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Current Status of Rocket Developments in Universities -Development of a Small Hybrid Rocket with a Swirling Oxidizer Flow Type Engine
http://hdl.handle.net/10228/00008464
http://hdl.handle.net/10228/00008464d2b6ef0a-4401-482f-ab42-6cdb2ebd9a6f
名前 / ファイル | ライセンス | アクション |
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jsts.21.1_1.pdf (1.6 MB)
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Item type | 学術雑誌論文 = Journal Article(1) | |||||||||||
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公開日 | 2021-09-15 | |||||||||||
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 | Current Status of Rocket Developments in Universities -Development of a Small Hybrid Rocket with a Swirling Oxidizer Flow Type Engine | |||||||||||
言語 | ||||||||||||
言語 | eng | |||||||||||
著者 |
Yuasa, Saburo
× Yuasa, Saburo× 北川, 幸樹
WEKO
23865
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抄録 | ||||||||||||
内容記述タイプ | Abstract | |||||||||||
内容記述 | To develop an experimental small hybrid rocket with a swirling gaseous oxygen flow type engine, we made a flight model engine. Burning tests of the engine showed that a maximum thrust of 692 N and a specific impulse of 263 s (at sea level) were achieved. We designed a small hybrid rocket with this engine. The rocket measured 1.8 m in length and 15.4 kg in mass. To confirm the flight stability of the rocket, wind tunnel tests using a 112-scale model of the rocket and simulations of the flight attitude and trajectory were carried out. A flight test was conducted at Taiki-cho, Hokkaido, Japan on March 2001. The rocket reached an altitude of about 600 m, thus recording the first successful flight of a hybrid rocket in Japan. For the next stage, future issues to develop larger hybrid rockets using a swirling liquid oxygen flow type engine are discussed, and preliminary burning tests of the engine have been carried out. | |||||||||||
書誌情報 |
The Journal of Space Technology and Science 巻 21, 号 1, p. 1_1-1_11, 発行日 2005 |
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出版社 | ||||||||||||
出版者 | 日本ロケット協会 | |||||||||||
DOI | ||||||||||||
関連タイプ | isIdenticalTo | |||||||||||
識別子タイプ | DOI | |||||||||||
関連識別子 | https://doi.org/10.11230/jsts.21.1_1 | |||||||||||
日本十進分類法 | ||||||||||||
主題Scheme | NDC | |||||||||||
主題 | 538 | |||||||||||
NCID | ||||||||||||
収録物識別子タイプ | NCID | |||||||||||
収録物識別子 | AA10925183 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | ISSN | |||||||||||
収録物識別子 | 2186-4772 | |||||||||||
ISSN | ||||||||||||
収録物識別子タイプ | ISSN | |||||||||||
収録物識別子 | 0911-551X | |||||||||||
著作権関連情報 | ||||||||||||
権利情報 | Copyright (c) 2005 Japanese Rocket Society | |||||||||||
キーワード | ||||||||||||
主題Scheme | Other | |||||||||||
主題 | Hybrid Rocket | |||||||||||
出版タイプ | ||||||||||||
出版タイプ | VoR | |||||||||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||||||||
査読の有無 | ||||||||||||
値 | yes | |||||||||||
研究者情報 | ||||||||||||
表示名 | https://hyokadb02.jimu.kyutech.ac.jp/html/100001324_ja.html | |||||||||||
URL | https://hyokadb02.jimu.kyutech.ac.jp/html/100001324_ja.html | |||||||||||
論文ID(連携) | ||||||||||||
値 | 10380598 | |||||||||||
連携ID | ||||||||||||
値 | 9274 |