Výsledky vyhledávání - "惑星間宇宙機"

Autor: Ichikawa, Tsutomu, Kato, Takaji, Yoshikawa, Makoto, Takeuchi, Hiroshi

Publikováno v: 第7回宇宙科学シンポジウム = Proceedings of the 7th Space Science Symposium. :693-697

The navigation (Earth-based Orbit determination) technology have interest in examining the possibility of using one-way Doppler data alone to navigate interplanetary spacecraft. The one-way data can be formulated as the standard count Doppler or as p

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9adf8802fdde92eca40539918086192a
http://id.nii.ac.jp/1696/00011162/

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In-orbit operations of battery aboard HAYABUSA spacecraft: Second Report

Autor: Oto, Hiroki, Yamamoto, Masahiro, Eguro, Takashi, Sone, Yoshitsugu, Hirose, Kazuyuki, Tajima, Michio

Publikováno v: 第25回宇宙エネルギーシンポジウム平成17年度 = The Twenty-fifth Space Energy Symposium March 10, 2006. :6-10

Li ion batteries for space applications possess high discharge voltage, high specific energy, and lightweight properties, their research and development being conducted rapidly in recent years not only in the U.S. and France but also in Japan. Becaus

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::dee796d30fdda620f945ac3a8bb92130
http://id.nii.ac.jp/1696/00008062/

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The research on the next-generation ion engine

Autor: Hayakawa, Yukio, Okawa, Yasushi, Miyazaki, Katsuhiro, Yoshida, Hideki, Kitamura, Shoji

Publikováno v: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems. :129-134

This paper describes the status of the next-generation xenon-ion-engine research at ISTA (The Institute of Space Technology and Aeronautics). A set of ion extraction grids which would be ready for producing 200-mN thrust with a shorter aging period t

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d9c93c6c06d4f45fd10f4f3924784fab
http://id.nii.ac.jp/1696/00006276/

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磁気セイル探査機地上試験装置の開発

Autor: Shimizu, Yukio

The Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA) is studying a new magnetic sail propulsion system, called MagSail since 2002. A MagSail travels interplanetary space by capturing the energy of the s

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::93a3f19ab7f76924f4cf739f2c6b7fcd
http://id.nii.ac.jp/1696/00006274/

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BepiColombo, the Joint Japanese and European Mercury Exploration Program: The most recent status of Science Team. The updated status of BepiColombo/Mercury Magnetospheric Orbiter: FY2005

Autor: Hayakawa, Hajime, Kasaba, Yasumasa, Takashima, Takeshi, Yamakawa, Hiroshi, Ogawa, Hiroyuki, Sone, Yoshitsugu, Mukai, Toshifumi

Publikováno v: 第6回宇宙科学シンポジウム = Proceedings of the 6th Space Science Symposium. :514-521

BepiColombo計画は、JAXAが「水星磁気圏探査機・MMO(Mercury Magnetospheric Orbiter)」、ESAが「水星表面探査機・MPO(Mercury Planetary Orbiter)」を分担する初の本格的な日欧共同計画で、JAXAとESAの国際協力�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e2b6f2b3310f4fe07e692642cf1d0274
http://id.nii.ac.jp/1696/00011244/

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Experimental study of magnetic sails

Autor: Kojima, Hidenori, Minami, Tsubasa, Funaki, Ikko, Yamakawa, Hiroshi, Fujita, Kazuhisa, Ogawa, Hiroyuki, Nishida, Hiroyuki, Nakayama, Yoshinori

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: 9th Spacecraft Charging Technology Conference. :709-714

A magnetic sail is a unique propulsion system, which travels interplanetary space by capturing the energy of the solar wind. In order to simulate the interaction between the artificial magnetic field produced around a spacecraft and the solar wind, a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f2d96d1abba15a21b773e050079aee20
http://id.nii.ac.jp/1696/00006389/

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Development of magnetic sail simulator using an MPD arcjet

Autor: Kojima, Hidenori, Minami, Tsubasa, Funaki, Ikko, Nakayama, Yoshinori, Yamakawa, Hiroshi

Publikováno v: 第24回宇宙エネルギーシンポジウム平成16年度 = The Twenty-fourth Space Energy Symposium March 7, 2005. :97-100

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3006e3c0c339d723f4f7e7dbeb62717c
http://id.nii.ac.jp/1696/00008100/

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磁気プラズマセイル(MPS)の研究

Autor: Funaki, Ikko, Fujita, Kazuhisa, Yamakawa, Hiroshi, Ogawa, Hiroyuki, Nonaka, Satoshi, Asahi, Ryusuke, Nakayama, Yoshinori

Publikováno v: 宇宙航空研究開発機構特別資料: 宇宙インフラストラクチャ研究会宇宙環境計測技術WG:第6回宇宙飛翔体環境研究会報告書 = JAXA Special Publication: Proceedings of the 6th Spacecraft Environment Research Network Meeting. :68-71

A magnetic sail is the way to propel a spacecraft by the solar wind in the interplanetary space. Although original concept of the magnetic sail depends solely on very large magnetic field generated by using such device as superconductors coil, in 200

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::91bdbaf41bef4f3eb03a111b78ed5df6
http://id.nii.ac.jp/1696/00006652/

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惑星探査機の軌道決定に対するノンコヒーレントドップラーデータの一適用

Autor: Ichikawa, Tsutomu

Publikováno v: 平成15年度アストロダイナミクスシンポジウム:講演後刷り集 = ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers. :254-259

惑星探査機の軌道決定(電波航法)においては、精度に限界があるが地上局で取得する2-wayのレンジ・ドップラーを観測量として用いており安定した結果が得られている。そこでドップラー

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d063c64fd679ac7a9b2ca84e35f5af38
http://id.nii.ac.jp/1696/00007736/

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