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オゴハラ カズノリ
OGOHARA Kazunori
小郷原 一智 所属 京都産業大学 理学部 宇宙物理・気象学科 職種 准教授 |
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| 発行・発表の年月 | 2012 |
| 形態種別 | 研究論文（国際会議プロシーディングス） |
| 査読 | 査読あり |
| 標題 | Return to venus of the Japanese venus climate orbiter akatsuki |
| 執筆形態 | その他 |
| 掲載誌名 | Proceedings of the International Astronautical Congress, IAC |
| 巻・号・頁 | 3,1727-1732頁 |
| 著者・共著者 | Nakamura M,Kawakatsu Y,Hirose C,Imamura T,Ishii N,Abe T,Yamazaki A,Yamada M,Ogohara K,Uemizu K,Fukuhara T,Ohtsuki S,Satoh T,Suzuki M,Ueno M,Iwagami N,Taguchi M,Watanabe S,Takahashi Y,Hashimoto G.L,Yamamoto H |
| 概要 | Japanese Venus Climate Orbiter/AKATSUKI was proposed in 2001 with strong support by international Venus science community and approved as an ISAS (Institute of Space and Astronautical Science) mission soon after the proposal. The mission life we expected was more than two Earth years in Venus orbit. AKATSUKI was successfully launched at 06:58:22JST on May 21, 2010, by H-IIA F17. After the separation from H-IIA, the telemetry from AKATSUKI was normally detected by DSN Goldstone station (10:00JST) and the solar cell paddles' expansion was confirmed. The malfunction happened on the propulsion system during the Venus orbit insertion (VOI) on Dec 7, 2010. We failed to make the spacecraft become a Venus orbiter, and the spacecraft entered an orbit around the Sun with a period of 203 days. Most of the fuel still had remained, but the orbital maneuvering engine was found to be broken. We decided to use only the reaction control system (RCS) for orbital maneuver and three minor maneuvers in Nov 2011 were successfully done so that AKATSUKI will meet Venus in 2015. We are considering several scenarios for VOI using only RCS. Copyright © (2012) by the International Astronautical Federation. |
| ISSN | 0074-1795 |
| Put Code(ORCID) | 52343291 |
| PermalinkURL | http://www.scopus.com/inward/record.url?eid=2-s2.0-84883545839&partnerID=MN8TOARS |
| researchmap用URL | http://orcid.org/0000-0001-7666-4442 |