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A Concept of the Small Chemical Thruster with High Energetic Ionic Liquids

Autor: ITOUYAMA, Noboru, WADA, Asato, HABU, Hiroto

Publikováno v: 宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 令和3年度研究成果報告書 = JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2021). :6-8

アンモニウムジニトラミドを基材とするイオン液体系推進剤 (ADN-EILPs) は，低毒・高密度比推力が期待される有望な一液推進剤の一つである．これまで筆者らは，ADN-EILPs が内包する点火�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::96d12ccb8fa9dd389232f063e30a24cf
http://id.nii.ac.jp/1696/00048269/

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Report of main combustion test for material of deployable nozzle

Autor: TAKEUCHI, Shinsuke, KITAGAWA, Koki, TOKUDOME, Shinichiro, TOBE, Hirobumi, ARAKAWA, Satoshi, MOCHIHARA, Yoshitaka, SUZUKI, Naohiro, YOSHINAKA, Toshinari, MORISHITA, Naoki, IWASAKI, Akihiro, IWABUCHI, Shota, WADA, Asato

Publikováno v: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report. :1-51

本報告書は、2020年1月20日から同年2月4日にかけてJAXA宇宙科学研究所あきるの実験施設において実施した「展開ノズル材耐熱試験本試験」の試験目的から得られた実験データまでをまとめ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::5283d87f56f4272282fcbdc97df7ec68
http://id.nii.ac.jp/1696/00047380/

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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

Publikováno v: 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

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) sys

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::47ef6b13d4139f68dabe655024b5b6f2
http://id.nii.ac.jp/1696/00047358/

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宇宙探査に向けた小電力ホールスラスタの研究

Autor: WATANABE, Hiroki, WADA, Asato, TSUKIZAKI, Ryudo, IKEDA, Tomoyuki

Research and development of low-power Hall thruster system is important for the realization of space explorations using micro spacecrafts. In this paper, technical problems for the development of low-power Hall thruster system was discussed based on

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::205658e909ce19aea7c3b99d44e8e8ce
http://id.nii.ac.jp/1696/00047357/

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Technical Report of the Research Activity for Innovative Micro Propulsion Systems for Future Deep Space Explorations (2020)

Autor: WADA, Asato, WATANABE, Hiroki, TSUKIZAKI, Ryudo, IKEDA, Tomoyuki, IIZUKA, Toshiaki, SAHARA, Hironori, KAKAMI, Akira, ITOUYAMA, Noboru, MATSUNAGA, Hiroki

Publikováno v: 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report. :1-19

形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA2030017000
レポート番号: JAXA-RR-20-008

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8e78015a76873ad0c947ee683a4f8f1e
http://id.nii.ac.jp/1696/00047355/

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Study on Innovative Micro-Propulsion System Technologies for Micro-Space Probes

Autor: WADA, Asato, WATANABE, Hiroki, ITOUYAMA, Noboru, TSUKIZAKI, Ryudo, IKEDA, Tomoyuki, IIZUKA, Toshiaki, SAHARA, Hironori, KAKAMI, Akira, MATSUNAGA, Hiroki, IZATO, Yuichiro, SHIOTA, Kento, MATSUMOTO, Kotaro, KATSUMI, Toshiyuki, MIYAKE, Atsumi, KASAHARA, Jiro, SHIDA, Maki, FUNASE, Ryu, FUNAKI, Ikko, HABU, Hiroto

For the implementation of future space science missions at the father away from Earth, it is necessary to build the technological platforms for performing various challenging missions with high frequency and to mature the technology, and breakthrough

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::25085a3d676f53ff1294b584429431c3
http://id.nii.ac.jp/1696/00047356/

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