Studies on Solar System Explorations using DESTINY: the Demonstration and Experiment of Space Technology for Interplanetary Voyage
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- IWATA Takahiro
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, JAXA Sagamihara Campus, Sokendai
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- KAWAKATSU Yasuhiro
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, JAXA Sagamihara Campus, Sokendai
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- MURAKAMI Go
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, JAXA
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- EZOE Yuichiro
- Tokyo Metropolitan University
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- KAMEDA Shingo
- Rikkyo University
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- KEIKA Kunihiro
- Solar-Terrestrial Environment Laboratory, Nagoya University
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- ARAI Tomoko
- Chiba Institute of Technology
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- MATSUURA Shuji
- Kwansei Gakuin University
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- SAIKI Takanao
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, JAXA
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- IMAMURA Takeshi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, JAXA
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- OGOHARA Kazunori
- University of Shiga Prefecture
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- OYAMA Akira
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, JAXA
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- IKENAGA Toshinori
- Japan Aerospace Exploration Agency, JAXA
抄録
<p>DESTINY: the Demonstration and Experiment of Space Technology for Interplanetary Voyage, which is a candidate mission of Epsilon Launch Vehicle, plans to execute scientific observations using instruments with the mass of up to about 10 kg on the transfer and Halo orbit of the sun to earth Lagrangian point L1/L2 or on the fly-by orbit of near earth objects (NEO). Potential scientific objects include in-situ observation and remote sensing from these space are solar system explorations, such as, the observations of plasma and energetic particles around the terrestrial magnetosphere, inter-planetary and inter-stellar dust, and NEO. It is also considered to be useful for the pilot observations for future infrared, gamma-ray, and cosmic-ray space astronomical telescope in the deep space. Applied missions of DESTINY will be able to go to deep space with higher mass of payloads. Using the Epsilon Launch Vehicle, it will convey instruments of up to 50 kg to the space between Venus and Mars. DESTINY launched by the improved launch vehicle with the power of M-V rocket will carry payloads of up to 200 kg into the orbit of Venus and Mars. In these phases, Explorations for Venus, Mars, and multiple NEO, and astronomical observations from the deep space observatory will be realized by low cost deep space missions.</p>
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 14 (ists30), Pk_111-Pk_116, 2016
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001205321551232
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- NII論文ID
- 130005252789
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- ISSN
- 18840485
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可