Výsledky vyhledávání

Micrometeoroid impact on ceramic thin components for interplanetary probe

Autor: K. Okudaira, Y. Motoyashiki, Eiichi Sato, Sunao Hasegawa

Publikováno v: International Journal of Impact Engineering. 35:1666-1671

A new advanced ceramic thruster made of monolithic silicon nitride (Si3N4) is under development for the next interplanetary probe of PLANET-C Venus exploration mission in Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploratio

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::610c46fab57f0b9361f5210be4c76b1f
https://doi.org/10.1016/j.ijimpeng.2008.07.051

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Uncooled mid-infrared camera onboard a Venus probe

Autor: Taguchi, Makoto, Imamura, Takeshi, Nakamura, Masato, Iwagami, Naomoto, Ueno, Munetaka

Publikováno v: 大気圏シンポジウム第18回平成15年度 = Atmospheric Science Symposium the 18th 2003. :49-52

資料番号: AA0046920015

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c43ecea15bbcc3c138968e026995b880
http://id.nii.ac.jp/1696/00019740/

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Study on scientific satellite power supply systems using PPT control systems

Autor: Tazawa, Takashi, Yoshida, Teiji, Takahashi, Keiji, Ichikawa, Tsutomu, Tajima, Michio

Publikováno v: 第22回宇宙エネルギーシンポジウム平成14年度 = The 22nd ISAS Space Energy Symposium March 12, 2003. :6-10

There are various power supply systems for scientific satellite applications. They must be properly used according to the feature of satellite missions. In most of the power supply systems for domestic satellites, the upper limit voltage control has

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::259ea7253c0763555e91cbebeb54adec
http://id.nii.ac.jp/1696/00008146/

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Venus entry capsule: From entry to balloon release

Autor: Yamada, Tetsuya, Hiraki, Koju, Izutsu, Naoki, Morita, Yasuhiro, Honda, Masahisa

Publikováno v: 第3回宇宙科学シンポジウム = Proceedings of the 3rd Space Science Symposium. :105-108

金星に水蒸気気球を浮遊させ大気観測を行なうミッションを想定し、惑星間遷移軌道から金星突入を行い、高度45kmに観測気球を放出する小型金星カプセルの研究を行なっている。満膨張

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e5a0f91a2fdb92439c85a46217e648fc
http://id.nii.ac.jp/1696/00011627/

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Launching and floating of a Venus probe balloon onboard a solar sail experiment satellite

Autor: Izutsu, Naoki, Yamada, Tetsuya, Honda, Hideyuki, Yajima, Nobuyuki, Hiraki, Koju, Imamura, Takeshi, Yamada, Yukio, Honda, Masahisa

Publikováno v: 第3回宇宙科学シンポジウム = Proceedings of the 3rd Space Science Symposium. :101-104

資料番号: AA0045441027

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fe43eae73e1226ee57cdf8a36bc4a245
http://id.nii.ac.jp/1696/00011626/

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Venus mission by a small space probe: Experimental plan on Venus capsule balloon and solar sail

Autor: Morita, Yasuhiro, Kawaguchi, Junichiro, Yamada, Tetsuya, Hiraki, Koju, Matsui, Masayasu, Honda, Masahisa

Publikováno v: 第3回宇宙科学シンポジウム = Proceedings of the 3rd Space Science Symposium. :113-116

小型探査機による金星ミッションについて、初期検討を行った結果を紹介する。想定している探査機の規模は地球脱出時の総重量で約150kgである。計画の目的は、金星カプセルによる金�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d283b4963699a21309ce322609d4bed0
http://id.nii.ac.jp/1696/00011629/

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Planetary exploration and astronomical observation by using a solar sail propulsion system

Autor: Yano, Hajime, Hasegawa, Sunao, Ishiguro, Masateru, Matsuura, Shuji, Imamura, Takeshi

Publikováno v: 第3回宇宙科学シンポジウム = Proceedings of the 3rd Space Science Symposium. :109-112

資料番号: AA0045441029

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::890e104e9071aef6633da77751f45778
http://id.nii.ac.jp/1696/00011628/

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Venus entry capsule: From the entry to the release of a sounding balloon

Autor: Yamada, Tetsuya, Hiraki, Koju, Izutsu, Naoki, Honda, Masahisa

Publikováno v: 宇宙航行の力学シンポジウム平成14年度 = Symposium on Flight Mechanics and Astrodynamics 2002. :95-98

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::80be9f5391c31c49767a0e31836c8565
http://id.nii.ac.jp/1696/00014706/

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Minimum ballistic coefficients of Venus exploration: Possibility of an aerocapture satellite

Autor: Nakazawa, Eiko, Yamada, Kazuhiko, Suzuki, Kojiro

Publikováno v: 宇宙航行の力学シンポジウム平成14年度 = Symposium on Flight Mechanics and Astrodynamics 2002. :103-106

資料番号: AA0045913027

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f2bf92a5e0dcbbe5dd1abba495aea2b0
http://id.nii.ac.jp/1696/00014708/

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The 22nd ISAS Space Energy Symposium March 12, 2003

Autor: Institute of Space and Astronautical Science

Publikováno v: 第22回宇宙エネルギーシンポジウム平成14年度 = The 22nd ISAS Space Energy Symposium March 12, 2003.

宇宙エネルギーシンポジウム宇宙科学研究所 20030312 神奈川日本
ISAS Space Energy Symposium Institute of Space and Astronautical Science 20030312 Kanagawa Japan
資料番号: AA0045915000

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::25e5f16049d4d83526d4b0da3976dc91
http://id.nii.ac.jp/1696/00008144/

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