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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/10748/5990
http://hdl.handle.net/10748/5990e4baf154-07e0-4c4a-9963-dc85c16e481b
名前 / ファイル | ライセンス | アクション |
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10638-001.pdf (218.4 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2013-12-24 | |||||
タイトル | ||||||
言語 | en | |||||
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 | |||||
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 | |||||
著者 |
湯浅, 三郎
× 湯浅, 三郎× 北川, 幸樹 |
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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. 1-11, 発行日 2005 |
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ISSN | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 0911-551X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA10925183 | |||||
権利 | ||||||
権利情報 | 日本ロケット協会 | |||||
著者版フラグ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
出版者 | ||||||
出版者 | 日本ロケット協会 | |||||
資源タイプ | ||||||
内容記述タイプ | Other | |||||
内容記述 | Article | |||||
関係 | ||||||
関連タイプ | isVersionOf | |||||
識別子タイプ | DOI | |||||
関連識別子 | https://dx.doi.org/10.11230/jsts.21.1_1 |