Large-Scale CAMUI Type Hybrid Rocket Motor Scaling, Modeling, and Test Results

Viscor, Tor; Kamps, Landon; Yonekura, Kazuo et al.

Aerospace, 2022, 9(1), 1

Permalink : https://hdl.handle.net/2115/84182

このアイテムのアクセス数:369件（2026-01-15 11:03 集計）

ファイル	フォーマット	サイズ	閲覧回数	説明
https://doi.org/10.3390/aerospace9010001

アクセス権	metadata only access
URI	https://hdl.handle.net/2115/84182
タイトル	Large-Scale CAMUI Type Hybrid Rocket Motor Scaling, Modeling, and Test Results
著者	Viscor, Tor ; Kamps, Landon ; Yonekura, Kazuo ; Isochi, Hikaru ; Nagata, Harunori
著者名 Viscor, Tor
著者名 Kamps, Landon
著者名 Yonekura, Kazuo
著者名 Isochi, Hikaru
e-Rad_Researcher 40281787 著者名 Nagata, Harunori
言語	英語
キーワード	commercialization
	hybrid rocket
	CAMUI
	modeling
発行日	2022-01
出版者	MDPI
収録物名	Aerospace
巻(号)	9(1)
ページ	1
抄録	An understanding of the scalability of hybrid rocket regression models is critical for the enlargement and commercialization of small-scale engines developed within universities and similar research institutions. This paper investigates the fuel regression rates of recent 40 kN thrust-class motor experiments, which were designed based on fuel regression rate correlations of 2.5 kN thrust-class motors from previous research. The results show that fuel regression rates of the 40 kN experiments were within 26% of predictions made using correlations based on 2.5 kN experiments.
資源タイプ	学術雑誌論文
出版タイプ	Version of Record
PISSN	2226-4310
関連情報 (isIdenticalTo)	出版社版DOI https://doi.org/10.3390/aerospace9010001