Trade-Off Evaluation of the Integration Propulsion Systems for Space Explorations
| Autor: | WADA, Asato, IIZUKA, Toshiaki, SAHARA, Hironori, KAKAMI, Akira, WATANABE, Hiroki, FUNASE, Ryu, HABU, Hiroto |
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| Jazyk: | japonština |
| Rok vydání: | 2021 |
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| Zdroj: | 宇宙航空研究開発機構研究開発報告: 将来深宇宙探査に向けた革新的超小型推進系研究グループ 2020年度研究成果報告書 = JAXA Research and Development Report: Technical Report of the Research Activity for Innovative Micro Propulsion Systems for Future Deep Space Explorations (2020). :13-19 |
| ISSN: | 2433-2216 |
| Popis: | In order to obtain the exploration flexibility by the propulsion control technology of the micro-spacecraft, it is important to optimize the propulsion system. The objective of this paper is evaluated the trade-off of the chemical propulsion (CP) systems, the electric propulsion (EP) systems, and the combined CP and EP systems with shared propellant for 100 kg-class micro-spacecraft. As a result, it was confirmed that the effectiveness of combined CP and EP system with shared the high energetic propellant was clarified. In addition, at the higher thruster operation ratio for reaction control, it is necessary that the thruster performance is improved by using the higher thermal potential propellant. At the higher delta-V for orbit maneuver, it was confirmed that the integration propulsion systems of the higher thrust density are validity. 形態: カラー図版あり Physical characteristics: Original contains color illustrations 資料番号: AA2030017003 レポート番号: JAXA-RR-20-008 |
| Databáze: | OpenAIRE |
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