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Development of Flow Controller for LPG Arcjet Thruster
http://hdl.handle.net/10458/6801
http://hdl.handle.net/10458/68017c96722d-55aa-4bf9-a176-3400347638af
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
本文 (1.5 MB)
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| Item type | 会議発表論文 / Conference Paper(1) | |||||
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| 公開日 | 2020-06-21 | |||||
| タイトル | ||||||
| タイトル | Development of Flow Controller for LPG Arcjet Thruster | |||||
| 言語 | en | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| 資源タイプ | ||||||
| 資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
| 資源タイプ | conference paper | |||||
| 著者 |
S., Masui
× S., Masui× I, Kawagoe× N., Hidaka× T., Koiwaya |
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| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | An arcjet thruster is used to control an attitude and an orbit of Artificial satellites. A propellant of the arcjet thruster has used hydrazine(N2H4) as propellant from the viewpoint of the specific impulse and the reliability. However, hydrazine is high toxicity liquid. Thereby it is required that an arcjet thruster use green propellant, for example DME or LPG. We propose to apply LPG to a DC arcjet thruster. LPG, composed of butane(C4H10) and propane(C3H8), is non-toxic and non-reactive liquefied gas. Thus, the LPG arcjet thruster is more available than hydrazine arcjet thrusters. In this report, we discuss a development of a flow controller for the LPG arcjet thruster. The flow controller is combined a flow mater, Arduino and a solenoid valve. This reduce a cost because the flow controller is customized without an excessive performance. In the experiment, it is demonstratable that the flow controller is applicable to the LPG arcjet thruster. However, the LPG arcjet thruster is stopped by the soot. | |||||
| 言語 | en | |||||
| 書誌情報 |
en : International Conference on Science, Technology & Education (ICSTE 2016) p. 37-40, 発行日 2016-09 |
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| 著者版フラグ | ||||||
| 出版タイプ | VoR | |||||
| 出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
