日本地球惑星科学連合2016年大会

講演情報

ポスター発表

セッション記号 P (宇宙惑星科学) » P-EM 太陽地球系科学・宇宙電磁気学・宇宙環境

[P-EM19] 太陽圏・惑星間空間

2016年5月25日(水) 17:15 〜 18:30 ポスター会場 (国際展示場 6ホール)

コンビーナ:*坪内 健(東京工業大学大学院理工学研究科)、西野 真木(名古屋大学宇宙地球環境研究所)、成行 泰裕(富山大学人間発達科学部)

17:15 〜 18:30

[PEM19-P02] Solar neutron observations with ChubuSat-2 satellite

*山岡 和貴1宮澤 拓也1尾関 真二1馬場崎 康伸1林 祐貴1石原 大助1伊藤 和也1金田 英宏1河原 宏晃1久保 信2松下 幸司1宮田 喜久子1長野 方星1成澤 泰貴1西野 真木1野田 宗佑1朴 大逸1定本 真明2田島 宏康1田村 啓輔1田中 秀孝1Dao Tam1渡部 豊喜1周 大東1 (1.名古屋大学、2.クリアパルス株)

キーワード:Sun, Neutron, Satellite observations

Solar neutron observation is a key in understanding of ion accerelation mechanism in the Sun surface since neutrons are hardly affected by magnetic field around the Sun and intersteller mediums unlike charged particles. However, there was only a few tenth detections so far since its discovery in 1982. Actually SEDA-AP Fiber detector (FIB) onboard the International Space Station (ISS) was suffered from a high neutron background produced by the ISS itself.
ChubuSat is a series of 50-kg class microsatellite jointly depeloped by universities (Nagoya university and Daido university) and aerospace companies at the Chubu area of central Japan. The ChubuSat-2 is the second ChubuSat following the ChubuSat-1 which was launched by Russian DNEPR rocket on November 6, 2014. It was selected as one of four piggyback payloads of the X-ray astronomy satellite ASTRO-H in 2014 summer, and will be launched by the H-IIA launch vehcles from from JAXA Tanegashima Space Center (TNSC) in February 2016. The ChubuSat-2 carries a mission instrument,
radiation detector (RD). The main mission of ChubuSat-2 is devoted for monitoring neutrons and gamma-rays which can be background source for ASTRO-H celestrial observations with the RD. The mission also involves a function of solar neutron observations which were originally proposed by graduate students who join the leadership development program for space exploration and research, program for leading graduate schools at Nagoya University. The RD has a similar detection area and efficiency to those of the SEDA-AP FIB, but is expected to have lower backgrounthan the ISS thanks to much smaller mass of the micro-satellite. In this paper, we will describe details of ChubuSat-2 satellite and RD, and in-orbit performance of RD.