Výsledky vyhledávání - "プラズマ推進"

Present status and future prospect of the VASIMR type plasma thruster

Autor: Ando, Akira, Hattori, Kunihiko, Inutake, Masaaki

Publikováno v: 宇宙航空研究開発機構特別資料: 2005年度宇宙関連プラズマ研究会講演集 = JAXA Special Publication: Proceedings of Space Plasma Symposium 2005. :64-69

有人火星探査を目指した高性能の比推力可変電気推進機VASIMR(Variable Specific Impulse Magnetoplasma Rocket)がNASAを中心に提案され実用化研究が進められている。このシステムでは一定電力下で自由

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::727031cc7bb357ea38763079097f0b7a
http://id.nii.ac.jp/1696/00006112/

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A proposal of laboratory simulation of a magneto-plasma sail

Autor: MPS研究会, Minami, Tsubasa, Funaki, Ikko, Kojima, Hidenori, Yamakawa, Hiroshi, Nakayama, Yoshinori, Ogawa, Hiroyuki, Magneto Plasma Sail Research Group

Publikováno v: スペース・プラズマ研究会平成16年度 = Space Plasma Conference FY2004. :64-67

資料番号: AA0063347018

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::dde0001086aeb9119376d7bc8458fd5d
http://id.nii.ac.jp/1696/00012693/

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Analysis of propulsion performance of a microwave excitation micro plasma thruster

Autor: Takao, Yoshinori, Ono, Koichi, Takahashi, Kazuo, Setsuhara, Yuichi

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :304-307

資料番号: AA0047118075

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::166d77b3ea69e7c9c0effd93032b0522
http://id.nii.ac.jp/1696/00017299/

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Basic research on a forward-acceleration-type laser plasma thruster

Autor: Oyaizu, Keishi, Kuramoto, Hideaki, Izumi, Masaya, Horisawa, Hideyuki, Kimura, Itsuro

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :332-335

資料番号: AA0047118082

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9ab6b2d7c870ff06710d8f01fc413cf8
http://id.nii.ac.jp/1696/00017306/

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磁気セイルの地上シミュレータの構築

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

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :276-279

To realize magnetic sails, momentum of the solar wind should be efficiently transferred to a spacecraft via magnetic field, which is produced around a spacecraft. In this paper, two important physical processes are addressed: 1) diffusive processes c

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7dbfa1fce019ad7401455e45a07da23f
http://id.nii.ac.jp/1696/00017292/

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Evaluation of basic characteristics of a Mach probe for plasma flow measurement

Autor: Watanabe, Toshiaki, Watanabe, Takashi, Tobari, Hiroyuki, Hattori, Kunihiko, Ando, Akira, Inutake, Masaaki

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :352-355

資料番号: AA0047118087

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b655888e198138bd44f9c1f5f873a6d6
http://id.nii.ac.jp/1696/00017311/

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Plasma behavior of a laser-driven pulse plasma thruster and measurement of thrust performance

Autor: Kawakami, Masatoshi, Horisawa, Hideyuki, Kimura, Itsuro

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :400-403

資料番号: AA0047118099

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a545d301164687e5241807e8828c5040
http://id.nii.ac.jp/1696/00017323/

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Plasma properties of a multi-purpose, large capacity and high density helicon source

Autor: Shinohara, Shunjiro, Tanikawa, Takao

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :296-299

資料番号: AA0047118073

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0808b32a7435527cf4bacc2e1672fb53
http://id.nii.ac.jp/1696/00017297/

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MagnetoPlasma Sailの電磁流体解析

Autor: Funaki, Ikko, Yamakawa, Hiroshi, Fujita, Kazuhisa, Ogawa, Hiroyuki, Nonaka, Satoshi, Sawai, Shujiro, Kuninaka, Hitoshi, Otsu, Hirotaka

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :312-315

In 2001, Winglee et al. proposed an efficient in-space propulsion system, which realizes a huge magnetic field around a spacecraft with an assistance of plasma emission. From their theoretical analysis of what they call mini-magnetospheric plasma pro

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7394236f5ea34843cb273a6c7b713ac0
http://id.nii.ac.jp/1696/00017408/

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