Development of Hybrid Kick-Motors for Share-Riding Small Space-Probes
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- NAGATA Harunori
- Hokkaido University
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- HIRAI Shota
- Letara Ltd.
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- KAMPS Landon
- Letara Ltd.
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- GALLO Giuseppe
- Hokkaido University
Bibliographic Information
- Other Title
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- 相乗り小型宇宙機用ハイブリッドキックモータの開発
Abstract
<p>The authors are developing a hybrid kick motor for small share-riding spacecraft. The authors launched the venture company Letara to commercialize hybrid kick motors in 2020. Critical technologies for practical use are fuel regression history prediction, nozzle erosion rate prediction, and ignition technology capable of re-ignition. This paper first describes why hybrid kick motors are necessary and how the authors started this development. The nitrous oxide the authors employed as a liquid oxidizer has a vapor pressure above the combustion chamber pressure. As a result, the combustion flow field changes according to the injection conditions, changing the axial distribution of the fuel regression velocity. The successful measurement of nozzle erosion rate history, which has been difficult in hybrid rockets, has allowed the authors to elucidate the mechanism of nozzle erosion. The introduction of a re-ignitable ignition system appropriate for small spacecraft with limited resources follows. Finally, the development status of a small-scale hybrid kick motor is presented.</p>
Journal
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- Journal of the Combustion Society of Japan
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Journal of the Combustion Society of Japan 66 (215), 9-15, 2024-02-15
Combustion Society of Japan
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Details 詳細情報について
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- CRID
- 1390581070839168512
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- ISSN
- 24241687
- 13471864
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- Text Lang
- ja
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- Data Source
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- JaLC
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- Abstract License Flag
- Disallowed