Quantitative Evaluation of the Impulse-bit Generated in a Magnetic Thrust Chamber
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- INATOMI Taiki
- Kyushu University
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- MORITA Taichi
- Kyushu University
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- YAMAMOTO Naoji
- Kyushu University
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- NAKASHIMA Hideki
- Kyushu University
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- KOJIMA Tomihiko
- Kyushu University
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- KURAMOTO Eisuke
- Kyushu University
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- IKEBE Masaki
- Kyushu University
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- SUNAHARA Atsushi
- Purdue University Institute of Laser Engineering, Osaka University
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- NAMBA Shinichi
- Hiroshima University
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- MORI Yoshitaka
- The Graduate School for the Creation of New Photonics Industries
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- ISE Toshiyuki
- IHI AEROSPACE Co Ltd.
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- YAGI Kazuhiro
- IHI AEROSPACE Co Ltd.
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- JHOZAKI Tomoyuki
- Hiroshima University Institute of Laser Engineering, Osaka University
説明
<p>A magnetic thrust chamber is a component of a propulsion system which obtain thrust from a plasma in using a magnetic field. A laser fusion rocket has been assumed to use this system and will be used for interplanetary flight. To realize this rocket, we need to investigate the thrust performance of the magnetic thrust chamber. Previous work has investigated the plasma behaviour and thrust using simulations and experiments. However, quantitative comparison has not been much. In this work, we quantitatively compared computational and experimental results of plasma behaviour and performance. It was observed that the impulse bit increases as the magnetic field strength however, results from the experiment were approximately 3 times larger than that of simulation.</p>
収録刊行物
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- Journal of Evolving Space Activities
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Journal of Evolving Space Activities 1 (0), n/a-, 2023
宇宙技術および科学の国際シンポジウム
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詳細情報 詳細情報について
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- CRID
- 1390576844714555776
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- DOI
- 10.57350/jesa.4
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- ISSN
- 27581802
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- 本文言語コード
- en
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- データソース種別
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- JaLC
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- 抄録ライセンスフラグ
- 使用可