抄録
A new hybrid rocket combustion method which can improve the fuel regression rate more than that of conventional method. The new method is named as Multi-Section Swirl Injection Method, which generates swirling flows at some cross-sections in combustion chamber. Combustion experiments with carefully tuned oxygen injections to keep each O/F at optimum value has been successfully conducted. Also throttling experiments, vaporization experiments of liquid oxygen, flight experiments with multi-section swirl injection method have been successfully. The results shows proposed method of vaporization of liquid oxygen is useful and also hybrid rocket engine with Multi-Section Swirl Injection Method can operate with acceleration environment.
| 元の言語 | 英語 |
|---|---|
| ホスト出版物のタイトル | 68th International Astronautical Congress, IAC 2017 |
| ホスト出版物のサブタイトル | Unlocking Imagination, Fostering Innovation and Strengthening Security |
| 出版者 | International Astronautical Federation, IAF |
| ページ | 8624-8628 |
| ページ数 | 5 |
| ISBN（印刷物） | 9781510855373 |
| 出版物ステータス | 出版済み - 1 1 2017 |
| イベント | 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017 - Adelaide, オーストラリア 継続期間: 9 25 2017 → 9 29 2017 |
出版物シリーズ
| 名前 | Proceedings of the International Astronautical Congress, IAC |
|---|---|
| 巻 | 13 |
| ISSN（印刷物） | 0074-1795 |
その他
| その他 | 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017 |
|---|---|
| 国 | オーストラリア |
| 市 | Adelaide |
| 期間 | 9/25/17 → 9/29/17 |
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All Science Journal Classification (ASJC) codes
- Aerospace Engineering
- Astronomy and Astrophysics
- Space and Planetary Science
これを引用
Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method. / Aso, Shigeru; Tani, Yasuhiro; Yamashita, Masato; Komori, Kazuya; Yamasaki, Tomohiro; Saiga, Shohei; Arakawa, Ryohei; Shimada, Toru.
68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, 2017. p. 8624-8628 (Proceedings of the International Astronautical Congress, IAC; 巻 13).研究成果: 著書/レポートタイプへの貢献 › 会議での発言
}
TY - GEN
T1 - Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method
AU - Aso, Shigeru
AU - Tani, Yasuhiro
AU - Yamashita, Masato
AU - Komori, Kazuya
AU - Yamasaki, Tomohiro
AU - Saiga, Shohei
AU - Arakawa, Ryohei
AU - Shimada, Toru
PY - 2017/1/1
Y1 - 2017/1/1
N2 - A new hybrid rocket combustion method which can improve the fuel regression rate more than that of conventional method. The new method is named as Multi-Section Swirl Injection Method, which generates swirling flows at some cross-sections in combustion chamber. Combustion experiments with carefully tuned oxygen injections to keep each O/F at optimum value has been successfully conducted. Also throttling experiments, vaporization experiments of liquid oxygen, flight experiments with multi-section swirl injection method have been successfully. The results shows proposed method of vaporization of liquid oxygen is useful and also hybrid rocket engine with Multi-Section Swirl Injection Method can operate with acceleration environment.
AB - A new hybrid rocket combustion method which can improve the fuel regression rate more than that of conventional method. The new method is named as Multi-Section Swirl Injection Method, which generates swirling flows at some cross-sections in combustion chamber. Combustion experiments with carefully tuned oxygen injections to keep each O/F at optimum value has been successfully conducted. Also throttling experiments, vaporization experiments of liquid oxygen, flight experiments with multi-section swirl injection method have been successfully. The results shows proposed method of vaporization of liquid oxygen is useful and also hybrid rocket engine with Multi-Section Swirl Injection Method can operate with acceleration environment.
UR - http://www.scopus.com/inward/record.url?scp=85051484377&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85051484377&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85051484377
SN - 9781510855373
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 8624
EP - 8628
BT - 68th International Astronautical Congress, IAC 2017
PB - International Astronautical Federation, IAF
ER -