Measurement of the directional distribution of incident particles in the Shuttle-Mir mission orbit

Takao Sakaguchi; Tadayoshi Doke; Nobuyuki Hasebe; Jun Kikuchi; Sachiko Kono; Toru Takagi; Kenichi Takahashi; Shunji Nagaoka; Tamotsu Nakano; Shimpei Takahashi; Gautam D. Badhwar

Measurement of the directional distribution of incident particles in the Shuttle-Mir mission orbit

Takao Sakaguchi^*, Tadayoshi Doke, Nobuyuki Hasebe, Jun Kikuchi, Sachiko Kono, Toru Takagi, Kenichi Takahashi, Shunji Nagaoka, Tamotsu Nakano, Shimpei Takahashi, Gautam D. Badhwar

^*この研究の対応する著者

研究成果: Article › 査読

7 被引用数 (Scopus)

抄録

The measurement of the directional distribution of incident particles was made by using the Real time Radiation Monitoring Device (RRMD)-III placed inside the Space Shuttle STS-84 cruised at an altitude of 400 km and an inclination angle of 51.6°, which are the same as the cruising orbit of the International Space Station (ISS). The directional distributions of incident particles were evaluated over the observed linear energy transfer (LET) range (1-100 keV/μm). The pitch angle distribution is also obtained using the geomagnetic model of IGRF-95. The result is roughly in good agreement with the distribution obtained by the VF1-MIN anisotropy model calculation within the present experimental errors, if the shielding distribution is assumed to be uniform.

本文言語	English
論文番号	1999JA900231
ページ（範囲）	22793-22799
ページ数	7
ジャーナル	Journal of Geophysical Research: Space Physics
巻	104
号	A10
出版ステータス	Published - 1999

ASJC Scopus subject areas

地球化学および岩石学
地球物理学
地球惑星科学（その他）
宇宙惑星科学
大気科学
天文学と天体物理学
海洋学

他のファイルとリンク

引用スタイル

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title = "Measurement of the directional distribution of incident particles in the Shuttle-Mir mission orbit",

abstract = "The measurement of the directional distribution of incident particles was made by using the Real time Radiation Monitoring Device (RRMD)-III placed inside the Space Shuttle STS-84 cruised at an altitude of 400 km and an inclination angle of 51.6°, which are the same as the cruising orbit of the International Space Station (ISS). The directional distributions of incident particles were evaluated over the observed linear energy transfer (LET) range (1-100 keV/μm). The pitch angle distribution is also obtained using the geomagnetic model of IGRF-95. The result is roughly in good agreement with the distribution obtained by the VF1-MIN anisotropy model calculation within the present experimental errors, if the shielding distribution is assumed to be uniform.",

author = "Takao Sakaguchi and Tadayoshi Doke and Nobuyuki Hasebe and Jun Kikuchi and Sachiko Kono and Toru Takagi and Kenichi Takahashi and Shunji Nagaoka and Tamotsu Nakano and Shimpei Takahashi and Badhwar, {Gautam D.}",

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T1 - Measurement of the directional distribution of incident particles in the Shuttle-Mir mission orbit

AU - Sakaguchi, Takao

AU - Doke, Tadayoshi

AU - Hasebe, Nobuyuki

AU - Kikuchi, Jun

AU - Kono, Sachiko

AU - Takagi, Toru

AU - Takahashi, Kenichi

AU - Nagaoka, Shunji

AU - Nakano, Tamotsu

AU - Takahashi, Shimpei

AU - Badhwar, Gautam D.

PY - 1999

Y1 - 1999

N2 - The measurement of the directional distribution of incident particles was made by using the Real time Radiation Monitoring Device (RRMD)-III placed inside the Space Shuttle STS-84 cruised at an altitude of 400 km and an inclination angle of 51.6°, which are the same as the cruising orbit of the International Space Station (ISS). The directional distributions of incident particles were evaluated over the observed linear energy transfer (LET) range (1-100 keV/μm). The pitch angle distribution is also obtained using the geomagnetic model of IGRF-95. The result is roughly in good agreement with the distribution obtained by the VF1-MIN anisotropy model calculation within the present experimental errors, if the shielding distribution is assumed to be uniform.

AB - The measurement of the directional distribution of incident particles was made by using the Real time Radiation Monitoring Device (RRMD)-III placed inside the Space Shuttle STS-84 cruised at an altitude of 400 km and an inclination angle of 51.6°, which are the same as the cruising orbit of the International Space Station (ISS). The directional distributions of incident particles were evaluated over the observed linear energy transfer (LET) range (1-100 keV/μm). The pitch angle distribution is also obtained using the geomagnetic model of IGRF-95. The result is roughly in good agreement with the distribution obtained by the VF1-MIN anisotropy model calculation within the present experimental errors, if the shielding distribution is assumed to be uniform.

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JO - Journal of Geophysical Research: Space Physics

JF - Journal of Geophysical Research: Space Physics

IS - A10

M1 - 1999JA900231

ER -

Measurement of the directional distribution of incident particles in the Shuttle-Mir mission orbit

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ASJC Scopus subject areas

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