平

× 小澤, 晃平

WEKO 23864
e-Rad 90801879
Scopus著者ID 56432040000
九工大研究者情報 100001001

en Ozawa, Kohei

ja 小澤, 晃平

ja-Kana オザワ, コウヘイ


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Wang, Han-wei

× Wang, Han-wei

en Wang, Han-wei

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Yoshino, Takuro

× Yoshino, Takuro

en Yoshino, Takuro

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坪井, 伸幸

× 坪井, 伸幸

WEKO 14118
e-Rad 40342620
Scopus著者ID 7007127548
九工大研究者情報 20

en Tsuboi, Nobuyuki

ja 坪井, 伸幸

ja-Kana ツボイ, ノブユキ


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抄録
内容記述タイプ Abstract
内容記述 The function of time-resolved fuel regression measurement is integrated into additively manufactured hybrid rocket fuels and conceptually demonstrated through the comparison with time-resolved optical fuel regression measurements during burns. This function is enabled by multi-material additive manufacturing of mainly thermoplastic solid fuels with a ladder-shaped resistor made of a conductive thermoplastic. This functionalization has many advantages, as indicated by its wide range of applicability, including solid fuel grains with emerging complex geometries, cost-effectiveness, ease of implementation, and minimal influence on the original propulsive performance and fuel regression behavior. Fuel regression is detected by a step change in the voltage applied to the ladder-shaped resistor, indicating the breakage of its top fuel surface rung during a burn. For ignited cases, all the rung breaks were detected, while the fuel regression was also optically measured using high-speed video. Errors were observed between the fuel regression time-histories measured using the two methods; however, most of these errors could be explained by the distribution of the fuel regression in the camera direction and the camera resolution and the melted fuel layer thickness. Considering these uncertainties, the remaining errors that could not be explained by these factors were less than ±0.15 mm, corresponding to ±1 layer of additive manufacturing applied to the prototyping of the solid fuels.
書誌情報 en : Acta Astronautica

巻 187, p. 89-100, 発行日 2021-06-29
出版社
出版者 Elsevier
DOI
識別子タイプ DOI
関連識別子 https://doi.org/10.1016/j.actaastro.2021.06.031
ISSN
収録物識別子タイプ EISSN
収録物識別子 1879-2030
ISSN
収録物識別子タイプ PISSN
収録物識別子 0094-5765
著作権関連情報
権利情報 Copyright (c) 2021 IAA. Published by Elsevier Ltd. All rights reserved
キーワード
主題Scheme Other
主題 Hybrid rockets
キーワード
主題Scheme Other
主題 Additive manufacturing
キーワード
主題Scheme Other
主題 Functional solid fuels
キーワード
主題Scheme Other
主題 Real-time regression measurements
出版タイプ
出版タイプ AM
出版タイプResource http://purl.org/coar/version/c_ab4af688f83e57aa
査読の有無
値 yes
研究者情報
URL https://hyokadb02.jimu.kyutech.ac.jp/html/100001001_ja.html
論文ID(連携)
値 10366584
連携ID
値 9005
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