端面燃焼式ハイブリッドロケットにおける燃料後退特性の圧力依存性に関する実験的および解析的考察

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Material Type: 記事
Title: 端面燃焼式ハイブリッドロケットにおける燃料後退特性の圧力依存性に関する実験的および解析的考察
Author/Editor: 齋藤勇士
横井俊希
嶋田泰三
安河内裕之
添田建太郎
戸谷剛
脇田督司
永田晴紀
Author Heading: 齋藤勇士
横井俊希
嶋田泰三
安河内裕之
添田建太郎
戸谷剛
脇田督司
永田晴紀
Alternative Title: Experimental and Analytical Investigation of Effect of Pressure on Regression Rate of Axial-Injection End-Burning Hybrid Rockets
Periodical title: 年会講演会 = JSASS annual meeting
No. or year of volume/issue: 47:2016.4.14・15
Volume: 47
Pages: 9p
Publication date of volume/issue (W3CDTF): 2016-04
Publication (Periodical Title): [東京] : 日本航空宇宙学会
Place of Publication (Country Code): JP
Text Language Code: jpn
Subject Heading: Propulsion
Combustion
Hybrid Rocket
Regression Characteristics
Regression Model
NDLC: ZN25
Target Audience: 一般
Holding library: 国立国会図書館
Call No.: YH247-857
Data Provider (Database): 国立国会図書館 : 国立国会図書館雑誌記事索引
https://ndlsearch.ndl.go.jp
Bibliographic ID (NDL): 027289127
http://id.ndl.go.jp/bib/027289127
Bibliographic Record Category (NDL): 632