Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method

Shigeru Aso, Yasuhiro Tani, Masato Yamashita, Kazuya Komori, Tomohiro Yamasaki, Shohei Saiga, Ryohei Arakawa, Toru Shimada

研究成果: 著書/レポートタイプへの貢献会議での発言

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 20179 29 2017

出版物シリーズ

名前Proceedings of the International Astronautical Congress, IAC
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
オーストラリア
Adelaide
期間9/25/179/29/17

Fingerprint

hybrid rocket engines
throttling
liquid oxygen
vaporization
Rocket engines
Vaporization
engine
injection
Oxygen
Experiments
combustion
Swirling flow
swirling
Liquids
oxygen
combustion chambers
Combustion chambers
Rockets
rockets
experiment

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Astronomy and Astrophysics
  • Space and Planetary Science

これを引用

Aso, S., Tani, Y., Yamashita, M., Komori, K., Yamasaki, T., Saiga, S., ... Shimada, T. (2017). Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method. : 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security (pp. 8624-8628). (Proceedings of the International Astronautical Congress, IAC; 巻数 13). International Astronautical Federation, IAF.

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

Aso, S, Tani, Y, Yamashita, M, Komori, K, Yamasaki, T, Saiga, S, Arakawa, R & Shimada, T 2017, Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method. : 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. Proceedings of the International Astronautical Congress, IAC, 巻. 13, International Astronautical Federation, IAF, pp. 8624-8628, 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017, Adelaide, オーストラリア, 9/25/17.
Aso S, Tani Y, Yamashita M, Komori K, Yamasaki T, Saiga S その他. Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method. : 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).
Aso, Shigeru ; Tani, Yasuhiro ; Yamashita, Masato ; Komori, Kazuya ; Yamasaki, Tomohiro ; Saiga, Shohei ; Arakawa, Ryohei ; Shimada, Toru. / Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method. 68th International Astronautical Congress, IAC 2017: Unlocking Imagination, Fostering Innovation and Strengthening Security. International Astronautical Federation, IAF, 2017. pp. 8624-8628 (Proceedings of the International Astronautical Congress, IAC).
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