Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane

Kengo Ohe, Masato Mizuchi, Shigeru Aso, Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Hiroshi Tada, 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

3 引用 (Scopus)

抄録

Hybrid rocket engine with multi-section swirl injection method was designed and tested for the flight experiments of subscale space plane. Combustion experiments were carried out with high density polyethylene (HDPE) and paraffin fuel and gaseous oxygen with several combustion conditions. Fundamental data for flyable hybrid rocket including usefulness of high pressure CFRP oxygen tank have been revealed. Flight simulation using the measured thrust data clarified the reachable altitude and required thrust to future flight experiments.

元の言語英語
ホスト出版物のタイトル50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
出版者American Institute of Aeronautics and Astronautics Inc.
ISBN(電子版)9781624103032
DOI
出版物ステータス出版済み - 1 1 2014
イベント50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 - Cleveland, 米国
継続期間: 7 28 20147 30 2014

その他

その他50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
米国
Cleveland
期間7/28/147/30/14

Fingerprint

Rockets
Oxygen
Experiments
Carbon fiber reinforced plastics
Rocket engines
High density polyethylenes
Paraffins

All Science Journal Classification (ASJC) codes

  • Energy Engineering and Power Technology
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

これを引用

Ohe, K., Mizuchi, M., Aso, S., Tani, Y., Ohyama, S., Araki, K., ... Shimada, T. (2014). Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane. : 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014 American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2014-3954

Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane. / Ohe, Kengo; Mizuchi, Masato; Aso, Shigeru; Tani, Yasuhiro; Ohyama, Sho; Araki, Kentaro; Tada, Hiroshi; Shimada, Toru.

50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., 2014.

研究成果: 著書/レポートタイプへの貢献会議での発言

Ohe, K, Mizuchi, M, Aso, S, Tani, Y, Ohyama, S, Araki, K, Tada, H & Shimada, T 2014, Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane. : 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014, Cleveland, 米国, 7/28/14. https://doi.org/10.2514/6.2014-3954
Ohe K, Mizuchi M, Aso S, Tani Y, Ohyama S, Araki K その他. Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane. : 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc. 2014 https://doi.org/10.2514/6.2014-3954
Ohe, Kengo ; Mizuchi, Masato ; Aso, Shigeru ; Tani, Yasuhiro ; Ohyama, Sho ; Araki, Kentaro ; Tada, Hiroshi ; Shimada, Toru. / Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., 2014.
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