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  1. 学術雑誌論文

Trajectory of HAYABUSA Reentry Determined from Multisite TV Observations

http://hdl.handle.net/10173/781
http://hdl.handle.net/10173/781
d2e265a5-17a2-4b5f-9ee2-a4531fd1eb40
名前 / ファイル ライセンス アクション
PASJ_63_5_947.pdf PASJ_63_5_947.pdf (1.9 MB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2012-01-27
タイトル
タイトル Trajectory of HAYABUSA Reentry Determined from Multisite TV Observations
言語
言語 eng
キーワード
主題Scheme Other
主題 meteors
キーワード
主題Scheme Other
主題 meteoroids
キーワード
主題Scheme Other
主題 space vehicles
キーワード
主題Scheme Other
主題 individual (HAYABUSA)
キーワード
主題Scheme Other
主題 space vehicles
キーワード
主題Scheme Other
主題 trajectory
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ journal article
著者 UEDA, Masayoshi

× UEDA, Masayoshi

UEDA, Masayoshi

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SHIBA, Yasuo

× SHIBA, Yasuo

SHIBA, Yasuo

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YAMAMOTO, Masa-yuki

× YAMAMOTO, Masa-yuki

YAMAMOTO, Masa-yuki

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FUJITA, Kazuhisa

× FUJITA, Kazuhisa

FUJITA, Kazuhisa

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WATANABE, Jun-ichi

× WATANABE, Jun-ichi

WATANABE, Jun-ichi

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SATO, Mikiya

× SATO, Mikiya

SATO, Mikiya

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ABE, Shinsuke

× ABE, Shinsuke

ABE, Shinsuke

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KAKINAMI, Yoshihiro

× KAKINAMI, Yoshihiro

KAKINAMI, Yoshihiro

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UEHARA, Satoshi

× UEHARA, Satoshi

UEHARA, Satoshi

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OKAMOTO, Sadao

× OKAMOTO, Sadao

OKAMOTO, Sadao

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FUJIWARA, Yasunori

× FUJIWARA, Yasunori

FUJIWARA, Yasunori

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TANABE, Tsutomu

× TANABE, Tsutomu

TANABE, Tsutomu

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抄録
内容記述タイプ Abstract
内容記述 The asteroid explorer HAYABUSA reentered into the Earth's atmosphere on 2010 June 13. We made simultaneous TV (television) observations at seven ground sites in order to calculate the trajectories of HAYABUSA and its sample return capsule (SRC), which both reentered into the atmosphere. Our TV observations showed that, after HAYABUSA reentered the atmosphere, the beginning time of its light emission on video was 13:51:57.4 UT at a height of 101.00.2 km. The end time was 13:52:42.0 UT at a height of 38.60.2 km. The initial velocity at the beginning was 12.10.3 km s, and the entry angle was 9. After identifying SRC as separated light emission independent of the mother spacecraft, we analyzed the trajectory of SRC from a height of 52.9 km to 35.7 km based on video images. The actual trajectory of the capsule, determined from the TV observations, was almost the same as the predicted trajectory in terms of the position, velocity, and time. We then calculated the fall spots of the SRC heat shields from the multisite TV observations.
書誌情報 Publications of the Astronomical Society of Japan

巻 63, 号 5, p. 947-953, 発行日 2011-10-25
ISSN
収録物識別子タイプ ISSN
収録物識別子 0004-6264
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA1082896X
権利
権利情報 (c) 2011 Astronomical Society of Japan
著者版フラグ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
出版者
出版者 Astronomical Society of Japan
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